www.iccm22.com

Conference hosts

Information is correct at time of publication and is subject to change. PROGRAM BOOK 2 WELCOME MESSAGE 3

WELCOME TO MELBOURNE, AUSTRALIA AND THE 22ND INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS CONTENTS We are very proud to be organising ICCM22 and we trust you will have an outstanding experience at the conference and during your stay in WELCOME MESSAGE 2 Melbourne and Australia. VENUE OVERVIEW 6 ICCM22 continues the 44 year history of the International Conferences on GENERAL INFORMATION 8 Composite Materials, which commenced in 1975. This is the second time SOCIAL PROGRAM 10 an ICCM has been held in Australia, with the first conference (ICCM11) held in Queensland in 1997. ICCM22 is proudly brought to you by the Australian SPONSORS 11 Composites Structures Society, which is a professional society of Engineers EXHIBITION 22 Australia. COMMITTEE LISTS 25 The theme of ICCM22 is ‘Advanced Composites: Research to Impact’ with the overall objective of exploring the latest research into composites SCIENTIFIC PROGRAM CODES 28 and how the materials will be used in the future for applications including aerospace, construction, wind energy and automotive. SCALA AND PLENARY LECTURES 30 The scientific program of ICCM22 contains about 1513 presentations with the authors coming from over 50 countries representing the three ICCM KEYNOTE LECTURES 32 world regions. Delegates from all parts of the composites sector, including SCIENTIFIC PROGRAM 34 universities, research institutions, government agencies, material suppliers, manufacturers and other industry, are attending ICCM22. Such diversity POSTER PROGRAM 95 will ensure a vibrant, engaging and multifaceted conference. We are grateful to all authors for their outstanding contributions to the ICCM22 scientific program, which we believe is first rate. CONFERENCE CHAIRS The full ICCM22 program is printed in this book along with helpful information, including the locations of the session rooms in the Melbourne Convention and Exhibition Centre, Exhibition display area, locations for lunch and breaks, and details about the conference sponsors.

The ICCM22 conference proceedings contain the abstract, full paper or PowerPoint slides for presentations. The proceedings also contain the poster for poster presentations. You can easily access the proceedings via the ICCM22 website Adrian Mouritz (www.iccm.com) or the ICCM22 App. This program booklet is also accessible via the website and App.

We hope you greatly enjoy the many events and technical tours planned throughout ICCM22, all of which are described in this program. Conference updates on events and practical matters will be issued throughout the program via electronic notifications through the website and Conference app. Also remember to check the electronic notice boards in front of each session room for last minute, unavoidable changes to the program. If you need any assistance during the conference then please do not hesitate to Chun Wang contact the ICCM22 secretariat or us for help. Assistants will be present in all session rooms.

We sincerely thank Engineers Australia, MCI, the Local Organising Committee and the International Scientific Committee and student volunteers for their outstanding work; without which the conference would not be possible. Once again, welcome to Melbourne Australia and enjoy ICCM22. Bronwyn Fox

Research Program

Building on our strong collaborations between industry and university partners ATLAS will train urgently needed commercially focused researchers specialising in lightweight multi-material structures obtained through advanced, agile and digital manufacturing technologies.

ATLAS comprises an integrated research program encompassing four themes as outlined below:

LIGHTWEIGHT DESIGN AND ADVANCED MATERIALS MANUFACTURING

Research underpinning the development and Advancement of agile and digital manufacturing efficient processing of high-performance technologies such as additive manufacturing, lightweight materials like carbon-fibre flexible roll forming technologies and composites and highly formable metal alloys multi-material joining techniques to enable for the manufacture of next generation local manufacturers to efficiently produce lightweight components and assemblies high value products for local and by Australian manufacturers. international markets.

INTEGRATED WHOLE OF LIFE MULTI-MATERIAL ASSESSMENT

STRUCTURES Validating the whole of life economic, Design and demonstration of smart integrated environmental and societal benefits of multi-material structures such as those with next generation lightweight multi-material gradient physical properties for controlled structures through quantitative life cycle crush or imbedded functional features like the assessments and the development of decision capacity to store electrical energy for future making tools to help guide design choices. mobility solutions.

Our Partners

COMPOSITE MATERIALS ENGINEERING PTY LTD

Building 251, RMIT University, P: +61 3 9925 6048 @AtlasInnov8n Bundoora East, VIC E: [email protected] @AtlasInnov8n Plenty Rd, Bundoora VIC 3083 @AtlasInnov8n JOIN THE CONVERSATION

How to use the app About Program SEARCH MCI GROUP EVENT PORTAL IN YOUR PHONE OR TABLET’S APP STORE. ONCE THIS IS DOWNLOADED, Speakers Exhibitors Sponsors ENTER THE EVENT CODE: ICCM22

Floor Plans Venue Technical Tours PROGRAM

EXHIBITORS

VIRTUAL SATCHEL

SPEAKERS

TECHNICAL TOURS

SPONSORS VENUE OVERVIEW 6 7

ICCM22 session rooms are indicated in red Entry

1 2 CONVENTION CENTRE Foyer GROUND FLOOR

Entry

Plenary Cafe PLENA2 RY 2 PLENARY 1 1 3

Foyer PLENARY 3 Exhibition C 3 Link: PLENARY COMBINED Thr en ough to tre Doors 1-10

SSTAtagGE • Entry CONVENTION CENTRE PLENARY • LEVEL 2 BACK OF HOUSE CUSTOMER SERVICE • WINDOWS • • CONVENTION CENTRE •

oom 1

LEVEL TWO F Melbourne R oyer

206 205 2

1 Foyer oom 2 211 Melbourne R 210 209 214 208 204 207 212 215 203 Foyer 213

216 217 218 219 3 220 PLENAR Y MEETING ROOMS

BACK OF HOUSE ORGANISERS’ OFFICES SPEAKER PREPARATION ROOM

DRESSING ROOMS

WINDOWS

Clarendon Street Entrance

Clarendon Street Shed Café G Entrance

EXHIBITION CENTRE Shed Café G GROUND FLOOR 1 2

3

4 1 5 2 6 1 Convention Centre Place 3 Entrance 7 Link 4 CONVENTION CENTRE 8 5 Goldfields Northern concourse 9 Café and Bar 6 Novotel Melbourne 1 Convention Centre Place 10 South Wharf and Entrance 7 Link DFO car park 11 8

Goldfields 12 26 Northern concourse 9 Café and Bar Novotel Melbourne 25 13 South Wharf and 24 Foyer 10 23 Courtyard 14 DFO car park 1 11 22 15 21 2 12 26 Exhibition 16 25 Centre link 13 3 Foyer 24 2 17 23 1 14 1 Courtyard 22 18 EXHIBITION BAYS 15 21 2 19 GOLDFIELDS EVENT SPACE Exhibition 16 Centre link GOLDFIELDS THEATRE 3 20 2 17 1 MEETING ROOMS 18 ORGANISERS’ OFFICES 19 KIOSKS / CAFÉ 20 WINDOWS GENERAL INFORMATION 8 9

REGISTRATION DESK OPENING TIMES INTERNET ACCESS The registration desk will be located in the exhibition Most Australian hotels offer wired or wireless high- PROCEEDINGS concourse foyer and will be open during the following speed internet access in their guest rooms. Most All accepted presentations will be included in the In case you are not feeling well please find the nearest times: hotels will also have a business centre with available official ICCM proceedings. The proceedings will be GP clinics. Fees may apply to any medical treatment. computers and printers for their guests to use. INFORMATION GENERAL DATE TIME available to registered ICCM22 delegates via the official website and conference app. Sunday 11 August 1400–1800 While onsite at the conference a complimentary wifi Freshwater Place Wellness Medical Practice service is available to all delegates: Monday 12 August 0700–2100 Suite 13-15/1 Freshwater Place, Southbank VIC 3006 T: +61 3 9926 3646 Tuesday 13 August 0700–1830 Network Name: ICCM22 CPD HOURS Password: Composites www.fpwmp.com.au Wednesday 14 August 0700–1830 Attendance at the 22nd International Conference on Thursday 15 August 0700–1830 There is no other Business Lounge facility provided at Composite Materials entitles you to earn professional My Clinic Southbank Friday 16 August 0700–1530 the conference or at the Melbourne Convention and development hours from Engineers Australia. We Exhibition Centre. recommend visiting the official conference website, 63 Power Street, Southbank, 3006 specifically the conference program page for more T: +61 3 9131 4210 SPEAKER PREPARATION ROOM www.myclinicgroup.com.au/our-clinics/myclinic-southbank CATERING AND SPECIAL DIETS details. A speaker preparation room is available for all chairpersons and speakers during the conference. Morning and afternoon tea, as well as lunches are FIRST AID This is a room specifically reserved for speakers being served for all delegates within the exhibition. The conference will have professional first aid and chairpersons to work on, load and practice their A special diet requirement is when a person chooses assistance onsite – see staff at the registration desk for presentations/chairing duties or simply just to relax to omit certain foods or food groups from their diet on information. and de-stress prior to their program responsibilities. religious, ethical, moral or medical grounds. Provision The speaker preparation room is located in Meeting will be made for food intolerances, halal and kosher Room 220 at the Melbourne Convention and requests, as well as vegetarian/vegan requests. EMERGENCY Exhibition Centre and will be staffed by professional If you have confirmed a special dietary requirement In an emergency, dial 000 for fire, police, and AV technicians and will be open during the following at time of registration, there will be a separate special ambulance. The nearest public hospitals are: times: dietary requirements table available during the catering breaks. DATE TIME Alfred Hospital Monday 12 August 0700–1800 SMOKING 55 Commercial Road, Melbourne Tuesday 13 August 0700–1800 T: +61 3 9076 2000 There is no smoking indoors or within enclosed public www.alfredhealth.org.au Wednesday 14 August 0700–1600 areas in Melbourne. The Melbourne Convention and Thursday 15 August 0700–1800 Exhibition Centre is also a smoke free environment. Royal Melbourne Hospital Friday 16 August 0700–1500 300 Grattan Street, Parkville LANGUAGE T: +61 3 9342 7000 www.thermh.org.au EXHIBITION OPENING TIMES The official language of the 22nd International The ICCM22 exhibition will be in exhibition bays 11/12, Conference on Composite Materials is English. accessible via door 6.

DATE TIME INSURANCE Monday 12 August 1030–2100 The 22nd International Conference on Composite Tuesday 13 August 1000–1830 Materials is unable to accept responsibility for Wednesday 14 August 1000–1630 accidents or damage to the private property of participants. Please ensure that you do not leave Thursday 15 August 1000–1830 portable and valuable pieces of equipment unattended Friday 16 August 1000–1530 anywhere, and that you make your own arrangements for health, travel, general and other insurance.

SOCIAL PROGRAM SPONSORS 10 11

WELCOME RECEPTION - MONDAY 12 AUGUST 2019 DESTINATION SPONSOR ICCM22 PARTNER

Time: 1845–2100 Location: Exhibition Bays 11 and 12, Melbourne Convention and Exhibition Centre (MCEC) Dress Code: Business Casual

Sponsor: PRINCIPAL PARTNER

MAJOR PARTNER

STUDENT PARTY - TUESDAY 13 AUGUST 2019 a c c i s

ADVANCED COMPOSITES COLLABORATION FOR INNOVATION & SCIENCE Time: 1900–2300 Location: Wunderbar – Munich South Wharf 45 South Wharf Promenade, South Wharf VIC 3006 Dress Code: Business Casual ASSOCIATE PARTNER Please make your way to Munich South Wharf or be at the conference registration desk at 1845 to be escorted to the student party venue.

Sponsor:

ICCM22 BANQUET - THURSDAY 15 AUGUST 2019 SUPPORTING PARTNER Time: 1845-2230 Location: Melbourne Room, Melbourne Convention and Exhibition Centre (MCEC) Dress Code: Semi Formal/ Business “Jacket”

Sponsor:

Academic Open Access Publishing since 1996 SPONSORS 12 13

DESTINATION SPONSOR PRINCIPAL PARTNER SPONSORS Melbourne Convention Bureau Altair

With its vibrant culture, multicultural population, Altair (Nasdaq: ALTR) is a global technology company temperate climate and outstanding quality of life, that provides software and cloud solutions in the Melbourne is an ideal destination for delegates. The city areas of product development, high-performance is compact, convenient and easy to navigate inviting computing (HPC), and data intelligence. Altair enables you to discover its creative culture through all its organizations across broad industry segments to elements; from art and fashion, to the sports scene and compete more effectively in a connected world while renowned diverse gastronomy. creating a more sustainable future.

The city is home to historical and modern architecture, BOOTH 17 & 18 We are a leading provider of enterprise-class hidden laneways, beautiful green spaces, art galleries, Rajneesh Shinde engineering software enabling innovation, reduced music venues and a wealth of attractions providing T: +91 9890 025 140 development times, and lower costs through the unlimited choices for exploration. E: [email protected] entire product lifecycle from concept design to W: altair-anz.com in-service operation. Boasting a myriad of restaurants, bars, hatted dining rooms and coffee shops, Melbourne is a foodie paradise for all visitors and locals alike. PRINCIPAL PARTNER Boeing Once your conference day is over, be prepared to feel the city in every corner and on the countless immersive Holly Row Boeing’s presence in Australia is the company’s T: +61 3 9002 2395 experiences on offer. E: [email protected] largest footprint outside the United States, with more W: melbournecb.com.au than 3,000 employees in 38 locations. Boeing has the For more information and ideas, visit melbourne.org broadest portfolio in Australian aerospace, with its employees and an extensive supply chain supporting BOOTH 27 & 28 our advanced manufacturing of commercial aircraft ICCM22 PARTNER Melanie de Git composite components, defence systems design and AFOSR T: +61 423 829 505 development, modeling and simulation, research and E: [email protected] development, support and training, and unmanned The Air Force Office of Scientific Research (AFOSR) is W: boeing.com.au systems. an integral part of the Air Force Research Laboratory (AFRL).

As its basic research manager, AFOSR provides MAJOR PARTNER grants and contracts to universities worldwide, MSC Software small businesses in the U.S., and various Technology Directorates of AFRL. All support basic research MSC Software develops simulation software technology activities with potential applications to the future Air that enables engineers to validate and optimize Force. AFOSR is a global organization with branches their designs using virtual prototypes. Customers in located in Arlington, Virginia; London, UK; Tokyo, Japan; almost every part of manufacturing use our software and Santiago, Chile. to complement, and in some cases even replace the physical prototype “build and test” process that has We believe basic research is the foundation of all traditionally been used in product design. Molly Lachance science and engineering discovery and progress and T: +1 703 588 0198 spawns the inventions and concepts - many of which As a trusted partner, MSC Software helps companies E: [email protected] BOOTH 19 improve quality, save time and reduce costs associated W: www.afresearchlab.com are revolutionary. Kingsley Edgar with design and test of manufactured products. Our T: +61 418 727 791 products accurately and reliably predict how products E: [email protected] will behave in the real world to help engineers design W: mscsoftware.com more innovative products - quickly and cost effectively. MAJOR PARTNER ASSOCIATE PARTNER University of Bristol DMTC Limited 14 15 Bristol in the UK is THE place in the world for DMTC works collaboratively with many successful SPONSORS a c c i s ADVANCED COMPOSITES COLLABORATION FOR INNOVATION & SCIENCEcomposites R&D. Not only is it a hub for industries and innovative Australian industry, research and leading the way in composites adoption it is home to government agencies to advance technologies in s two world-leading composites partners - The National areas identified as priorities by Defence. Our focus is a c c i SPONSORS

ADVANCED COMPOSITES COLLABORATION FOR INNOVATION & SCIENCE Composites Centre and Bristol Composites Institute on delivering enhanced defence and national security (ACCIS). capabilities, and strengthening Australian industrial capacity. a c c i s The NCC is a world-leading authority on composites ADVANCED COMPOSITES COLLABORATION FOR INNOVATION & SCIENCE R&D, bringing together and developing the best minds Our proven approach delivers outstanding and technologies, to solve the world’s most complex Harry Baxter achievements in industrially-relevant research and BOOTH 20 engineering challenges. Bristol Composites Institute T: +61 3 9214 4447 adoption and commercialisation of technology, E: [email protected] Michael Wisnom (ACCIS) is a world-leading institute for composites W: dmtc.com.au underpinned by ISO:9001 accredited business T: +44 1173 315 311 research and education that combines cutting-edge processes. E: [email protected] fundamental science with strong industrial links for W: bristol.ac.uk/composites/ exploitation and technology transfer

ASSOCIATE PARTNER ASSOCIATE PARTNER Atlas Innovations Fill Gesellschaft m.b.H

Atlas aims to accelerate the transformation of Australia’s Fill is a family owned company located in Austria. 850 automotive industry through new research capabilities employees are developing, manufacturing high tech in lightweight automotive structures design and production solutions for different markets. manufacture. From fiber to the finished part – Fill delivers systems from the preforming process through to NDI. If you are seeking the best solution, shape your future with Fill. BOOTH 23 BOOTH 02 Cara Jordan T: +61 405 770 731 Wilhelm Rupertsberger E: [email protected] T: +43 6646 147 070 W: atlas-innovation.com.au E: [email protected] W: fill.co.at

ASSOCIATE PARTNER ASSOCIATE PARTNER Deakin University – Carbon Nexus Langzauner GmbH

Carbon Nexus is a globally unique open-access Langzauner is the leading expert in the development carbon fibre and composite research centre owned and production of hydraulic presses, automation and operated by Deakin University. Located at the solutions, special solutions and tailor-made concept Geelong Waurn Ponds Campus, Carbon Nexus solutions in the automotive, aerospace and sports facilitates world-class innovation in carbon fibre and industries. composite materials, researching all aspects of fibres BOOTH 01 BOOTH 22 and composites, scale-up, characterisation, applied Composite Presses, HP RTM Presses, Sandwich.Crush. Derek Buckmaster analysis and advanced manufacturing concepts. The Alexander Wiesner Core Honeycomb, Thermoforming/Thermoplastic/ T: +61 3 5247 9247 facility houses an industrial-scale carbon fibre Pilot Line T: +61 4377 652 310 Thermoset, Laboratory Presses, Ski/Snowboard Press E: [email protected] complemented by a Research-Scale Line to enhance E: [email protected] W: langzauner.at PCM-Prepreg Compression Molding, Sintering Press, W: carbonnexus.com.au research efficiency and flexibility. Molding Presses, Multi Processes, Panel Presses, Hot Presses/Heating Presses, Laboratory Presses, Electric Spindle Presses. ASSOCIATE PARTNER SUPPORTING PARTNER NETZSCH Australia Pty Ltd ARC Training Centre for Automated Manufacture of 16 Advanced Composites (AMAC) 17 The Analyzing & Testing business unit of the NETZSCH SPONSORS Group (est. 1873, Germany) develops and manufactures AMAC provides a platform for world-class Australian a complete high-precision instrument line for thermal capability to create high-value, high-performance analysis and thermophysical properties measurement, composites using high-rate, error-free processes.

as well as offering world class commercial testing SPONSORS services in our laboratories. Our instrumentation is The Training Centre lowers the barriers for Australian employed for research, quality control and process industry to access, engage, adopt and propagate BOOTH 21 BOOTH 03 control in the composites sector, the chemical automated composite manufacturing innovations. Andrew Gillen industry and the areas of inorganics and building Gangadhara Prusty T: +61 2 9641 2846 materials. Our innovative technological leadership and T: +61 2 9385 5939 E: [email protected] E: [email protected] W: netzsch.com.au uncompromising quality standards make us one of the W: advanced-composites.unsw.edu.au world’s leading manufacturers in our trade.

ASSOCIATE PARTNER SUPPORTING PARTNER Swinburne University of Technology Anton Paar Australia Pty. Ltd.

Swinburne is a world-ranked university leading the way Anton Paar develops, produces and distributes highly in innovation, industry engagement and social inclusion. accurate laboratory instruments and process measuring Our education, research and industry partnerships systems, and provides custom-tailored automation and create positive change for students, staff and the robotic solutions. community. BOOTH 24 It is the world leader in the measurement of density, At Swinburne, we’re proud that our high-quality concentration and CO2 and in the field of rheometry. Ashish Kumar Anton Paar GmbH is owned by the charitable Santner research meets the demands of society, government T: +61 2 8315 4419 and industry, and aims to improve the way we live and E: [email protected] Foundation. build a sustainable future. W: anton-paar.com/au-en/

Five key areas of focus drive our research centres and institutes. They include: future manufacturing, BOOTH 10 sustainable futures, digital frontiers, personal and societal wellbeing, and inspirational science and Alex Campbell technology. Our Manufacturing Futures Research T: +61 3 9214 4932 Institute integrates advanced manufacturing in the SUPPORTING PARTNER E: [email protected] ARC Centre for Advanced Manufacturing of W: swinburne.edu.au global value chain. Prefabricated Housing (CAMP.H), The University of Melbourne

The ARC Training Centre for Advanced Manufacturing of Prefabricated Housing (CAMP.H) is the centrepiece for collaborative and innovative prefabricated building ASSOCIATE PARTNER research in Australia. AND WELCOME RECEPTION SPONSOR University of Southern Queensland The centre aims to unlock the potential growth of BOOTH 25 Australia’s prefabricated building industry by creating University of Southern Queensland (USQ) has gained Prof. Priyan Mendis a co-operative training system between industry and a reputation for pioneering research and development T: +61 419 312 481 universities leading to local employment growth and in engineered fibre composites. USQ prioritises R&D in E: [email protected] increased exports of prefabricated products advanced composite manufacturing, civil composites, W: camph.eng.unimelb.edu.au/ and services. BOOTH 04 smart materials, and geopolymer & concrete. USQ operates a dedicated industry test service for more Laura Hunt than 1000 business clients across multiple sectors both T: +61 7 4631 2296 E: [email protected] nationally and internationally. W: Composites.usq.edu.au SUPPORTING PARTNER SUPPORTING PARTNER CIMComp 18 AND ICCM22 BANQUET SPONSOR Elsevier 19 The EPSRC Future Composites Manufacturing SPONSORS Elsevier is a global information analytics business Research Hub was launched in January 2017, led by the that helps scientists and clinicians to find new University of Nottingham and Bristol and includes 11 answers, reshape human knowledge, and tackle other national spokes. the most urgent human crises. For 140 years, we SPONSORS have partnered with the research world to curate It is a £10.3m investment to expand the UK’s research and verify scientific knowledge. Elsevier’s materials effort towards delivering a step change in the science journals’ programme is the largest publishing production of polymer matrix composites, whilst programme in materials science, which includes training the next generation of composite engineers our flagship title Materials Today as well as over 60 Lee Harper T: +44 115 951 3823 specialty journals covering full spectrum of materials E: [email protected] science. In composites field, we are proud to serve W: cimcomp.ac.uk Elsevier Materials Team the community with our premium collection of 6 titles: T: +44 1865 843 577 Composites Science and Technology, Composites Part E: [email protected] W: elsevier.com A and B, Composite Structures, Cement and Concrete Composites, and Composites Communications

SUPPORTING PARTNER SUPPORTING PARTNER CONE Technology Instron

CONE Technology Group, located in US, Japan and Founded in 1946, Instron® is a recognized worldwide China, is committed to bring Carbon Nanotubes (CNTs) market leader in the materials testing industry. into our life. Instron offers one of the largest product ranges in With the mass production capability of high quality the industry, supplying systems and accessories CNTs, a variety of available CNT morphologies from screw-driven electromechanical machines to including aligned CNT forest, powder, fiber, and servohydraulic fatigue, impact, rheology, through to BOOTH 08 BOOTH 13 Lindsey Gadinski freestanding films will meet your needs. structural testing rigs and crash simulation sleds. T: +13 0253 36024 Rajesh Jagmohan E: [email protected] T: +61 3 9720 3477 W: chinacone.com E: [email protected] W: instron.com.au/en-au/our-company/about- us?region=Australia&lang=en-AU

SUPPORTING PARTNER DKSH Australia SUPPORTING PARTNER JEC Group DKSH Scientific Instrumentation, within Business Unit Technology, supplies a wide range of la-boratory JEC Asia 2019, the 3-day business & networking event instruments, scientific equipment, life science products dedicated to composites in Asia Pacific, will be held and consumables, to laboratories in the government, in Seoul on November 13-15, 2019 in parallel to eMove research, university, contract analysis and industrial Asia. sectors. We also provide applications support and service across all the sectors. Join composites key players gathering every year at JEC Asia to network and discover the endless possibilities The DKSH Scientific Instrumentation group offers BOOTH 12 of composites. products and services for Scientific Instrumenta-tion, Nelly Baron Jenny Thistlethwaite Automation & Online Analysers, General Laboratory T: +06 46 39 19 16 T: +61 408 761 177 E: [email protected] E: [email protected] Equipment, Environmental & Clinical Diagnostic Kits, W: jeccomposites.com W: direct.dksh.com.au/lab Consumables and Reagents. SUPPORTING PARTNER SUPPORTING PARTNER AND ICCM22 WOMEN MDPI 20 IN COMPOSITES LEADERSHIP FORUM SPONSOR RMIT University 21 MDPI is an academic open-access publisher with SPONSORS headquarters in Basel, Switzerland. MDPI publishes 202 RMIT is a global university of technology, design peer-reviewed, scientific, open access journals. and enterprise. One of Australia’s original tertiary institutions, RMIT University enjoys an international

All journals uphold a peer-reviewed, rapid, and rigorous reputation for excellence in professional and vocational SPONSORS Academic Open Access Publishing education, applied research, and engagement with the since 1996 publication process to publish your work under a CC BY license, in a fast and straightforward manner, and to needs of industry and the community. RMIT’s School of reach a wide readership. Engineering is renowned for its industry-relevant high- quality teaching and research, its globally competitive BOOTH 14 graduates and its international linkages. Our vision is to Adrian Mouritz MDPI Marketing Department T: +61 3 9925 6269 be recognised for innovative, industry-relevant teaching T: +86 10 6256 3691 E: [email protected] and research, and work-ready graduates E: [email protected] W: rimit.edu.au/schools/engineering W: mdpi.com

SUPPORTING PARTNER SUPPORTING PARTNER Quickstep Holdings Limited Thermo Fisher Scientific

Quickstep Holdings Limited is Australia’s largest Thermo Fisher Scientific is the world leader in serving independent aerospace-grade advanced composite science, enabling customers to make the world manufacturer, operating from advanced manufacturing healthier, cleaner and safer. facilities at Bankstown, NSW and an R&D/ process development centre in Geelong, Victoria. Quickstep Our comprehensive range includes high-end analytical employs more than 240 people in Australia and is and process instrumentation, laboratory equipment, partnering with some of the world’s largest aerospace/ a complete range of consumables, chemicals and defence organisations including Lockheed Martin, reagents as well as the service and support to BOOTH 26 Northrop Grumman, Boeing Defense and BAE BOOTH 16 optimise your results. Systems, as well as Australian-based Marand Precision Carl de Koning Customer Service T: +61 413 884 209 Engineering and Chemring Australia. T: (Australia) 1300 735 292 (International) +61 3 9757 4486 E: [email protected] E: [email protected] W: quickstep.com.au W: thermofisher.com.au

SUPPORTING PARTNER Rheology Solutions Pty Ltd SUPPORTING PARTNER AND STUDENT PARTY SPONSOR The University of Queensland Rheology Solutions was established in April, 1998 as a specialist sales and service organisation dedicated to Our ambition is to make a transformational impact on the science of materials characterisation and are the our region, and the world. exclusive Australian distributors for Thermo Scientific, Optical Control Systems, Sofraser and Schleibinger At UQ, we are developing new manufacturing Gerate range of equipment and instrumentation. methods and materials that provide solutions to the manufacturing and materials sector in a global Rheology Solutions has an established contract testing economic context. service and applications laboratory, equipped with a Trent Leggatt BOOTH 15 comprehensive range of rheology instruments to meet T: +61 3346 9976 E: [email protected] Pat Griffin the requirements of materials characterisation testing. W: uq.edu.au T: +61 414 446 050 Seminars and application specific workshops are E: [email protected] regularly offered and are designed to meet the needs of W: rheologysolutions.com specific customer and industry applications. EXHIBITION 22

The exhibition will be located in the Exhibition Hall, Melbourne Convention and Exhibition Centre.

BOOTH ORGANISATION BOOTH ORGANISATION 1 Langzauner GmbH ARC Centre for Advanced Manufacturing 25 of Prefabricated Housing (CAMP.H), The 2 Fill Gesellschaft m.b.H. University of Melbourne

ARC Training Centre for Automated 26 Quickstep Holdings Limited 3 Manufacture of Advanced Composites (AMAC) 27 Boeing 4 University of Southern Queensland 28 Boeing 5 ICCM23 Belfast 6 PerkinElmer EXHIBITION FLOOR PLAN 7 Blink Technology Australia 8 CONE Technology

9 TA Instruments POSTER AREA 10 Swinburne University of Technology 11 Bruker Pty Ltd

12 DKSH Australia 8 28 9 10 13 Instron 7 27 12 11 14 MDPI 6 26 15 Rheology Solutions Pty Ltd 5 7 8 25 16 Thermo Fisher Scientific 4 10 9 24 17 Altair 3 23 18 Altair 17 18 19 MSC Software 2 22 19 20 1 21 20 University of Bristol 21 NETZSCH Australia Pty Ltd 22 Deakin University - Carbon Nexus

23 Atlas Innovations 24 Anton Paar Australia Pty. Ltd. ARC Centre for Advanced Manufacturing of Prefabricated Housing (ARC‐CAMPH) “Unlocking the potential growth of Australia’s prefabricated building industry through Research and Innovation”

Driven by industry, the ARC Training Centre for Advanced Manufacturing of Prefabricated Housing (CAMPH) is the centrepiece for collaborative, eco‐friendly, prefabricated housing and buildings research in Australia, striving to deliver breakthrough product and process innovations that will enable the Australian housing industry to compete on a global stage. The centre aims to unlock the potential growth of Australia’s prefabricated building industry by creating a co‐operative training system between industry and universities leading to local employment growth and increased exports of prefabricated products and services. The centre brings together a highly collaborative venture involving four universities and twelve industry partners. The four research programs being run in the centre are: 1. Innovation in design and enhancement of end‐user experience 2. Developing advanced building systems and assembly techniques 3. Creating novel materials and composite structures 4. Supply chain and financing models This initiative is a testament to the critical importance of this industry in Australia, and demonstrates the value that both industry and government place in collaborative, cross‐ disciplinary research. The centre will, in partnership with industry, prepare the next generation of industry professionals and researchers, and develop the materials, systems and design thinking that will transform the construction industry towards an advanced manufacturing future. Website: https://camph.eng.unimelb.edu.au/ Contact: Prof. Priyan Mendis (Centre Director), [email protected] Dr. Kasun Shanaka Baduge (Centre Manager), [email protected]

24 COMMITTEE LISTS 25

ICCM22 would like to thank our valued contributors; • Dr Michael Heitzmann, University of Queensland the ICCM Executive Council, the Local Organising • Professor Luke Henderson, Deakin University Committee and the International Organising • Dr Chris Howe, Boeing Research and Technology Committee. Australia • Professor Xiao Hu, University of Western Australia

• Dr Everson Kandare, RMIT University ICCM EXECUTIVE COUNCIL • Associate Professor Akbar Afaghi Khatibi, RMIT • Leif Asp, Sweden – President University • Woo-II Lee, Korea – Senior Vice President • Dr Nam Kim, University of Auckland • Matthew Jevons, Germany – Vice President, Region 1 • Associate Professor Krishnan Jayaraman, University • Jinsong Leng, China – Vice President, Region 2 of Auckland • Pascal Hubert, Canada – Vice President, Region 3 • Dr Mathew Joosten, Deakin University • Nobuo Takeda, Japan – Immediate Past President • Dr Raj Ladani, RMIT University • Christian Berggreen, Denmark – Member • Professor Alan Lau, Swinburne University of • Chiara Bisagni, The Netherlands – Member Technology • Laifei Cheng, China – Member • Professor Guoxing Lu, Swinburne University of • Carlos Cimini, Brazil – Member Technology • Martine Dube, Canada – Member • Dr Richard Lin, University of Auckland • Stephanie Feih, Singapore – Member • Associate Professor Jun Ma, University of South • Sayata Ghose, USA – Member Australia • Suong Hoa, Canada – Member • Dr Sardar Malek, University of Technology Sydney • Masaki Hojo, Japan – Member • Associate Professor Allan Manalo, University of • Hyonny Kim, USA – Member Southern Queensland • Stephan Lomov, Belgium – Member • Professor Priyan Mendis, University of Melbourne • Silvestre Pinho, UK – Member • Professor Evgeny Morozov, University of New South • Paul Smith, UK – Member Wales (ADFA) • Ole Thomsen, UK – Member • Dr Minoo Naebe, Deakin University • Anoush Poursartip, Canada – Member • Professor Tran Ngo, University of Melbourne • Murray Scott, Australia – Member • Dr Kate Nguyen, RMIT University • Michael Wisnom, UK – Member • Associate Professor Adrian Orifici, RMIT University • Stephen Tsai, USA – Member • Dr Garth Pearce, University of New South Wales • Associate Professor Ganga Prusty, University of New South Wales LOCAL ORGANISING COMMITTEE • Professor Peter Schubel, University of Southern • Dr Mark Battley, University of Auckland Queensland • Professor Andrew Chan, University of Tasmania • Dr Nisa Silam, RMIT University • Dr Venkata Chevali, University of Southern • Dr Nigel StJohn, Defence Science & Technology Group Queensland • Professor Murray Scott, ACS Australia • Professor Wing Kong Chiu, Monash University • Professor Liyong Tong, University of Sydney • Associate Professor Paul Compston, Australian • Dr Jonathan Tran, RMIT University National University • Professor Russell Varley, Deakin University • Dr Claudia Creighton, Deakin University • Associate Professor Hao Wang, University of • Dr Ali Daliri, RMIT University Southern Queensland • Associate Professor Raj Das, RMIT University • Dr Shuying Wu, Macquarie University • Dr Jayantha Epaarachchi, University of Southern • Professor Yang Xiang, University of Western Sydney Queensland • Professor Lin Ye, University of Sydney • Dan Eyckens, Deakin University • Professor Tao Yu, University of Wollongong • Dr Joel Galos, RMIT University • Dr Xuesen Zeng, University of Southern Queensland • Professor Michelle Gee, RMIT University • Dr Jin Zhang, Deakin University • Associate Professor Rebecca Gravina, RMIT University • Dr Nishar Hameed, Swinburne University of Technology INTERNATIONAL ORGANISING COMMITTEE 26 • Prof Suresh Advani, University of Delaware, USA • Prof Daniel J Inman, University of Michigan, USA

COMMITTEE LISTS COMMITTEE • Prof Malin Akermo, KTH Royal Institute of • Prof Thomas Keller, Ecole Polytechnique Fédérale de Technology, Sweden Lausanne, Switzerland • Prof Leif Asp, Chalmers University, Sweden • Prof Jang Kuo Kim, Hong Kong University of Science • Prof Janice Barton, University of Southampton, UK and Technology, Hong Kong • Dr Jeffrey W Baur, Air Force Research Laboratory, US • Prof Tony Kinloch, Imperial College, UK • Prof Christian Berggreen, TU Denmark, Denmark • Prof Woo-II Lee, Seoul National University, Republic of Korea • Prof Lars Berglund, KTH Royal Institute of Technology, Sweden • Prof Josef Jančář, CEITECH, Czech Republic • Prof Debes Bhattacharyya, Auckland University, New • Prof Jinsong Leng, Harbin Institute of Technology, Zealand China • Prof Simon Bickerton, Auckland University, New • Prof Xioling Liu, University of Nottingham, Nigbo, Zealand China • Prof Chiara Bisagni, TU Delft, Netherlands • Prof Staffan Lundstrom, Lulea University of Technology, Sweden • Prof Alexander Bismarck, Imperial College/University of Vienna, UK/Austria • Prof Yiu-Wing Mai, University of Sydney, Australia • Prof Brina Blinzler, Chalmers University of • Prof Roberta Massabo, Universita degli Studi di Technology, Sweden Genova, Italy • Prof Ian Bond, Bristol University, UK • Prof Manjusri Misra, University of Guelph, Canada • Prof Pedro Camanho, Universidade do Porto, • Prof Ozden Ochoa, Texas A&M, USA Portugal • Dr Soraia Pimenta, Imperial College London, UK • Prof Wesley Cantwell, Khalifa University, UAE • Prof Silvestre Pinho, Imperial College, UK • Prof Miroslav Cerny, Czech Technical University, • Prof Anoush Poursartip, University of British Czech Republic Columbia, Canada • Prof Wojciech Ciesielski, Jan Dlugosz University, • Prof H Jerry Qi, Georgia Institute of Technology, USA Poland • Prof Abbasli Saboktakin, University of Sistan & • Prof Tsu-Wei Chou, University of Delaware, USA Baluchestan, Iran • Prof Carlos Cimini, Federal University of Minas • Prof Karl Schulte, Technische Universität Hamburg- Gerais, Brasil Harburg (TUHH), Germany • Dr Peter Davies, IFREMER, France • Prof Paul Smith, University of Surrey, UK • Prof Martine Dube, ETS Montreal, Canada • Prof Coutis Soutis, University of Manchester, UK • Prof Martin L Dunn, University of Colorado, USA • Prof Ole Thomsen, University of Southampton, UK • Prof Brian Falzon, Queens University, Northern • Prof Ignass Verpoest, Catholic University Leuven, Ireland Belgium • Dr Stefanie Feih, SIMTech, Singapore • Prof Anthony Waas, University of Washington, USA • Dr Sayata Ghose, Boeing, USA • Prof Michael Wisnom, Bristol University, UK • Prof Larissa Gorbatikh, KU Leuven, Belgium • Prof Zhong Zhang, National Center for Nanoscience • Prof Emile S Greenhalgh, Imperial College London, and Technology, China UK • Prof Soung Hoa, Concordia University, Canada • Prof Pascal Hubert, McGill University, Canada Advanced Composite Manufacturing Solutions

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For further information go to www.quickstep.com.au 28

SCIENTIFIC PROGRAM SCIENTIFIC PROGRAM CODES 29

The guide below shows you how to find sessions/presentations using session numbers/program numbers.

Please note that you can also search for presentations using the ICCM22 conference app.

ORAL PRESENTATION SESSIONS In the printed program, the names of the concurrent rooms are listed below and their location can be found The session number is made up of 4 digits: XYZZ in the venue map of this program book. X = day (Monday = 1, Tuesday = 2) Session room number Convention Centre room number Y = session number on the day 01 Plenary hall 2 ZZ = room code 02 Meeting room 205 03 Meeting room 206 The program number of oral presentations is made up 04 Meeting room 208 of the session number and the order of the presentation 05 Meeting room 209 in each session. 06 Meeting room 210 XYZZ-VV 07 Meeting room 211 X = day (Monday = 1, Tuesday = 2) 08 Meeting room 212 09 Meeting room 213 Y = session number on the day 10 Meeting room 214 ZZ = room code 11 Meeting room 215 VV = presentation order in the session 12 Meeting room 216 13 Meeting room 217 14 Meeting room 218 15 Meeting room 219 MINI ORAL PRESENTATION AND POSTER PRESENTATION SESSIONS The poster session number is made up of 5 digits: PROGRAM COLOUR CODE PXYZZ

P = poster MONDAY 12 AUGUST X = day (Monday = 1, Tuesday = 2) TUESDAY 13 AUGUST Y = session number on the day WEDNESDAY 14 AUGUST ZZ = room code for presentation THURSDAY 15 AUGUST The program number for the mini oral presentations are made up as follows: PXYZZ-VV FRIDAY 16 AUGUST P = poster

X = day (Monday = 1, Tuesday = 2)

Y = session number on the day

ZZ = room code for presentation

VV = presentation order in the session 30

SCALA AND PLENARY LECTURES SCALA AND PLENARY LECTURES 31

The Scala lecture and all plenary lectures will be held in Plenary 2, Melbourne Convention and Exhibition Centre. MONDAY 12 AUGUST Time Title Presenter Affiliation 0900-0945 SCALA Lecture: ADVANCED COMPOSITES RESEARCH AND INNOVATION - AN AUSTRALIAN PERSPECTIVE Murray Scott Advanced Composite Structures Australia, Australia 0945-1030 NEW STRATEGIES FOR MANUFACTURING MULTIFUNCTIONAL COMPOSITES Nancy Sottos University of Illinois, USA 1400-1445 LIGHTWEIGHT CARBON FIBRE COMPOSITE AUTOMOTIVE WHEELS - FROM CONCEPT TO INDUSTRIALISATION Jake Dingle Carbon Revolution, Australia

TUESDAY 13 AUGUST Time Title Presenter Affiliation 0805-0850 THE STORY OF BIOBASED NANOMATERIALS AND THEIR USE IN COMPOSITE MATERIALS Kristiina Oksman Lulea University of Technology 1350-1435 SHAPE MEMORY POLYMER COMPOSITES AND 4D PRINTING TECHNOLOGIES: FROM THE AEROSPACE TO Jinsong Leng Harbin Institute of BIOMEDICAL APPLICATIONS Technology

WEDNESDAY 14 AUGUST Time Title Presenter Affiliation 0805-0850 FUTURE CHALLENGES FOR CARBON FIBRE COMPOSITES: A JOURNEY THROUGH THE VALUE CHAIN Bronwyn Fox Swinburne University, Australia 1345-1430 COMPOSITES 4.0: FROM DESIGN TO AUTOMATED MANUFACTURING Peter Middendorf University of Stuttgart, Germany

THURSDAY 15 AUGUST Time Title Presenter Affiliation 0805-0850 TRENDS IN AEROSPACE COMPOSITES Jerry Young Boeing, USA

1420-1505 DESIGN, MANUFACTURE AND PERFORMANCE OF TEXTILE COMPOSITES Andrew Long Nottingham University, UK

FRIDAY 16 AUGUST Time Title Presenter Affiliation 0805-0850 CHALLENGES IN COMPOSITES FOR MARINE STRUCTURES Yapa Rajapakse United States Office of Naval Research, USA 32

KEYNOTE LECTURES KEYNOTE LECTURES 33

MONDAY 12 AUGUST Time Title Presenter Affiliation Room 1100-1130 STRONTIUM TITANIUM OXIDE-GRAPHENE NANOCOMPOSITE THERMOELECTICS Ian Kinloch University of Plenary 2 Manchester 1100-1130 MULTIFUNCTIONAL ENERGY STORAGE COMPOSITE (MESC) STRUCTURES Fu-Kuo Chang Stanford University Meeting room 210

1100-1130 FATIGUE LIFE OF POST-BUCKLED COMPOSITE STRUCTURES Chiara Bisagni TU Delft Meeting room 211

1100-1130 ENHANCING LIGHTWEIGHTING: JOINING COMPOSITES WITH 3D PRINTED STRUCTURES Stefanie Feih A-Star Meeting room 212

1100-1130 FILLING THE PROPERTY GAP OF MULTI- PHASE COMPOSITES THROUGH ARCHITECTURAL DESIGN Hua-Xin Peng ZheJiang University Meeting room 213

1100-1130 3D PRINTABLE SHAPE MEMORY POLYMER COMPOSITES Zhang Zhong National Center for Meeting room 219 Nanoscience and Technology

TUESDAY 13 AUGUST Time Title Presenter Affiliation Room 0900-0930 NANOCOMPOSITES AND HIERARCHICAL NANOENGINEERED ADVANCED COMPOSITES FOR Brian Wardle MIT Plenary 2 ENHANCED MECHANICAL AND MULTIFUNCTIONAL PERFORMANCE 0900-0930 SELF-HEALING FIBRE REINFORCED POLYMER COMPOSITES – A BRISTOL PERSPECTIVE Ian Bond University of Bristol Meeting room 210

0900-0930 VIRTUAL DESIGN OF HIGH-PERFORMANCE DISCONTINUOUS-COMPOSITE STRUCTURES Soraia Pimenta Imperial College Meeting room 211

0900-0930 POLYMER NANOCOMPOSITES UNDERFILL MATERIALS FOR ELECTRONIC PACKAGING Yiu-Wing Mai University of Meeting room 212 Sydney 0900-0930 OPPORTUNITIES AND CHALLENGES FOR COMPOSITES IN NEXT GENERATION MULTI-MATERIAL Patrick Blanchard Ford Meeting room 213 VEHICLES 0900-0930 ACCELERATED TESTING METHOD FOR DURABILITY OF CFRP Yasushi Miyano Kanazawa Institute Meeting room 219 of Technology

WEDNESDAY 14 AUGUST Time Title Presenter Affiliation Room 0900-0930 MECHANICAL PROPERTIES AND FRACTURE RESISTANCE OF THREE-DIMENSIONAL GRAPHENE/ Jang-Kyo Kim University Science Plenary 2 POLYMER COMPOSITES & Technology 0900-0930 MODELING OF IMPACT DAMAGE AND COMPRESSION AFTER IMPACT OF LAMINATED COMPOSITE Paul Davidson Michigan University Meeting room 211 AEROSPACE STRUCTURES 0900-0930 INTERFACIAL DAMAGE IN FIBRE REINFORCED COMPOSITES MODELLED IN THE FRAMEWORK OF Stepan Lomov KU Leuven Meeting room 212 FINITE ELEMENTS WITH EMBEDDED REGIONS 0900-0930 CHARACTERISATION AND MODELLING OF STRUCTURAL BATTERY COMPOSITES Lief Asp Chalmers University Meeting room 213

0900-0930 AN INTEGRATED APPROACH TO DESIGN AND MONITOR COMPOSITE STRUCTURES UNDER IN- Marino Quaresimin Universita degi Meeting room 219 SERVICE FATIGUE LOADINGS Studi di Padova

THURSDAY 15 AUGUST Time Title Presenter Affiliation Room 1100-1130 DYNAMIC INSTABILITY OF ANISOTROPIC CYLINDERS IN CONFINING ENVIRONMENTS Arun Shukla University of Rhode Plenary 2 Island 1100-1130 THERE IS NO SUCH THING AS A COMPOSITE MATERIAL – ONLY COMPOSITES OF MATERIALS John Hart-Smith Boeing (retired) Meeting room 211

1100-1130 INTEGRATING IMAGING TECHNIQUES FOR ASSESSING THE PERFORMANCE OF LARGE Janice Barton University of Meeting room 213 COMPOSITES STRUCTURES Southhampton 1100-1130 REVEALING THE MOLECULAR-SCALE ROLE OF CARBON FIBRE FUNCTIONALISATION IN POLYMER Tiffany Walsh Deakin University Meeting room 219 COMPOSITES

FRIDAY 16 AUGUST Time Title Presenter Affiliation Room 0900-0930 AMELOGENESIS: NATURE’S 3D PRINTING SYSTEM FOR MULTI-SCALE LAMINATES Brian Cox Plenary 2

0900-0930 MANUFACTURING RELATED DEFECTS –WHERE AND WHY THEY OCCUR, AND DO THEY MATTER? Simon Bickerton Auckland University Meeting room 212

0900-0930 RESIN INFUSION COMPOSITES FOR AEROSPACE Michael Edwards Boeing Australia Meeting room 213

0900-0930 MULTI-SCALE MODELING OF FIBER-REINFORCED PLASTIC COMPOSITES: FROM ATOMISTIC Tomonaga Okabe Tohoku University Meeting room 219 MODELING TO STRUCTURAL DESIGN 34 SCIENTIFIC PROGRAM MONDAY 12AUGUST 1100-1300 1030-1100 0945-1030 Time 1200-1220 1140-1200 1130-1140 0900-0945 0830-0900 1100-1130 Nano-composites 1101 hall Exhibition break Coffee 2 Plenary properties. and enhancement of leading to control is demonstrated and microstructure control orientation of strengths.fields The low (<100mT) very using composites are actuated inepoxy Graphene flakes Oxide. decoration with Iron grapheneof via the magnetisation This investigates paper University Mark Eaton NANOCOMPOSITES EPOXY IN GRAPHENE MICROSTRUCTURE OF CONTROL MAGNETIC 1101-2 Bhd Research Sdn Aba Norfarah PAINTOFFSHORE SERVICE LIFE OF IMPROVING PROTECTION; CORROSION FOR MATERIALBARRIER NOVEL GRAPHENE: 1101-1 2: KEYNOTE 1: KEYNOTE STRATEGIES NEW MANUFACTURING FOR MULTIFUNCTIONAL LECTURE: PLENARY COMPOSITES 2 Plenary ADVANCED Lecture: SCALA AND INNOVATION RESEARCH COMPOSITES -AN AUSTRALIAN PERSPECTIVE 2 Plenary 3: KEYNOTE KEYNOTE 6: KEYNOTE 5: KEYNOTE KEYNOTE 4: KEYNOTE Move to concurrent sessions Opening ceremonyOpening

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MULTIFUNCTIONAL ENERGY STORAGE COMPOSITE (MESC) STRUCTURES STRONTIUM TITANIUMSTRONTIUM Manchester 2) of (Plenary OXIDE-GRAPHENE, University NANOCOMPOSITE THERMOELECTICSIan Kinloch FATIGUE LIFE OFPOST-BUCKLED COMPOSITE STRUCTURES 3D PRINTABLE SHAPE POLYMER MEMORY Zhang Zhong COMPOSITES OFMULTI-PHASE GAP FILLING THEPROPERTY DESIGN ARCHITECTURAL THROUGH COMPOSITES STRUCTURES WITH3DPRINTED JOININGCOMPOSITES ENHANCING LIGHTWEIGHTING:

future. inthe composites reinforced or glass fiber natural reinforced- fiber substitute to partially with high potential materialbio-based and high-performance promising lightweight, anew represents wood densified Delignified Marion Frey (DWRC) COMPOSITES REINFORCED DELIGNIFIED WOOD 1102-2 investigated. were sheets composite the of and formability composite) fabrics, yarn, (dry scale dry indifferent composites fabrics /polypropylene woven hempfibre of behaviour mechanical In this study, Technology Troyes of of University Antony,Sheedev COMPOSITE POLYPROPYLENE WOVEN FABRICS / HEMP FIBRE BEHAVIOUR OF AND FORMING MECHANICAL INVESTIGATE THE ANALYSIS TO MULTISCALE 1102-1 composites &naturalGreen fibre 1102 Meeting room 205

, Eth Zürich , Eth bonded joint. bonded adhesively composite for interface adhesive the adherend-of properties mechanics charactercould the which parameters, elasticity the interface to determine proposed is An inverse method Tong University Wei Xiao BONDED JOINT ADHESIVELY SINGLE-LAP COMPOSITE FOR INVERSE ANALYSIS 1103-2 estimated. are composite for the purposed properties effective is The proposed. fibers piezoelectric nanotubes (CNTs) and with carbon reinforced composite A hybrid smart Rajasthan,Kota, India Technical University Godara SS COMPOSITES HYBRID NANO OF PROPERTIES EFFECTIVE 1103-1 properties composite of Analysis 1103 Meeting room 206 , Shanghai Jiao , Rajasthan curved surfaces. curved layup onfreeform machine for (AFP) robotic placement fibre with an automated/ foruse optimization generation andits tool fortrajectory to provide asimple The attempts paper Technology andDesign of Singapore University Raspall Felix SURFACESCURVED ON PLACEMENT ROBOTIC FIBRE GENERATION FOR STRATEGY & TOOLPATH 1104-1 process parameters. process and material properties discussed, including panel were stiffened distribution hat- of geometric andfibre Factors influencing process. co-curing placementfibre and based onautomated was manufactured A hat-stiffened panel Astronautics and Aeronautics of University Zhao Cong PLACEMENT FIBRE WITH AUTOMATED PANELTIFFENED HAT-INTEGRAL OF CO-CURED MANUFACTURE 1104-2 placement Automated fibre 1104 Meeting room 208

Chiara Bisagni , Nanjing , Nanjing , , National Center for Nanoscience andTechnology, National forNanoscience Center room 219) (Meeting (Meeting room 211) (Meeting Delft , TU Fu-Kuo Chang Raman spectroscopy. using composite model glass fiber/epoxy strain sensors ina grown graphene as and continuous CVD graphene nanoplatelets discontinuous both of demonstrated the use This study has Manchester of The University Jingwen Chu COMPOSITES EPOXY MODEL IN FIBRE/ SENSORS STRAIN MATERIALS AS GRAPHENE-BASED 1105-1 the hybrids. of properties interfacial the and especially damage initiation strain moisture the reduced temperature and investigated. Both glass layers were continuous between discontinuous carbon continuous and configurations with Interlayer hybrid Economics Technologyof and Budapest University Czél Gergely COMPOSITES THIN-PLY HYBRID OF DUCTILITY ON THEPSEUDO- TEMPERATURETEST AND MOISTURE OF EFFECT THE COMBINED 1105-2 Hybrid composites 1105 Meeting room 209 Nancy Sottos , , (Meeting room 210) (Meeting , Stanford University Stefanie Feih Stefanie Murray Scott , University of Illinois, USA USA Illinois, of , University Universidade doMinho Universidade Raul Fangueiro ABSORPTION ENERGYFOR COMPOSITES THERMOPLASTIC AND THERMOSET NOVEL AUXETIC 1106-1 (LMAT) Limited (LMAT) Technologies Assembly Manufacturing & Tomasz Garstka ZONAL CURING OUT-OF-OVEN VIA COMPOSITES OUT-OF-AUTOCLAVE DEFORMATION OF CURE-DRIVEN ELIMINATING 1106-2 Composite structuresComposite 1106 Meeting room 210 , ZheJiang University (Meeting room 213) (Meeting Hua-Xin, ZheJiang University Peng (Meeting room 212) , A-Star(Meeting

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PP with 20 wt% kenaf.PP wt% with 20 parameters kenaf/ of to optimise different is (RSM) used method surface Response numerical simulation. investigated by PP composites kenaf/moulded parameter injection of The moulding Malaysia Kebangsaan Universiti Sulong Bakar Abu SIMULATION NUMERICAL PROCESS BY MOULDING IN INJECTION PP COMPOSITES MOULDED KENAF/ INJECTION FOR OF SINK MARKS MINIMIZATION 1107-1 Manchester of The University Julio Aguilar-Tadeo COMPOSITES BILAYER MORPHING TRIGGERED PHOTOTHERMAL DESIGN OF 1107-2 finite elementmethods finite and Computational 1107 Meeting room 211

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FIDAMC Saenz-Castillo Diego PROPERTIES AND MECHANICAL IMPACT ONNDT COMPOSITES: THERMOPLASTIC OF CF/PEEK CONTENT CRITICAL VOID 1108-2 Technology of University Delft Nijgh Martin LOADING STATIC AND CYCLIC UNDER RESIN STEEL-REINFORCED OFA PROPERTIES MECHANICAL 1108-1 materials Polymer matrix 1108 Meeting room 212

, , matrices. inepoxy and adhesion properties physical improvement their of andthe fibres carbon this has to led coloured andhow modification in surface efforts summarise ourrecent desired. This talkwill has longbeen fibers oncarbon colour The generation of University Deakin Luke Henderson PROPERTIES ADHESION PHYSICAL AND WITH ENHANCED CARBON FIBERS COLOURED 1109-2 (PPS_ImCl). sulfide polyphenylene imidazolium modified (PPS) and sulfide were polyphenylene matrices which different and two fibers carbon ex-PANbetween interphase built investigated the we In this work, Lyon University deLyon - -INSA Lab Baptiste Gaumond COMPOSITES IN PPS/CARBON STRENGTH SHEAR INTERFACIAL ENHANCED AGENT FOR INTERFACIALNEW 1109-1 interphases and Interfaces 1109 Meeting room 213

, , IMP were clarified. property the electric of dependence frequency The temperature and change. property the electric by plastics was measured reinforced fiber carbon The strain short of Institute Technology of Keisuke Iizuka PROPERTY USING ELECTRIC PLASTICS FIBER REINFORCED SHORT CARBON OF 3DPRINTED MEASUREMENT STRAIN 1110-2 Chester of University Xie PengHeng SENSORSPRINTED COMPOSITE WITH MULTIFUNCTIONAL 1110-1 sensing Sensing 1:embedded 1110 Meeting room 214

, Tokyo , London College Imperial Greenhalgh Emile SUPERCAPACITORS STRUCTURAL STRATEGIES FOR ADOPTION AND INDUSTRIAL CHALLENGES FUTURE 1111-2 composites and their fibres activated carbon electrochemically using possibilities multifunctional these the present status of of anoverview give The presentation will Institute Technology of Zenkert Dan HARVESTING AND ENERGY ACTUATORS SENSORS, BATTERIES, AS COMPOSITES CARBON FIBRE 1111-1 and modelling design multifunctional Structural power 1: 1111 Meeting room 215

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measurements. fast andsimple a strong focus on historical data, with measurements or forreference need the without textiles semi-finished of assessment a quality provide based methods The presented airflow- Auckland of University HermannTino TEXTILES SEMI-FINISHED FOR ASSESSMENT QUALITY NON-DESTRUCTIVE 1112-2 components. large aerospace and for complex which is important mode, in reflection used and mostly defects in locating highaccuracy defects, formost sensitivity ahigh provides Thermography inindustry.applied measurement is being thermography and more automated surely,Slowly but more (DLR) Center Aerospace German Christoph Frommel MODEL TOMOGRAPHY ON 3DTHERMO- BASED COMPONENT AEROSPACELARGE EVALUATION OF 1112-1 evaluation Non-destructive 1112 Meeting room 216

, The , The , Queensland Southern of University Khotbehsara Mehrinejad Mojdeh MATERIALS COMPOSITE FOR FILLERS FIRE RETARDANT WITH FLY ASH AND POLYMER COATING EPOXY-BASED RESISTANCE OF TEMPERATURE 1113-2 University Cranfield Ghasemnejad Hessam SANDWICH PLATES OF CURVED IMPACT RESPONSE ON STIFFNESS VARIABLE CORE OF EFFECT 1113-1 route to impact materials: Composite 1113 Meeting room 217

, , mechanical loading.mechanical elevated pressure and inwater,immersion environment of to an exposed when specimens composite of ageing the accelerated use of This work investigates Surrey of University Materials / / Element Laboratory Physical Jasmine Bone COMPOSITES OF POLYMER PROPERTIES AND CHEMICAL ON MECHANICAL ABSORPTION MOISTURE AGEING AND ACCELERATED OF EFFECT 1114-2 microscope. electron scanning and measurement, strain optical emission, with the acoustic use of region the interfacial in particularly CFRP weaveweave, andtwill plain unidirectional, water on exposure of the influence This study presents University Cardiff Faisel Almudaihesh CFRP AND 2D WOVEN UNIDIRECTIONAL MECHANISM OF ON THEDAMAGE WATER ABSORPTION THE INFLUENCE OF 1114-1 environment and aggressive Durability, creep 1114 Meeting room 218

, National , stainless-steel. coating onthe asilane by improved were welded joints of performances Mechanical matrix. with the PPS affinity which have low heating element a stainless-steel with performed is composites thermoplasticof welding Resistance supérieure detechnologie École Vincent Rohart ELEMENT STEEL HEATING ON THESTAINLESS- SOL-GEL COATING USING ASILANE COMPOSITE JOINTS THERMOPLASTIC WELDED RESISTANCE- STRENGTH OF SHEAR THE LAP IMPROVEMENT OF 1115-2 ENSTA Bretagne 6027, UMR CNRS Johnatan Leplat ADHESIVE BONDING PROPAGATION IN CRACK INTERFACIAL ON THE 1115-1 Joints 1115 Meeting room 219

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Meeting room 219 room Meeting 1215 Joints 1115-4 1115-4 EFFECTS OF RESISTANCE ELEMENT HEATING ON JOINING OF CF/ STRENGTH COMPOSITES PPS Tamura Kota University focuses study This heatingon resistance elements and aims reveal bonding the to of CFRTP the behavior by welding resistance method carbon using fiber element. heating 1115-3 1115-3 LASER BASED PRETREATMENT OF ALUMIUM FORCASTINGS INJECTION HYBRID MOLDING Steinberg Julian Universität Technische - Institute Braunschweig of Joining and Welding For reducing vehicles weight, paper this presents a promissing using approach injection hybrid the molding process join to cast pretreated laser partsaluminum with polyamid 6. 1215-1 SPOT ULTRASONIC BEHAVIOR WELDING OF WOVEN-CF/PPS USING LAMINATES ENERGY CF/PPS DIRECTOR Horiuchi Tokiyuki of Institute National Wakayama Technology, College to aims study This development the welding spot ultrasonic process of CFRTP flat using energy director and carbon fiber energy reinforced director. , , ,

Meeting room 218 room Meeting 1214 award Tsai presentations 1114-4 ASSESSMENT OF A TEMPERATURE LOW CURE RESIN FOR HIGH TEMPERATURE COMPOSITE OVERWRAP REPAIRS Chech Tan Yee PETRONAS Research 1114-3 EFFECTMICROBIAL ON THE DURABILITY OF WOVEN CARBON/VINYL ESTER COMPOSITES Alejandra Castellanos University of Wisconsin- madison 1214-1 INVESTIGATION OF THE HYBRID EFFECT IN HIGH PERFORMANCE QUASI-ISOTROPIC THIN-PLY CARBON/GLASS COMPOSITES UNDER TENSION Guillermo Idarraga UniversityNational of Colombia Stiffness theof and layers adjacent stacking sequencethe an importantplay role of strain failure in the carbonthe plies and hybrid in the therefore effect. , , , University of

Meeting room 217 room Meeting 1213 Recycling and sustainability 1113-3 BEHAVIOR IMPACT OF SANDWICH STRUCTURES ONBASED CORRUGATED CORESCOMPOSITE WITH PVCFILLED FOAM Jin Zhou Liverpool impactThe response of base sandwiches core on corrugation filling PVC with foam been investigated have experimentally and numerically. configuration The optimization of the sandwicheshybrid base studied was on thickness of cores and corrugation density of filled foam. 1113-4 INTERLAMINAR SHEAR PROPERTIES OF TOUGHENED FIBRE CARBON REINFORCED COMPOSITES Andreas Klingler for CompositeInstitute (IVWMaterials Gmbh) of Toughening thermoset based CFRP by core-shell rubber and block-copolymer a to leads hybrids improved drastically mode II, shear performance. Hence, damage increasing propertiesthreshold be expected. to are 1213-1 INVESTIGATION OF THE PROCESS OF RESISTANCE FIBRE SURFACE FOR TREATMENTS THERMOPLASTIC COMPOSITES USING CARBON RECYCLED FIBRE Froemder Christina Carbon Fibre ELG international The andresearch betweencollaboration universities and a novelindustry shows and offers forward step view ina tentative combining and gentle quick electrochemical on recycledtreatments carbon fibres. , , , LANL

Meeting room 216 room Meeting 1212 Non-destructive evaluation 1112-3 ULTRASONIC INSPECTION OF HYBRID COMPOSITES BONDEDAND JOINTSCOMPOSITE Ibrahim Matthew Defence Science and Technology 1112-4 / MATCH PAGOSA OFMODELING HIGH EXPLOSIVE LOW TO RESPONSES SPPED INSULTS Xia Ma 1212-1 1212-1 ON THE INTERACTION BETWEEN NONLINEAR WAVES SOLITARY LAMINATED AND BEAMS COMPOSITE Andreas Schiffer Khalifa University Experiments and calculations numerical performedare study to between interaction the nonlinear solitary in granular waves and laminated chains composite beams. , ,

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Meeting room 215 room Meeting 1211 2: power Structural multifunctional constituents 1111-3 MODELLING OF DESIGN AND STRUCUTRAL WITH BATTERIES CYCLE LIFE ASSESSMENT Wilhelm Johannisson KTH of Institute Royal Technology analyticalA bottom-up modelling of a battery’sstructural ability system save to mass. Investing mechanical properties, electrochemical properties, and a life cycle assessment. 1111-4 STRUCTURAL POWER PERFORMANCE REQUIREMENTS FOR FUTURE AIRCRAFT INTEGRATION Sang Nguyen College London paper investigates This of application the in power structural cabins by aircraft floor integrating panels sheets face with ofmade structural compositespower in-flight the power to entertainment system. 1211-1 FEASIBLE MANUFACTURING ANDTECHNIQUE MECHANICAL PROPERTIES OF STRUCTURAL BATTERY ELECTRODES Maria Schneider Lynn of Institute Kth Royal Technology A feasible processmanufacturing for multifunctional batteries structural The presented. is evaluated is technique respectwith the to multifunctional performance of the and of material matrix a negative structural electrode. , The - , The , Queen

Meeting room 214 room Meeting 1210 health Structural monitoring 1110-3 MULTIFUNCTIONAL FIBRE REINFORCED COMPOSITES: FROM SMART OUT-OF-OVEN MANUFACTURING INTEGRATED TO DE- AND SENSING CAPABILITIES ICING Zhang Han Mary University of London An extremely efficientenergy and safe intrinsically method manufacture to thermoset based integrated with FRPs multifunctionalities been developed.has embeddedThe nanocomposite layer can be used from out-of-oven to curing sensing strain/damage and de-icing. 1110-4 GRAPHENE OXIDE/GRAPHITE NANOSHEETS COMPOSITE FORTHIN FILMS WEARABLE STRAIN SENSORS Qingbin Zheng Hong Kong University of Science and Technology utilize graphene the We oxide and graphite nanosheets composite sensing filmsthin as fabricate to materials high-performance via sensors strain a simple, cost- effective and solution processable strategy. 1210-1 A NANOCOM POSITES-BASED, ALL-INKJET- FLEXIBLE,PRINTED, ULTRA-BROADBAND FOR SENSOR FILM IN-SITU OF ACQUISITION STRAIN DYNAMIC Pengyu Zhou Hong Kong Polytechnic University All inkjet-printed nanocomposite for structural sensors are health monitoring developed and the of are sensors printed advantages ofthe high sensitivity and fidelity, broadband as well as frequencysensing up 500 kHz.to , , Super

Meeting room 213 room Meeting 1209 Interfaces and interphases 1109-3 DIRECT MEASUREMENT OF INTERFACIAL SHEAR STRENGTH OF MWCNT/NBR NANOCOMPOSITE Hsu Chun-yen C Inc 1209-1 1209-1 COMPARISON OF DIFFERENT INTERFACIAL ENGINEERING METHODS ACHIEVE TO PSEUDO-DUCTILE OF BEHAVIOUR FIBER CARBON REINFORCED POLYMER COMPOSITES Balázs Magyar UniversityBudapest and of Technology Economics , Beihang , University , TUDortmund

Meeting room 212 room Meeting 1208 compositesHybrid 1108-3 INFLUENCE OF MOISTURE GRADIENTS ON THE BENDING PROPERTIES OF GLASSSHORT REINFORCEDFIBER 6 POLYAMIDE Anna Katharina Sambale University contribution This the investigates influence of moisture on the gradients bending properties of short-glass-fiber- reinforced polyamide integral constant 6 at using content moisture three-point bending test 1108-4 MANUFACTURING ANDPROCESS PROPERTIES OF FIBER CARBON REINFORCED PEEK COMPOSITES WITHMODEFIED MWNTS Jiupeng Song University work, this In carbon etherfiber/poly(ether (CF/PEEK)ketone) composites were by wet the prepared impregnation. powder were powders PEEK mixed different with of multi-walled content carbon nanotubes in water (MWCNTs) homogeneously. 1208-1 COMPRESSIVE OF FAILURE CFRP- HYBRID LAMINATED CFRP COMPOSITES Mark Battley of Auckland effectThe of of HMhybridisation and UHM carbon fibre on strength laminates and stiffness under compression was through investigated physical and testing analysis.

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Meeting room 211 room Meeting 1207 Langzauner GmbH industry session Changwon National National Changwon University it was study, this In developed the that analytical model of CFRP-to-CFRP by using structure cohesive zone modeling (CZM) method, which containing fiber-metal laminates. 1107-3 UNDERSTANDING INITIATION FAILURE IN LOCATIONS STOCHASTIC VIRTUAL COMPOSITE A USING SPECIMENS LEARNING MACHINE FRAMEWORK Kumar Nimal Balasubramani University of New South Wales 1107-4 FINITE ELEMENT OF ANALYSIS CFRP-TO-CFRP JOINT STRUCTURE FIBER- CONTAINING LAMINATES METAL Dong-woo Lee Langzauner GmbH industry session only *invitation event* CHALLENGES IN INDIVIDUAL AUTOMATION FORSOLUTIONS INCREASING PRODUCTION IN EFFICIENCY AVIATION Hauer Bernhard by Sponsored -

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Meeting room 210 room Meeting 1206 Composite structures 1106-3 FRACTURE MECHANICS-IN FORMED MULTI THERMO SCALE MECHANICAL MODEL DAMAGE FOR MA CERAMIC TRIX COMPOSITES Skinner Travis UniversityState 1106-4 CONTROLCRACK FOR BIO-INSPIRED TOUGHENING OF COMPOSITE AND MATERIALS STRUCTURES Adrian Orifici University 1206-1 THE INFLUENCE OF GEOMETRIC IMPERFECTIONS OF DIFFERENT TOLERANCE LEVELS ON THE LOAD BUCKLING OF UNSTIFFENED CYLINDRICAL CFRP SHELLS Hartwich Tobias UniversityHamburg of Technology Unstiffened CFRP cylindrical under shells axial compression buckle. One to prone of most the influencing buckling on the factor geometricload are imperfections which analysedare in this contribution. , , The , German

Meeting room 209 room Meeting 1205 fibre Automated placement 1105-3 OF INFLUENCE ALUMINIUM SURFACE ON TREATMENT BOND QUALITY IN ALUMINIUM/ GLASS/EPOXY FIBRE METAL LAMINATES Dunn Mitch University of Queensland compositeHybrid combining structures aluminium alloy are and glass/epoxy a with considered, the on how focus surface preparation of aluminium the influences bond quality. 1105-4 OF THE INFLUENCE RATE COOLING ON THE ADHESIVE PROPERTIES OF POLYAMID-6- GALVANIZED-STEEL IN THE HYBRIDS FORMINGONE-STEP PROCESS Fischer Tobias UniversityClausthal of Technology work of focus this The production the in ais one-step variothermal pressing process and contextin this the influence of cooling the bonding on the rate quality of mono- the materials. 1205-1 1205-1 XENON FLASH- LAMP IN- BASED SITU AUTOMATED PLACEMENTFIBER OF THERMOPLASTIC COMPOSITES Lars Brandt Aerospace Center (dlr) An opportunity for flexible, cost-effective production of componentsaerospace of usage found in the is new systems heating pulsed the as such since flashlamp, xenon useit the renders of complete safety unnecessary. housing , UNSW Meeting room 208 room Meeting

Sydney A successful methodology been has study to implemented influencethe of fiber on crush architecture performance. is This important for designing AFP manufactured absorbingenergy as such structures helicopter aircraft and subfloors. 1104-3 INVESTIGATION ON THE CRUSH PERFORMANCE OF AUTOMATED FIBRE PLACEMENT MANUFACTURED TUBESCOMPOSITE David Matthew , Nihon

Meeting room 206 room Meeting 1203 fibre Green & natural composites 1103-3 1103-3 CONTINUUM DAMAGE MECHANICS OF MODELLING A 3D PRINTED CURVILINEAR CFRTP UedaMasahito University 1203-1 1203-1 OF IN INFLUENCE SITU DEPOSITING SIZE-CONTROLLED NANO-SIO2 ON PARTICLES THE MECHANICAL SURFACE AND PROPERTIES OF JUTE FIBERS LiXuan u, Institute of Science Materials and Technology, Nanjing University of Aeronautics and Astronautics enhance to order In mechanical andthe surface properties of jute fibers, the surface of jute fibers depositedwere size- nano-SiO2controlled particles sol-gel via technique. , ,

Meeting room 205 room Meeting 1202 Processing & properties of composites 1102-3 1102-3 OF ENHANCEMENT MITIGATION NOISE FIBRE OF NATURAL COMPOSITES WITH PERFORATION Heow Pueh Lee UniversityNational of Singapore fiber based Natural composites are finding increasing in productsuse like parts interior the of automotives, electronics casings, reinforcementsas building andin the industry. construction Micro-perforated are (MPPs) plates sound new-generation absorbers and they commonlyare used absorption noise as panels. 1202-1 1202-1 BEHAVIOR THERMAL IN OF TAPES TAPE AUTOMATED PLACEMENT (ATP) PROCESS-MICRO ANALYSIS Ketaki Mishra Universite De Nantes model A numerical is analyze to presented of behavior thermal the tapesthe microscale at automated during tape placement process. A 3D (ATP) geometrical model is developed considering microstructure. real the

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Lunch Exhibition hall Sarah McSwineySarah Plenary 2 Emilie Storms Meeting 218 room Stuart Bateman modeling ? of material future the is Engineering, e-Xstream What Solution from Material - 10x roundtables Industry Software MSC only event**invitation Soumik Chakrabarty Boeing lunch symposium - University and industry collaboration, focus on composite material development development on composite material focus Boeing lunch symposium and industry - University collaboration, only event**invitation Michael Edwards Fox Bronwyn 1101-4 GRAPHENE JANUS NON-WOVEN FOR FABRICS ULTRALIGHT ELECTROMAGNETIC INTERFERENCE SHIELDING Ying Wu of Science and Beijing Technology Plenary 2 Research 1101-3 GRAPHENE- ENHANCED PAINTS COMPOSITE FOR CORROSION OF PROTECTION OFFSHORE RISERS Farid Mohd Shamsul Samsudin 1201-1 MANAGEMENT LIFE OF ADHESIVELY BONDED COMPOSITE STRUCTURES Li Lucy CouncilResearch Canada Jake Dingle Jake PLENARY LECTURE: INDUSTRIALISATION WHEELS - FROM CONCEPT TO LIGHTWEIGHT AUTOMOTIVE FIBRE COMPOSITE CARBON Plenary 2 sessions concurrent to Move 1201 Aerospace 1220-1240 1500-1520 1300-1400 1300-1400 1240-1300 1310-1355 1400-1445 Time 1445-1500 1500-1600 MONDAY 12 AUGUST 12 MONDAY

SCIENTIFIC PROGRAM 36 SCIENTIFIC PROGRAM SCIENTIFIC 39 , , Institut , Institut , Hefei

1315 Joints Meeting room 219 room Meeting 1215-3 INTERLAMINAR FRACTURE OF CO-TOUGHNESS CF/ CONSOLIDATED LAMINATES PEEK MANUFACTURED IN STMAP-JOINING PROCESS Weber Julian Verbundwerkstoffe Für Gmbh 1315-1 OFSTUDY ENVIRONMENTAL EFFECTS ON THE COMPOSITE-TO- LAP DOUBLE METAL SHEAR JOINTS Qian Zhang University of Technology 1215-2 INVESTIGATIONS ON THERMALLY INDUCED IN DELAMINATION MECHANICALLY CARBON JOINED COMPOSITES FIBER Vorderbrüggen Julian University of Paderborn inducedThermally indamages mechanically joined CFRP metal joints heatoccur during according to treatment automitive dip coating. areThose damages andbeing investigated minimized by suitable in countermeasures presentation. this

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1314 award Tsai presentations Meeting room 218 room Meeting 1214-3 MULTISCALE COMPUTATIONAL FORMODEL MATRIX POLYMER COMPOSITES UNDER IMPACT LOADING, INCLUDING HE ADIABATIC EFFECTS ATING SoriniChristopher Arizona State University; Nasa A multiscale computational to taken is approach effects the investigate adiabatic of local matrix ballistic on the heating impact of response 862 a T700/Epon triaxially [0°/60°/–60°] composite.braided 1314-1 TOUGHENING SYNTACTIC EPOXY FOAMS WITH CARBON MILLED FIBRES: MECHANICAL PROPERTIES AND TOUGHENING MECHANISMS He Sammy College London 1214-2 1214-2 PROCESS- FAILURE INDUCED IN OF DELTOID COMPOSITE FIBER- T-JOINT: OPTICBASED MONITORING NUMERICAL AND SIMULATION Hisada Shinsaku University of Tokyo , , Tampere , Tampere , University of

1313 Recycling and sustainability Meeting room 217 room Meeting 1313-1 IMPORTANCE OF CHEMICAL PRETREATMENT FOR FIBRE CARBON FROM RECYCLED BY COMPOSITE PYROLYSIS Siqi Hao NingboNottingham China 1213-2 ON THE RESIZING OF RECYCLED FIBRES Essi Sarlin University 1213-3 RESIN TRANSFER – APRESSING PROCESS NOVEL FOR LARGE SCALE COMPOSITE MANUFACTURING Christian Goergen für Institut Verbundwerkstoffe Gmbh A new process is calledintroduced, „Resin Transfer (RTP).Pressing“ RTP exploits specific advantages of recycled in fabrics nonwoven a thermoset press process and provides short cycle times. , ,

1312 Non-destructive evaluation Meeting room 216 room Meeting 1312-1 3D CHARACTERISATION FIBRE OF CARBON REINFORCED COMPOSITE MICROSTRUCTURE VIA X-RAY COMPUTED TOMOGRAPHY Silvano Sommacal National The Australian University State-of-art 3D X-ray computedmicro combined tomography, tomographic with volume analysis and tools, visualization has been utilized a study to of highlysuite different carbon fibre reinforced polymers. 1212-2 ASSESSMENT OF BONDADHESIVE QUALITY USING BY ULTRASONIC TESTING COMBINED WITH PATTERN RECOGNITION Jens Schuster University of Applied Sciences Kaiserslautern study aim ofThe this been develop to has recognition pattern to an approach as identify kissing bonds in adhesive joints by ofmeans ultrasonics. purpose,For this kissing bonds have be to been attempted in bymanufactured varying of a two- ratios part adhesive. , , , Imperial

1311 3: power Structural device assembly Meeting room 215 room Meeting Chalmers University of Technology Multiphysics modelling battery of structural composites is FE-models discussed. if study to setup are modelling techniques for conventional can bebatteries describe to used electrochemicalthe of thisbehaviour material. 1311-1 MANGANESE DIOXIDE DECORATED AEROGEL/ CARBON FIBRE CARBON ASCOMPOSITE A PROMISING ELECTRODE FOR STRUCTURAL SUPERCAPACITORS SenokosEvgeny Imperial College London dioxideManganese electrochemically deposited carbon onto fibres aerogel/carbon (CAG/CF) provides enhancement a large in capacitive performance of the carbon electrodes and potential a great show for multifunctional structural supercapacitors. 1211-2 THEPREDICTING CONSOLIDATION OF FABRIC- REINFORCED STRUCTURAL POWER COMPOSITES Maria Valkova College A laminate finiteconsolidation element model for prediction of meso- and fibre architecture packing structural in compositespower employing a hybrid fabric-reinforced woven construction. 1211-3 UNIT FOR CELLS MULTIPHYSICS OF MODELLING STRUCTURAL BATTERY COMPOSITES Carlstedt David , , Korea , Concordia

1310 Sensing 2: composites sensors stain as Meeting room 214 room Meeting 1310-1 ON THESTUDY CORE-SHELL STRUCTURED TYPEFIBER STRAIN WITH SENSOR BEARING LOAD CHARACTERISTICS IN COMPOSITE STRUCTURES On Seung Yoon Advanced Institute of Science and Technology 1210-2 MONITORING APPROACH FOR DAMAGE FATIGUE ONSET THRESHOLD DETERMINATION IN COMPOSITES FLAWS CONTAINING Ahmed Maslouhi Université de Sherbrooke paper presentsThis approach an original mainlybased on emissionacoustic to monitoring life fatigue determine damage to thresholds concernedinitiation in composites with embedded artificial study flaws. This combines two health techniquesmonitoring life fatigue determine to curves estimate and to stiffness degradation weave for plain composites containing flaws. 1210-3 OF IN-SITU SENSING RANDOM FAILURE IN COMPOSITE STRUCTURES Suong Hoa University Development of in failure random composite structures cyclicdue to loading can be detected using methodthe presented paper. in the , , ,

1309 Interfaces and interphases Meeting room 213 room Meeting 1309-1 MECHANICAL PROPERTIES OF NANO-GRAPHENE COATED PLATELETS FIBER CARBON COMPOSITES EPOXY Alok Srivastava Kumar of Indian Institute Bombay Technology of strength flexural The carbonthe fiber epoxy has laminates based been improve found to significantly GNP with addition the using method. coating spray 1209-2 1209-2 INTERPHASE OF ANALYSIS POLYAMIDE66 WITH LAMINATES PROTONATED DEUTERATED AND POLYMERS Matsumoto Takuya Kobe University focused on the We adhesion interphase of polyamide 66 Forlaminates. the analysis interphase confocalwith scattering Raman the spectroscopy, and protonated polyamide deuterated employed.66 were 1209-3 TAILORING INTERFACIAL INADHESION FIBRE BASALT REINFORCED POLYMER COMPOSITES Maria Carolina Seghini Sapienza-Università di Roma , , Institut , Institut

1308 matrix Polymer materials Meeting room 212 room Meeting 1308-1 1308-1 BEHAVIOUR TENSILE OF THIN-PLY COMPOSITES Wu Haihong Henan University of Technology 1208-2 OF EXAMINATION THE INTERFACE STRENGTH OF HYBRID, OVERMOULDED THERMOPLASTIC PARTS COMPOSITE Yves Becker Verbundwerkstoffe für Gmbh , University

1307 Computational and finite element methods Meeting room 211 room Meeting 1307-1 1307-1 APPROACH A NOVEL FOR MODELLING OF ROS AND ROS-HYBRID COMPOSITES Saeed Rizwan Choudhry of Derby A new approach for parametric ofmodel generation fibre discontinuous composites (DFC) that achieves a realistic non-overlapping ofarchitecture Random, Aligned, and Hybrid Tailored DFC for given volume fraction. Langzauner GmbH industry session only *invitation event* CHALLENGES IN INDIVIDUAL AUTOMATION FORSOLUTIONS INCREASING PRODUCTION IN EFFICIENCY AVIATION Hauer Bernhard by Sponsored CONTINUED , , , University 1306 Composite structures Meeting room 210 room Meeting 1306-1 1306-1 TEST VALIDATION OF EXTENSION- TWISTING COUPLED LAMINATES WITH MATCHED ORTHOTROPIC STIFFNESS Kim Kheng Lee PolytechnicSingapore An experimental is study validation for threepresented classes of coupled matching with laminate Extension-Twisting designs The coupling. matching have also orthotropic stiffness in extension and bending, been have which chosen specifically investigate to influencethe of mechanical Extension- and/or Shearing on Bending-Twisting performancethe of Extension-Twisting coupled designs under loads.axial tension 1206-2 STUDIES ON PROPERTY BY ENHANCEMENT OXIDE GRAPHENE IN POLYMER-BASED COMPOSITES LOW AT SERVICED TEMPERATURE ENVIRONMENT Hung Pui Yan UniversitySwinburne of Technology 1206-3 MANUFACTURING TESTING OFAND CLOSED-LOOP GLASS FIBER CYLINDRICAL COMPOSITESEPOXY VARTM USING Monis Kazmi of Auckland focuses research This on finding potential the hollow manufacture to cylindrical epoxy composite structures both flatwith and curved profiles using flat and The VARTM. curved composites under tested were and shear. tension

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1305 fibre Automated placement Meeting room 209 room Meeting 1305-1 IN-PROCESS OF USE AND MONITORING DETECT TO NDT DEFECTS IN THERMOPLASTIC AFP PARTS Ashley Chadwick German Aerospace Center (DLR) ofA combination in- process and monitoring scanning is ultrasound identify to used defects in a thermoplastic composite laminate produced using fibre automated placement. 1205-2 1205-2 EXPERIMENTAL ON INVESTIGATION THE PERFORMANCE OF CARBON- LAMINATES EPOXY GAPS CONTAINING BY FABRICATED FIBER AUTOMATED PLACEMENT Cadran Vincent University 1205-3 EFFECT OF ON TEMPERATURE BEHAVIOUR IMPACT 6/ OF POLYAMIDE BASALT WOVEN FIBRES LAMINATES Russo Pietro Council of Research , Clemson

1304 Design and for manufacture multifunctionality Meeting room 208 room Meeting 1304-1 DESIGN, AND FABRICATION PRELIMINARY EXPERIMENTATION OF A MULTISTABLE KIRIGAMI STRUCTURE Myers Oliver University , ,

1303 fibre Green & natural composites Meeting room 206 room Meeting triethylammonium triethylammonium sulphate hydrogen ionic liquid (IL) was the onto introduced surface of lignin micro/ nanoparticles extracted it was while biomass,from to a highlyprepare functional and reinforcing IL-Lignin filler in an epoxy matrix. 1303-1 HIERARCHICAL MODIFICATION OF FLAX FIBRES ZINC OXIDE BY NANOSTRUCTURES Sbardella Francesca Swinburne UniversitySwinburne of Technology study present The design to aims high performance functionalized lignin- epoxy composites. In work,this the University of Rome “sapienza” Surface modification of flaxthe fibres zinc with oxides via nanorods synthesis. hydrothermal 1203-3 EXTRACTED LIGNIN FROM NATIVE AUSTRALIAN LIGNOCELLULOSIC BIOMASS AS A POWERFUL FORAGENT HIGH- PERFORMANCE COMPOSITES Nisha Sultana Shammi 1203-2 1203-2 RESEARCH ON OF SYNTHESIS BASED CHITOSAN FLAME METAL FORRETARDANT FLAMMABLE COMPOSITES ., M.N Prabhakar National Changwon University , Beihang , Chongqing , University

1302 Bio-inspired composites Meeting room 205 room Meeting 1302-1 THEORETICAL PREDICTION OF BRITTLE- TO-DUCTILE TRANSITION OF BIO-INSPIRED NACREOUS COMPOSITES Cui Shaokang University mechanicalThe ofbehaviors nacre- compositeslike by evaluated are ofa combination analytical solution and numerical through simulation modificationthe of the tension-shear classic chain(TSC) model. 1202-3 WHOLE A NOVEL SELF-LOCKED THIN- COMPOSITE TUBEWALLED SYSTEM Zhao Yang University 1202-2 MANUFACTURING AND OF CARBON- GLASS-FIBER COMPOSITES FRONTAL USING POLYMERIZATION Elyas Goli of Illinois At Urbana- champaign

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, Nanjing Exhibition hall 1301 Nano-composites Coffee break 1301-1 1301-1 ADVANCED POLYMERIC NANOCOMPOSITES WITH FUNCTIONALIZED GRAPHENE OF ANALOGUES MOS2 Mojtaba Ahmadi Deakin University 1201-3 LIGHTNING DAMAGE ASSESSMENT COMPOSITE INTO ON SURFACE BASED EXPLOSION AND BREAKAGEFIBER Audrey Bigand Clément Ader of damage Study the CFRP in the generated strike lightning due to an Abaqusthanks to shock for VDLOAD explosion and pressure for damage a VUMAT law. Plenary 2 1201-2 EXPERIMENTAL OF ICE STUDY ON IMPACT ALUMINUM/ FIBER CARBON REINFORCED DUAL COMPOSITE PLATE Gang LUO University of Aeronautics and Astronautics, Nuaa An experiment of ice ball impact on Aluminum/Carbon Fiber Reinforced Composite dual plate out carried to was dynamic the study responses and damage of target. the The external and internal of Aluminum/ damage Composite dual plate described in this were presentation. 1630-1650 1520-1540 1630-1830 1600-1630 1540-1600 Time MONDAY 12 AUGUST 12 MONDAY

SCIENTIFIC PROGRAM 38 SCIENTIFIC PROGRAM SCIENTIFIC 41 , , Meeting room 219 room Meeting 1315-3 1315-3 INTEGRATED ASSESSMENT OF TO COMPOSITE JOINTSSTEEL IN MARINE APPLICATIONS Geir Ólafsson University of Southampton 1315-4 EXPERIMENTAL ON THESTUDY OFPERFORMANCE METAL- HYBRID JOINTSCOMPOSITE QUASI-STATIC AT INTERMEDIATE AND STRAIN RATES Karthik Ramaswamy University of Limerick 1315-2 SIMULATION OF INDUCTION PROCESS WELDING FOR GLASS FIBER THERMOPLASTIC COMPOSITES IN AEROSPACE APPLICATIONS Martine Dube , RMIT RMIT , -CT , University , Beijing Meeting room 218 room Meeting 1314-3 THE MODELLING FRACTURE ENERGY OF POLYMER NANOCOMPOSITES Mukesh Bhasin University Mechanistic-based analytical models to predict mode the I fracture interlaminar toughness of carbon nanoparticle reinforced polymer composites described,are and compared to data. experimental 1314-4 DEFECT CHARACTERIZATION MECHANICAL AND PROPERTIES OF MULTI- LATTICE LAYER STRUCTURE Chuanlei Li of Technology Institute A novel modeling been proposedhas μ based on the scan reconstruction investigate to data influencethe of geometrical defects mechanicalon the performance of lattice structure. 1314-2 CHARACTERISING MULTI-DIRECTIONAL LAMINATES SUBJECTED TENSION/ TO COMPRESSION- SHEAR LOADING A MODIFIED USING ARCAN FIXTURE Laux Tobias of Southampton An experimental devisedprocedure is based on a re- designed Modified FixtureArcan (MAF) to compositeinvestigate subjectedlaminates combinedto tension/ compression-shear Experimentalloading. results three for multidirectional, quasi- carbon/epoxy isotropic different with laminates ply thicknesses and anglesfibre orientation presented. are , , Mcgill , The Meeting room 217 room Meeting 1313-4 AND VALIDATION APPLICATION OF MICRO-CT FOR ANALYSIS CARBON RECYCLED WEB CARD FIBER REINFORCED THERMOPLASTICS Siyi Shao University of Tokyo proposed study The a method evaluate to fiberthe orientation (FOD)distribution of Carbon Fibre Reinforced Plastics Micro from (CFRP) Computed Tomography (Micro-CT) data. 1313-2 DEVELOPMENT OF A VERSATILE RECYCLED COMPRESSION MOULDING COMPOUND MADE FROM UNCURED AEROSPACE PREPREG OFFCUTS HubertPascal University paper introducesThis a recycling framework for compression moulding of uncured offcuts.prepreg The processing aspect is of framework the discussed in detail, thermochemical where resin characterization flow- and 1-D are compaction trials the understand to used a resin’s impact that processing viscosity and nature on the has of prepreg magnitude A recycling flow. process then is map in which presented flow and cycle tailoring is time customization achieved by increasing initial resin’s the degree-of-cure through staging. 1313-3 3D PRINTING OF RECYCLED PET POLYMER COMPOSITE WITH INFUSED SUSTAINABLE CARBON Rangari Vijaya Tuskegee , , School of , Defence Meeting room 216 room Meeting 1312-4 STACKING SEQUENCE DETERMINATION ELASTICAND PROPERTIES IDENTIFICATION FOR CFRP USING LAMINATES ULTRASONIC TECHNIQUES Jinling Zhao and PowerMechanical Engineering, Nanjing University Tech bulk Ultrasonic technique wave identify used to was stacking sequences on which of CFRP, guided wave basis further was approach towards investigated stiffness coefficients of a determination in the single lamina structure. 1312-2 LIFE FATIGUE FOR PROGNOSIS COMPOISTE USING LAMINATES LAMB WAVE VELOCITY Chongcong Tao Nanjing University of Aeronautics and Astronautics life prognosis Fatigue of composite laminates realized usingis toBayesian inference distribution obtain the of aof parameters velocity degradation model, and laser method ultrasonic velocityfor wave extraction. 1312-3 PENETRATION DEPTH LIMITS OF ACTIVE THERMOGRAPHY FOR DETECTION OF DAMAGE IMPACT FIBRE IN CARBON COMPOSITES Kelly Tsoi Science Technology Group An investigation of penetration the limitsdepth of two active thermographic inspection techniques, and sonicflash for thermography, quantitative sizing of barely impact visible in carbon fibredamage composite subjects. , , Imperial , KTH Royal Meeting room 215 room Meeting 1311-4 OFDESIGN OPTIMISED MULTI-SCALE STRUCTURES FOR MULTIFUNCTIONAL COMPOSITES Chanhui Lee College London 1311-2 STRUCTURAL POSITIVE ELECTRODES FOR MULTIFUNCTIONAL COMPOSITE MATERIALS Karl Bouton of Technology Institute at aims study The developing a coating for thetechnique ofmaking structural positive electrodes, i.e. Lithium oxide coated- carbon fibres. The subsequent technique consists a Layer- in assemblyby-Layer of lithium oxide the particles carbon the on fibres. deposition The process followed is by low-temperature carbonisation. 1311-3 MORPHOLOGICAL CONTROL OF STRUCTURAL FOR ELECTROLYTES MULTIFUNCTIONAL COMPOSITES DongWen Quan University,Durham UK , Hong , University , Beihang Meeting room 214 room Meeting 1310-4 LASER INDUCED FREESTANDING GRAPHENE FOR PAPERS MULTIFUNCTIONAL COMPOSITES Sida Luo University 1310-2 ZINC TAILORED INTERPHASE OXIDE FIBER IN CARBON REINFORCED COMPOSITES STRAINACROSS RATES Jalal Nasser of Michigan Zinc oxide interphases tailor the used to are interfacial properties of carbon fiber reinforced polymer compositesmatrix for simultaneously performanceoptimal in and ballistic structural applications. 1310-3 SKIN- HUMAN MIMICKING INTEGRATED WITH SENSOR ULTRAHIGH SENSITIVITY FOR MULTIDIRECTIONAL SENSING ChenHaomin Kong University of Science and Technology skin, Mimicking human a novel multidirectional consisting sensor strain of a PUGA composite and a spinosum- conductivelike is microstructure developed for sensing from deformation directions.different , IMP INSA , NUAA , Shaanxi Meeting room 213 room Meeting Lyon objectThe of this understand to is study extend what to involvedphenomenons interfacein the building of a self-reinforced polypropylene composite can be its to overall related mechanical properties. 1309-4 THE ENHANCING INTERFACIAL ADHESION VIA CHEMICAL GRAFTING MULTILAYER POLYDOPAMINE/GO FIBER ON CARBON SURFACE Qing Wu University of Science & Technology Nano-structured polyether amine/ GO multilayers attached were carbon fiberonto surface by chemical approach, grafting and its effects on interfacial adhesion of composites were investigated. 1309-2 FIBER/MATRIX A KEYINTERFACE: COMPONENT IN A SELF-REINFORCED POLYPROPYLENE COMPOSITE Amel Terras 1309-3 THE IMPROVING INTERFACIAL BONDING OF TI/ STRENGTH METAL FIBER CFRP BY LAMINATES MULTI- USING CARBON WALLED NANOTUBES Wang Hao Since interface the relatively weak the is of fiberarea metal (FMLs),laminates of reinforcement the metal/resin interface desiredis urgently. a study, this In metallic-inorganic- system and organic equations related developedwere to describe interfacial the behaviors. , Toray , Toray , Aerospace , University of Meeting room 212 room Meeting 1308-4 1308-4 FILLING MICROTUBULES WITH TRIPHENYL FOR PHOSPHATE FLAME-RETARDING COMPOSITESEPOXY Ma Jun South Australia 1308-2 1308-2 INVESTIGATION ON IMPROVING THE COMPRESSIVE OF THE STRENGTH UNIDIRECTIONAL FIBER CARBON REINFORCED POLYMER COMPOSITE LiLong Institute Research of and Materials ProcessingTechnology Effectkey of factors compressiveon the properties of unidirectional carbon fiberreinforced polymer investigated, is diameter including the of fibers, Young’s modulus of resin and interfacial bonding strength. 1308-3 HIGH HEAT RESISTANCE EPOXY-BASED COMPOSITES Tun Swezin Than Composite Materials America Inc. epoxy- that known It is compositebased been have materials servicelimited to of below temperatures 140°C, use forcing the of high temperature like materials (BMI,bismaleimide PEEK, or polyimide composites. Toray has group research recently developed an epoxy-based resin system has which transition a glass of (Tg) temperature serve will which 235°C of use the widen to epoxy a higher to range. temperature , , DTU , ETH Zurich Meeting room 211 room Meeting 1307-4 1307-4 INVESTIGATION OF CORRUGATED LAMINATES TO SUBJECTED TRANSVERSE SHEAR LOADING Daniel Thomas Filipovic presentation The on givewill insight resultsthe and the of an derivation efficient finite element model derived for the calculating ofresponse corrugated subjectedlaminates shear transverse to loading. 1307-2 1307-2 FUTURE MICROBOND TESTING - FINITE ELEMENT OF SIMULATION FIBERSOPTICAL FOR STRAINS Royson Dsouza University Tampere Finland paper presentsThe Element a 3D Finite (FE) modeling and of the simulation with test mirobond for FBG sensors sensing local strain and improved ofunderstanding the fiber interface.droplet 1307-3 CROSS-SECTION OF ANALYSIS BEAMSTAPERED Paola Bertolini A numerical of thecomparison stresses evaluated both 3D FEAwith and cross-section analysis highlights the how the lack currently latter capability correctly to recover stresses the in tapered beams. , , The , Swinburne Meeting room 210 room Meeting 1306-4 1306-4 STRUCTURAL OF RESPONSE BALLISTICALLY DAMAGED COMPOSITE HONEYCOMB SANDWICH STRUCTURES Binod Aryal University of New South Wales 1306-2 1306-2 LAMINATE FORDESIGN POST- IMPROVED STABLE CRITICALLY PERFORMANCE York Christopher of Institute Singapore Technology articleThis discusses performance,laminate pre- to and relating post-critically stable response,in-plane for double angle-ply are which laminates, stiffnessto matched standard equivalent symmetric laminate configurations; all fullywith uncoupled stiffness properties Extension-or with coupling. Shearing 1306-3 ENERGY ABSORPTION OF METAL EXPANDED TUBES UNDER LOAD EXPANDING Guoxing Lu University of Technology , , , Meeting room 209 room Meeting 1305-4 DEVELOPMENT OF DRY AUTOMATED FIBRE PLACEMENT FOR HIGH RATE DEPOSITION Evans Anthony University of Nottingham and Investigation the into explanation development and design of a high-speed dryautomated fibre machine placement (ADFP). Presentation focuses data on the acquisition and transfer, and heating Joule for control temperature rates high heating 1305-2 OF COMPARISON FOR SOURCES HEAT DRY AUTOMATED FIBRE PLACEMENT: XENON FLASHLAMP- VS. INFRARED-HEATING Dominik Deden German Aerospace Centre Augsburg a xenon- study, this In heating flashlamp system benchmarked is in radiators infrared to of peelterms strength distribution and heat lay-down various at Speeds for dry fibre placement. 1305-3 EVOLUTION OF CRYTALLINITY WITH MULTIPLE LAMINATION IN HIGHSTEPS PERFORMANCE THERMOPLASTIC COMPOSITES IN-SITU BY CONSOLIDATION PROCESS Ingrid Esguerra FIDAMC - - , DST , Harbin , University of Meeting room 208 room Meeting 1304-4 INKJETLOCALISED PRINTING OF RESIN ADDITIVES FOR SELECTIVE PROPERTY ENHANCEMENT Ian Gent Bristol inkjetA customised designed to was printer deposit resin additives. Open hole test specimens containing particlesthermoplastic exhibited a 3.8% in failure increase compared to strength unmodified specimens. 1304-2 MULTIFUNCTIONAL COMPOSITE HOLOGRAPHIC ANTENNA STRUCTURES Baum Thomas Group paper presentsThis preliminary work developing towards multi-functional antennas conformal based on new electromagnetic meta- approaches, material specifically holographic based on antennas artificial impedance surfaces (AIS). 1304-3 CHARACTERIZA TIONS APPLICATIONS AND OF NONPOSITIVE PARAMETRIC MECHANICAL METAMATERIALS Yang Hang of Technology Institute expands the work This appli multi-functional of cations non-positive mechanical parametric - metamaterials(neg Poisson’s ative/zero ratio,negative/zero stiffness)the based on of characterizations their unprecedented mechanical properties , , , Sapienza Meeting room 206 room Meeting 1303-4 1303-4 BLAST RESPONSE OF PANELS CONTAINING SUSTAINABLE MATERIALS Chris von Klemperer 1303-3 1303-3 CORK CORE SANDWICH STRUCTURES: AND STATIC DYNAMIC RESPONSE Claudia Sergi University of Rome ofComparison cork agglomerated and PVC foams mechanical properties and their application in bio-based sandwich subjected to structures impact loading. University of Cape Mechanical Town, Engineering fibre Sustainable reinforced epoxy composites or Flax containing Jute were reinforcement exposed explosive to loading and airblast resultsthe compared fibre epoxy glass to exposed also panels to airblast. 1303-2 BIOCOMPOSITES MANUFACTURED USING WATERASSISTED COMPOUNDING OF COFFEE GROUNDS WITH FOR POLYSTYRENE THERMOFORMING CUPS Daniel Schwendemann University of Applied Sciences Eastern Switzerland IWK Water-assisted compounding allows of using a new way spend coffee grounds in compounding a polymer/biobased composite material. more new, the With compoundcirccular vending cups are thermoformed. , , Imperial , School of Meeting room 205 room Meeting 1302-4 1302-4 OFTHE ROLE DEFECTS IN 3D PRINTING OF BIO- INSPIRED CELLULAR COMPOSITES Sardar Malek University of Sydney Technology 1302-3 1302-3 METHODS ANALYTIC RESIN PREDICT TO POCKET GEOMETRY AROUND THE MICROVASCULE IN SELF-HEALING COMPOSITES Ma Yihao Aeronautic Science and Engineering, Beihang University analytic methods Two developedare to predict resin pocket the geometry the around in self- microvascule healing composites. bending strain The calculated is energy fiberon the scale and scale respectively. layer 1302-2 HYBRID COMPOSITES WITH A CROSSED- LAMELLAR MICROSTRUCTURE FOR STRUCTURAL INTEGRITY Riikka Häsä College London designed We new CFRP and compositeshybrid bio-inspiredwith crossed-lamellar We microstructures. that demonstrated these composites preserve their integrity structural extremelyup to large and deformations exhibit extensive diffusion. damage

, , , Department 1301-4 1301-4 COMPETITION BETWEEN DIFFERENT TOUGHENING IN MECHANISMS COMPOSITES WITH NANOTUBE CARBON GRAFTED FIBERS Qiang Liu Toyama Prefectural Toyama University properties of Tensile PP and the PFA the nano-composites filled silica nanosphereswith untreated having surfaceshydrophilic with investigated were effects on the a focus of silica/polymer matrix interfacial debonding. of Materials Engineering, Leuven Ku 1301-3 1301-3 TENSILE PROPERTIES OF CRYSTALLINE POLYMER COMPOSITE SYSTEMS WITHFILLED SILICA SPHERICAL NANOPARTICLES HAVING HYDROPHILIC SURFACES Mitsuru Tanahashi Plenary 2 1301-2 1301-2 OF GRAPHENE USE RESIN REDUCE TO CURE SHRINKAGE Siang Sum Wei PETRONAS Research 1650-1710 1730-1750 1710-1730 Time MONDAY 12 AUGUST 12 MONDAY

SCIENTIFIC PROGRAM 40 SCIENTIFIC PROGRAM SCIENTIFIC 43 Meeting room 219 room Meeting Meeting room 218 room Meeting , , The Australian , The Australian Meeting room 217 room Meeting 1313-5 INVESTIGATING THE CONSISTENCY IN PHYSICAL PROPERTIES OF 3D PRINTED RECYCLED FIBER CARBON Peng Wang Hao UniversityPurdue a team study, this In Universityof Purdue School of Aviation and Transportation (SATT) Technology faculty and students up teamed have the investigate to consistency in physical properties of recycled3D printed carbon fiber. 1313-6 THE EFFECT OF FIBRE SURFACE TREATMENTS DURING CFRP PRODUCTION ON THE TENSILE OF STRENGTH CARBON RECYCLED FIBRES He Di University National A recycling on study carbon fibre reinforced polymers (CFRPs) found minor impacts of electrochemical and sizingoxidation during treatment CFRP production on of strength tensile the recycled carbon fibres. Meeting room 216 room Meeting 1312-5 FIBRE:INSEGT A USER-FRIENDLY SOFTWARE FOR FIBRE INDIVIDUAL SEGMENTATION Monica Jane Emerson, University ofTechnical Denmark a is Fibre Insegt toolbox software fibrefor volumetric By segmentation. individual measuring fibres X-ray from it enablestomograms, characterisation the compositeof real and its microstructure changes load. under , Meeting room 215 room Meeting 1311-5 POLYMERISIED INTERNALMEDIUM EMULSIONS PHASE AS STRUCTURAL SEPARATORS Shirshova Natasha UniversityDurham , Cornell Das, The Meeting room 214 room Meeting 1310-5 SENSORY OPTICAL NETWORKS IN SOFT MECHANICAL COMPOSITES Xu Patricia University optical Stretchable networkslightguide embedded 3D within scaffolds soft printed, for deformation of sensing the state body machine using learning. 1310-6 STRAIN SENSING CAPABILITY OF POLYANILINE- BASED CONDUCTIVE GLASS FIBER REINFORCED COMPOSITE Sukanta University of Tokyo Polyaniline-based conductive polymer, glassreinforced with fiber been studied has for self-sensing. A four probes electrical resistance measurement was technique measure to adopted change resistance the of composite under loading. - , The , Beihang Meeting room 213 room Meeting 1309-5 EFFECTOF CARBOXYL CONTENT ON CRABON FIBER ON SURFACE INTERFACILAL OFADHESION 6 FIBER/NYLON Zhang Tao University reportThis investigates effectthe of surface chemical of characteristics carbon fibers on the interfacial properties of carbon fibers/nylon 6 composites. 1309-6 DEVELOPMENT - OF HIGH-PERFOR TRILAYERED MANCE LAALO3/SRTIO3/ LAALO3 HETERO STRUCTURES FOR ELECTRONIC DEVICES Hu Hailong University of New South Wales , , The University

Meeting room 212 room Meeting 1308-5 1308-5 EFFECTOF CNTS CONTENT AS TERTIARY FILLER ON CNTS/XGNP/SG/ EPOXY NANOCOMPOSITES ON THE THROUGH-PLANE CONDUCTIVITY Suherman Hendra Universitas Hatta Bung Carbon nanotubes the have (CNTs) be as used to potential conductive third the filler nano-sized due to and tube-shaped, so as between fill gap to the secondthe conductive larger filler is which in size. 1308-6 THERMOSET HYBRID COMPOSITES FOR IMPROVING FRACTURE TOUGHNESS Kanokporn Tangthana- umrung of Manchester Combining the advantages of engineeringthe and thermoplastic nanoplatelets graphene fracture improve to toughness of epoxy maintaining while all mechanical and propertiesthermal of material. , Meeting room 211 room Meeting 1307-5 1307-5 AN ADAPTIVE METHODOLOGY FOR EFFICIENT MODELLING OF ARBITRARY DELAMINATIONS DURING CRASH SIMULATIONS Johannes Främby Chalmers University of Technology , , Meeting room 210 room Meeting 1306-5 1306-5 INTEGRATED AN METHODOLOGY FOR FULL-FIELD AND IMAGING NUMERICAL OF ANALYSIS COMPLEX COMPOSITE SUBSTRUCTURES CallaghanJack University of Southampton 1306-6 1306-6 THERMAL DEGRADATION STUDY OF BISMALEIMIDE COMPOSITE Dongbing Geng Aerospace Research of Materials Institute and Processing Technology , , Meeting room 209 room Meeting 1305-5 MANUFACTURING WITH THIN- STUDY COMPOSITE PLY PREPREGS IN FIBER AUTOMATED PLACEMENT (AFP) Hansen Christopher University of Massachusetts Lowell key material, The and spooling,slitting and AFP processing for parameters are materials thin-ply identified and tested produce consistent to feedand repeatable of the through material AFP head. 1305-6 DRIVEN DATA AUTOMATED - ENABLING LAYUP THE AUTOMATION POTENTIAL Philippe Monnot Composites National Centre , , RMIT RMIT , Meeting room 208 room Meeting 1304-5 MODEMODE I AND II FRACTURE PROPERTIES OF MENDABLE 3D WOVEN HYBRID COMPOSITES Raj Ladani University 1304-6 STRUCTURAL HEALTH FORMONITORING FIBRE REIN-FORCED COMPOSITES THE BY PRODUCED PROCESS WINDING Mario Naumann University ofTechnical Chemnitz ,

, School Meeting room 206 room Meeting 1303-5 1303-5 EXPERIMENTAL MOLECULARAND STUDIES DYNAMICS OF ANTIMICROBIAL ADDITIVE FROM MIGRATION BIOCOMPOSITE PACKAGING Venkata Chevali Venkata University of Southern Queensland 1303-6 1303-6 MANUFACTURING PLASTICWOOD FROMCOMPOSITE RPET/HDPE/ LDPE/UHMWPE REINFORCED RICE FIBRE HUSK Utai Meekum of Design Technology of Design Technology of Engineering,Institute UniversitySuranaree of Technology prevent the to order In of degradation thermal fiber on the natural the of wood manufacturing compositeplastic based on rPET/ UHMWPE/HDPE ricereinforced with processing fiber, husk below temperature prime the was 230oC objective. , , Meeting room 205 room Meeting 1302-5 1302-5 TIGR-NACRE: A NEW DAMAGE-TOLERANT COMPOSITE CFRP Pascoe John-Alan Imperial College London Ductility and damage diffusion in a CFRP- based composite possible.are We achieve these features by combining a micro-nacre-inspired titanium with structure interlayers. 1302-6 1302-6 AUTOMATICALLY PROCESSED BIOINSPIRED HIERACHICAL FIBER CARBON COMPOSITES Rodríguez Verónica FIDAMC One of main the of carbondrawbacks fibre reinforced polymers is (CFRPs) and delamination the failure catastrophic theymechanism reaching when present their mechanical limits. of limiting A way is kind ofthis failure in this investigated project.

, Welcome reception Welcome Exhibition hall Plenary 2 1301-5 1301-5 CARBON NANOTUBE/ 6 POLYAMIDE NANOCOMPOSITES VIA IN-SITU ANIONIC POLYMERISATION VillacortaByron University of Queensland 1750-1810 1810-1830 1845-2100 Time MONDAY 12 AUGUST 12 MONDAY

SCIENTIFIC PROGRAM 42 SCIENTIFIC PROGRAM SCIENTIFIC 45 , , ,

Meeting room 219 room Meeting 2115 Repair 2115-2 2115-2 RESIN-INJECTION OF BARELY REPAIR IMPACT VISIBLE ON DAMAGE FIBRE CARBON COMPOSITE LAMINATES LiangWei Lai UniversityNewcastle in Singapore approach A systematic employed investigate to vacuum-assisted how resin-injection repair method could restore mechanicalthe integrity of barely the impactvisible damage on carbon fibre composite laminates. 2115-3 AND NUMERICAL EXPERIMENTAL OFSTUDY STRUCTURAL FILM ADHESIVES AND SCARF REPAIR Sridhar Narayanaswamy of High Institute Performance Computing an present We experimentally numerical validated predict to framework response structural the scarfof repaired joints for varying and lay-up loading conditions. 2115-1 IN ADVANCES THE BONDLINE CONTROL FOR TECHNOLOGY THE CERTIFICATION OF ADHESIVELY BONDED COMPOSITE REPAIRS Lennert Heilmann German Aerospace Center (DLR) , , Rise ,

Meeting room 218 room Meeting 2114 creep Durability, and aggressive environment 2114-2 2114-2 ENVIRONMENTAL EFFECTS ON COMPOSITE BOLTED JOINTS SUBJECTED TO PRELOAD PivdiablykIvanna Ecole De Centrale Nantes 2114-3 EFFECT OF MOISTURE ON SATURATION THE THERMAL EXPANSION COEFFICIENT OF COMPOSITES Nigel St John Defence Science and Group Technology Effect Moisture of on the Saturation ExpansionThermal Coefficient of Composites 2114-1 2114-1 EFFECTS THIN-PLY ON LONG-TERM THERMAL OF HIGH STABILITY TEMPERATURE POLYIMIDE COMPOSITES FernbergPatrik Sicomp paper investigates The thin-ply the how effectrole a can play for high temperature composites. Mechanical performance in tension long-term as well as stabilitythermal are considered. - - - , Deakin , Ifremer , University

Meeting room 217 room Meeting 2113 energy Renewable 2113-3 CONTROLLED OF ROBUST DESIGN HIERARCHICALLY ANDPOROUS CARBON HOLLOW FIBRE TEXTILE FOR HIGH- PERFORMANCE FREESTANDING ELECTRODES Quanxiang Li University 2113-2 REACTIVE THERMO PLASTIC RESIN AS A FOR LAMI MATRIX CONTAINING NATES MICROENCAP PHASE SULATED MATERIALS CHANGE Giulia Fredi of Trento This paper describesThis early results from Realtidethe H2020 projectEuropean improve to aims which reliabilitythe of tidal generate to turbines marine renewable composite The energy. a criticalblades are component and a testing campaign been performedhas their investigate to durability. long term Results shown are aging for seawater and its influence on performance.fatigue These results be will models into integrated behaviour. of long term 2113-1 RELIABILITY OF TIDAL COMPOSITE TURBINE BLADES Mael Arhant

, Monash , Monash , Defence , Hanyang , Hanyang MN-PMN-

⟩ 011 Meeting room 216 room Meeting 2112 health Structural monitoring 2112-3 OFMONITORING HYDRATION CEMENT TERAHERTZUSING RADIATION Heonsu Kim University 2112-1 MEASURED LAMB RADIATION WAVE FROM PATTERNS ⟨ PZT RELAXOR FERROELECTRIC ON A DISKS PLATE COMPOSITE Benjamin Vien University 2112-2 A NOVEL HIGH DENSITY PIEZOELECTRIC SENSING CAPABILITY FOR DETECTION IN OF IMPACTS COMPOSITES Cedric Rosalie Science & Technology Group a novel paper, this In system sensing acoustic for aircraft suitable is implementation and used to presented localisation demonstrate of emission acoustic non- from generated impactsdamaging in a composite panel. , Korea , The , University

Meeting room 215 room Meeting 2111 by design Materials 2111-3 CONDUCTIVE NANOCOMPOSITES MANUFACTURED VIA FRONTAL POLYMERIZATION DeanLeon of Illinois Urbana- at Champaign 2111-1 - PIE COUPLED AND ZORESISTIVE THERMORESISTIVE - OF CAR BEHAVIOR BON NANOTUBE THEIR AND YARNS THERMOSETTING MONOFILAMENT COMPOSITES AbotJandro Catholic University of America Carbon nanotube lightweight, are yarns electrically and strong conductive fiber-like exhibit that materials outstanding physical properties and can be synthesized Their continuously. coupled piezoresistive being is response for investigated smart materials that could detect damage strain and measure polymersinside and polymeric composites. 2111-2 THE ORGANIC AND INORGANIC HYBRID NANOCOMPOSITE FOR FLEXIBLE UV SENSOR Park Teahoon of Materials Institute Science , , ETH, , KTH,

Meeting room 214 room Meeting 2110 1: morphing Actuation multifunctional composites 2110-3 MULTI-FUNCTIONAL ADAPTABLE SHAPE COMPOSITE METAMATERIAL FOR AEROSPACE APPLICATIONS Maria Sakovsky Zürich A novel single- procedure for cure of complexfabrication assemblies of fiber reinforced polymer proposed. It is is shells mechanicalapplied to capable metamaterial of achieving 60% global deformation potential the showing of for use such assemblies for stiff yet aerospacedeformable structures. University of Southern California telescopingA practical combined is wing with bio-inspired body-tail to configuration produce a novel design tail deploymentwhere and configuration clutchedcome from electrolaminate materials. 2110-1 ENABLING BIOMIMETIC UAVS MORPHING Geoffrey Spedding 2110-2 MORPHING FIBRE CARBON USING COMPOSITE ELECTROCHEMICAL ACTUATION Ross Harnden of Institute Royal Sweden Technology, A concept for a actuation structural device presented is and modelled. A carbon fibre laminate be to shown is capable of producing significant geometry changes by exploiting intercalation lithium-ion expansions.

, , RMIT RMIT , , Ku

Meeting room 213 room Meeting 2109 fibre Green & natural composites 2109-3 INVESTIGATING THE MECHANICAL PROPERTIES OF AND CELLULOSE AMORPHOUS BY CELLULOSE MOLECULAR DYNAMICS SIMULATION Ali Khodayari Leuven 2109-1 MICROSTRUCTURE MECHANICAL AND PROPERTIES OF HEMP ELEMENTARY FIBRES FOR COMPOSITE BY APPLICATIONS MICRO-COMPUTED AND TOMOGRAPHY IMAGE DIGITAL CORRELATION Carlos Rojas Fuentes KULeuven non-linear The of elementarybehavior and technical hemp fibres samples were bycharacterized, combining standard tests atensile with detailed full-field strain scale micro the at map loading. tensile during 2109-2 SUSTAINABLE MYCELIUM-DERIVED THINCHITINOUS FILMS Mitchell Jones University , , Deakin University

Meeting room 212 room Meeting 2108 Resin and polymers 2108-1 EXPERIMENTAL OF THESTUDY AND MECHANICAL FLAMMABILITY OF BEHAVIOUR RUBBER AND SILICA NANOCOMPOSITES Alexander Fergusson Technology Fac 2108-2 CURE KINETICS SHRINKAGE AND MEASUREMENTS CURING IN A FAST RESIN AMINE EPOXY SYSTEM Masihullah Jabarulla Khan kinetics,Cure chemical along withshrinkage CTE measurements for a commercially curing fast available epoxy amine resin beensystem have reported. work This valuable provide will for information of residualcalculation instresses occurring carbon fibre reinforced composites used in dynamic applications. ,

, Nanjing

, Universityof , Ford (Meeting 213) room 2107 Computational and finite methods element Meeting room 211 room Meeting 2107-3 THE 3D PRESSURE- DEPENDENT ELASTO-PLASTIC CONSTITUTIVE WITHINMODEL AND TENSION COMPRESSION ASYMMETRY AND ITS APPLICATION PREDICT TO OFF- LAMINATES’ AXIS LOADING RESPONSES Ren Rui University of Science and Technology A novel elasto-plastic constitutive model the incorporating tension-compression asymmetry and pressure hydrostatic dependence of yieldinglaminates’ behaviors, was developed for fiber- reinforced composite and validated laminates test results. by available Swinburne UniversitySwinburne Molecular Using Dynamics (MD), and pine LLDPE flour molecules are Benefitsconstructed. of combined the MD-semi empirical modelling approach up designfor bottom by discussed is predictedcomparing composite properties experiment.with 2107-2 PREDICTING TRENDS IN STRUCTURAL PHYSICAL AND PROPERTIES OF POLYMER HYBRID COMPOSITES MOLECULARUSING DYNAMICS Krishnamurthy Prasad 2107-1 DEVELOPMENT OF A 3D FINITE MODELELEMENT OF A QUASI-STATIC INDENTATION TEST IN A TYPE III PRESSURE VESSEL DeErick Montes Oca Valle Southampton A 3D FE model is developed predict to de-cohesionthe resultant and the of thedeformation aluminium liner of a III vesselpressure Type subjected a quasi- to test. indentation static , , , Lulea University, Lulea of Technology , Texas , Texas , Imperial College (Meeting 211) room

, University of Sydney (Meeting 212) room 2106 Scott White symposium Meeting room 210 room Meeting 2106-3 DESIGN PERSISTENT CHALLENGES: COMPATIBLE, SUSTAINABLE AND AFFORDABLE COMPOSITES OchoaOzden A&m University Life cycle prediction of multifunctional systems introduces new opportunities to address performance, cost and sustainability minimumwith impact.environmental Characterization and modeling consequences be will for hybriddiscussed composites. 2106-2 MICRO- MECHANICAL OFMODELING THROUGH FLOW PACKED RANDOMLY OF CYLINDERS BEDS & SPHERES: DISPERSION, AND DEFORMATION TRANSFER HEAT AS (PARTLY A AT PRESENTED SEMINAR BECKMAN 2014) APRIL Lundström Staffan universityLuleå of technology 2106-1 OF AMODELING NEW COMPOSITE MANUFACTURING BASEDPROCESS ON FRONTAL POLYMERIZATION Philippe Geubelle University of Illinois at Urbana-Champaign , University (Meeting 210) room of Bristol Kristiina Oksman - , - , Soraia PimentaSoraia , University

2105 Advanced and manufacturing automation Meeting room 209 room Meeting 2105-3 INFLUENCE OF POWER ON ULTRASONIC THE IMPREGNATION OF UNIDIRECTIONAL FIBRES INCARBON INJECTION CLOSED PULTRUSION WilhelmFrederik Research Fraunhofer for Casting,Institution Composite and Processing Technology Igcv of Implementation in the ultrasonic power processpultrusion with aim ofthe improving and impregnation the mechanical properties of parts. the 2105-2 OF INFLUENCE MA CONTACTING, SHAPE AND TERIAL ON THE RESIST OF HEATING ANCE CONTINUOUS FIBER REINFORCED- THER MOPLASTICS Jochen Wellekötter Für Institut Kunststofftechnik, Universität Stuttgart effectThe Jouleof heat to used is heating carben fiber reinforced High thermoplastics. low with rates heating consumption energy achieved.are betweenCorrelations influencing parameters and investigated are specified. Heating experiments com- are a thermo- using pared system. image graphic 2105-1 ADDITIVE MANUFACTURED ELECTROACTIVE MEMORY SHAPE POLYMER COMPOSITES GarcesIrina of Alberta Shape Memory CompositesPolymer can sensors be as used and actuators. This explores thestudy and manufacturing development of an electroactive self- SMPCsensing for field applications. (Meeting 219) room of Technology Institute , Kanazawa , - , , TWI

2104 Design and for manufacture multifunctionality Meeting room 208 room Meeting 2104-3 THERMALLY PIERCING; ASSISTED AND MANUFACTURE PROPERTIES OF MULTIPLY-PIERCED COMPOSITE Eghtesadi Faranak Bahrami comparison The for of strength the and thermally drilled piercedassisted thermoplastic (TAP) composite, Carbon Fibre/Polyamide-12. technique TAP The improved shown has when strength thecompared to drilling conventional technique. 2104-2 OPTIMIZA LAYUP WAYS TION AND THE IMPROVE TO - MANUFACTURABIL ITY OF COUPLED COMPOSITES Vermes Bruno UniversityBudapest and of Technology Economics and introduce We a layup validate optimization process for coupled composites by a case presenting propose we Also, study. mitigate methods to warping thermal the of composites with non-symmetric layups. 2104-1 ONA STUDY THE PREFORM IN DEFORMATION THERMOPLASTIC COMPOSITE OVERMOULDING Mario Adrian Valverde CompositeBristol (ACCIS)Institute experimental Two usedsetups are the investigate to compaction behaviour carbonof continuous fibre - Polyphenylene (CF- Sulphide compositesPPS) processed injection via overmoulding. , , Virginia , Virginia , School

(Plenary 2) 2103 Meta-composite Meeting room 206 room Meeting 2103-3 ASYMMETRIC ELASTIC-WAVE IN TRANSMISSION METACOMPOSITE STRUCTURES Bing Li of Aeronautics, Northwestern Polytechnical University 2103-2 AN ELECTRICALLY PROGRAMED ELASTIC FOR METASURFACE MODE WAVE TOTAL CONVERSIONS Guoliang Huang University of Missouri 2103-1 PORO-ELASTIC META ACOUSTIC WITH MATERIALS SOUND IMPROVED ABSORPTION Chris Fuller Tech - , MIT , - , , University , Department Brian Wardle Brian

2102 carbonRenewable 2102-3 SPINNING LIGNIN CARBONIZAAND NANO-LAY TION TO GRAPHITICERED STRUCTURE Mohini Sain of Toronto 2102-2 AND ELECTRICAL NANOSTRUCTURAL STUDIES OF RENEWABLE CARBON Maria Semeniuk University of Toronto 2102-1 FROM TO NANO MICRO: HARDNESS INPREDICTION BASED BIOCARBON COMPOSITES Oisik Das of and Polymer Fibre KTH Royal Technology, of Technology Institute the Using nanoindentation properties of the constituents, the comprehensive or bulk mechanical properties of composites the were predicted. accurately Meeting room 205 room Meeting

- - , - VIRTUAL DESIGN OF HIGH-PERFORMANCE DISCONTINUOUS-COMPOSITE STRUCTURESVIRTUAL OF HIGH-PERFORMANCE DESIGN Blanchard Patrick VEHICLES OPPORTUNITIES FOR COMPOSITES IN NEXT CHALLENGES AND MULTI-MATERIAL GENERATION TESTING METHOD FOR Miyano DURABILITYACCELERATED Yasushi OF CFRP Ian Bond Ian PERSPECTIVE COMPOSITES – A BRISTOL FIBRE REINFORCED POLYMER SELF-HEALING Mai Yiu-Wing FOR ELECTRONIC PACKAGING NANOCOMPOSITES UNDERFILL MATERIALS POLYMER NANOCOMPOSITES AND HIERARCHICAL NANOENGINEERED ADVANCED COMPOSITES FOR ENHANCED MECHANICAL AND MULTIFUNCTIONAL MULTIFUNCTIONAL AND MECHANICAL COMPOSITES FOR ENHANCED ADVANCED NANOENGINEERED HIERARCHICAL NANOCOMPOSITES AND PERFORMANCE , University , School

Day 2 Welcome & Announcements 2 Welcome Day Move to concurrent sessions concurrent to Move KEYNOTE 3: KEYNOTE 5: KEYNOTE 6: KEYNOTE 2: KEYNOTE 4: ability of produced the nanocomposites. 2101-3 EFFECT OF SURFACE FUNCTIONALIZA TION OF GRAPHENE ON THE PARTICLES PROPERTIES OF NA NOCOMPOSITES Annika Catherine Ackermann of Stuttgart, of Institute DesignAircraft effectThe of plasma of graphene treatment particles evaluated was respectwith the to of the characteristics material powder used process the as well as 2101-2 DESIGN, STRUCTURATION RHEOLOGICAL AND PROPERTIES OF LAPONITE BASED POLYMERIC NANOCOMPOSITES AbakarOmar Adam UNABA bestThe Laponite was dispersion solutionobtained from samplesprepared regardless of the of protecting the way particles PMMA/PEO blends nanocomposites behave as simple polymer nanocomposites at high concentration of PEO of Mechanical and Manufacturing Engineering, University of New South Wales 2101-1 SYNERGISTIC EFFECT OF DUAL-SCALE FILLERS CARBON ON SENSITIVITY OF STABILITY AND FLEXIBLE STRAIN SENSORS Zhang Fan KEYNOTE 1: MATERIALS COMPOSITE IN USE THEIR AND PLENARY LECTURE: NANOMATERIALS OF BIOBASED THE STORY Plenary 2 sessions concurrent to Move 2101 Nano-composites Plenary 2 0800-0805 0805-0850 0900-0930 0930-0940 0940-1000 1020-1040 1000-1020 0850-0900 0900-1040 TUESDAY 13 AUGUST TUESDAY Time

SCIENTIFIC PROGRAM 44 SCIENTIFIC PROGRAM SCIENTIFIC 47 , , , Harbin

2215 and wear Tribology Meeting room 219 room Meeting 2215-2 TRIBOLOGY PROPERTY AND ELECTRICAL RESISTIVITY OF C/C COMPOSITES WITH BACTERIAL CELLULOSE Ozawa Yoshihito UniversityFukushima 2215-3 TRIBOLOGICAL PROPERTIES CORROSIONAND OF RESISTANCE NANODIAMOND REINFORCED COMPOSITE ON NITI COATINGS ALLOYS Zhou Huimin Engineering University co-depositedThe ND changes the led to compositionin the of and structure compositeNi-P/ND coatings, contributing of increase the to microhardnessthe and corrosion ofresistance Ni-P/ ND nanocomposite coatings. 2215-1 EXPERIMENTAL SIMULATION AND ON WEARSTUDY OFPERFORMANCE EPOXY ECO-HYBRID COMPOSITE Awwad Khaled Eayal University of Southern Queensland to aims study This influence the study of Graphene and flaxNanoplatelets tribologicalfibre on the and mechanical performances of addition In epoxy. of the simulation to adhesive process. wear , , NASA , Flinders

2214 creep Durability, and aggressive environment Meeting room 218 room Meeting 2214-1 HYBRID ENHANCEMENTS AND INTERFACE ON FIBRE MATRIX REINFORCED POLYMER LAMINATES Tang Youhong University 2214-2 LARGE DEFORMATION BENDING RELAXATION OF THIN-PLY COMPOSITE LAMINATES FernandezJuan Langley Research Center A two-step homogenization employedprocess was ABD the study to stiffnessrelaxation ofof laminates thin NASA to forinterest spacedeployable applications structure and compared to data test uniaxial the test andproduced. The modelsviscoelastic developed help will fold-stow- the study unfold-recovery cycle of these flexible thin-shell increase to structures and long-term reliably predictionbehavior operational in the environment. 2214-3 EVALUATION OF CREEP-LESS COMPOSITES USING EPOXY TG-LESS RESIN AS THE MATRIX Hirofumi Nishida of Institute Kanazawa Tehnology resultsOur strongly thesuggested possibility of producing a creep-less composite good with material mechanical properties epoxy by Tg-less using resin modified with nano-particlerubber as the matrix. , , , Northwestern

2213 matrix Ceramic composites Meeting room 217 room Meeting 2213-1 FINITE ELEMENT SIMULATION ON PREDICTING NONLINEAR MECHANICAL OF BEHAVIOR 3D BRAIDED MATRIX CERAMIC COMPOSITES Xin Jing Polytechnical University 2213-3 BRITTLE FAILURE OF ANALYSIS UNI-DIRECTIONAL MATRIX CERAMIC COMPOSITE UNDERPLIES TRANSVERSE A LOAD: TENSILE COMPUTATIONAL MICROMECHANICS APPROACH Sai Pydi Yeswanth of Indian Institute Indore Technology, 2213-2 PROPERTIES OF YTTRIAPOROUS STABILIZED ZIRCONIA IMPREGRATING WITH SILICA AEROGELS Xiaoyan Wang Aerospace Research & of Material Institute Processing Technology Properties of porous yttria stabilized zirconia silica with impregrating studied. were aerogels the found that It is conductivitythermal and the lowered was compressive strength after increased was of silicaimpregnating aerogels. , The , University of , The University

2212 health Structural monitoring Meeting room 216 room Meeting 2212-1 IN-SITU DEEP LEARNING FOR AND PREDICTION CONTROLS IN COMPOSITESSMART AguasvivasSarah Manzano Colorado Boulder novel present We perform to tools neural networkpredictions in a composite material embeddedwith sensors, actuators and computers. We the demonstrate also possibility of making in complexestimations sensor systems where unknown are locations dynamicor where modeling for system identification be may very complex. 2212-3 IN-SITU MONITORING OF BRAIDED TUBESCOMPOSITE WITH OPTICAL FIBRES AND PIEZOELECTRIC SENSORS Neha Chandarana University of Manchester work, this In an optical fibre based strain integrated is sensor between plies the of compositea braided enables This tube. during monitoring strain resin infusion, braiding, Following and curing. flexuralmanufacture, completed. loading is 2212-2 A VIBRATION-BASED STRUCTURAL HEALTH MONITORING FOR SYSTEM GFRP LAMINATE STRUCTURES Ahmed Ahmed Shihab Al-saadi of Chester , , , Johns

2211 Bio-inspiration Meeting room 215 room Meeting 2211-1 SACRIFICIAL POLYMERS FOR RAPID MANUFACTURING OF VASCULAR MATERIALS Garg Mayank University of Illinois Champaign Urbana Conventional vascularization methods making for multifunctional composites limited are by time and energy- processes.intensive Exothermic curing of host the matrix simultaneouswith of the degradation sacrificial polymer enables rapid of manufacturing polymers andvascular composites. 2211-3 SELF-HEALING COMPOSITESCFRP WITH HIGH THERMAL STABILITY Henry Sodano University of Michigan 2211-2 BIO-INSPIRED OF SYNTHESIS MULTIFUNCTIONAL COMPOSITES WITH SELF-ADAPTABLE MECHANICAL PROPERTIES SELF- AND REGENERATION Sung Kang Hopkins University report a We multifunctional composite inspired reefbone and coral its can adapt that mechanical properties depending on the loading condition and damages.repair , Purdue , Harbin

2210 2:Actuation active composites Meeting room 214 room Meeting 2210-1 PROGRAMMABLE COMPOSITE STRUCTURES FROM BISTABILITY LOCAL Andres Arrieta University 2210-3 3D PRINTING OF CRYSTAL LIQUID ELASTOMERS AS SOFT FOR ACTUATORS MULTIFUNCTIONAL DEVICES H. Jerry Qi, Georgia Tech 2210-2 DIELECTRIC ELASTOMER SOFT ROBOTICS Liwu Liu of Technology Institute , , , UNSW

2209 and damage Fracture Meeting room 213 room Meeting 2209-1 NEAR-REAL-TIME OBSERVATION OF DAMAGE EVOLUTION IN BIAXIALLY STRESSED COMPOSITES USING HIGH-RESOLUTION IN SITU X-RAY COMPUTED TOMOGRAPHY French Jordan University of Utah Novel test biaxial developedmethodwas enablehigh- to resolution X-ray in situ CT of imaging tape- compositeslaminate under complex loading scenarios. 2209-3 DAMAGE CHARACTERISATION IN TEXTILE COMPOSITES: A COMPARISON BETWEEN NEUTRON X-RAY AND TOMOGRAPHY Garth Pearce Sydney 2209-2 EFFECT OF RGO ON COATING NANOSCRATCH OF BEHAVIOR NANOWIRE SILVER NETWORKS Byungil Hwang Chung-ang University , Rmit , The , RMIT RMIT ,

2208 Self-healing Meeting room 212 room Meeting 2208-1 INTRALAMINAR TOUGHENED CARBON/EPOXY COMPOSITES EXHIBITING SELF-HEALING CAPABILITIES Everson Kandare University 2208-3 FRACTURE PROPERTIES OF MENDABLE Z-PINNED COMPOSITES Loh Thomas University 2208-2 STRATEGY A FACILE FABRICATE TO COATING SMART WITH SELF-HEALING SELF- AND REPORTING DUAL FUNCTIONS Shusheng Chen Hong Kong University of Science onBase hexamethylene anddiisocyanate aggregation-induced emission luminogens, developedwe a facile one-part strategy, microcapsules embedded approach, a fabricate to smart coating autonomous with self-healing and self-reporting dual functions. , , Rafael , Tokyo , Tokyo

2207 Computational and finite element methods Meeting room 211 room Meeting 2207-1 NUMERICAL OF SIMULATION TRANSVERSECFRP FAILURE CONSIDERING NON-LINEAR VISCOELASTIC/ PLASTIC CONSTITUTIVE WITH EQUATION ENTROPY DAMAGE Mio Sato University of Science proposedThe model can express strain the of and creep behavior recovery process. In analysis,numerical A FORTRAN is program introduce to created a proposed nonlinear modelviscoelastic into resin. matrix 2207-3 FINITE ELEMENT MODELLING OF UNIT CELLS APPLIED TO PROBLEMS OF FINITE DEFORMATION Elena Sitnikova University of Nottingham of UCs Formulation previously established involving for problems was strains small and extendedadapted coverto cases geometricinvolving A nonlinearity. in drawback major finite deformation in FE codesformulation been exposed.have 2207-2 OF SIMULATION PROGRESIVE IN OPEN- DAMAGE COMPOSITEHOLE SPECIMENS: NUMERICAL INVESTIGATION Ofir Shor Advanced Defense Systems Ltd of response tensile The and[0/45/90/-45]2s [30/60/90/-60/-30]2s carbon/ IM7/977-3 epoxy open-hole coupons simulated is two numerical using approaches. , , , North

2206 Scott White symposium Meeting room 210 room Meeting 2206-1 EVOLUTION OF MULTIFUNCTIONAL MICROVASCULAR COMPOSITES Patrick Jason CarolinaState University 2206-3 PROCESSING LCM OF SELF-HEALING REINFORCEDFIBER COMPOSITES Michaud Veronique Epfl an overview is This of on our research self-healing structural long fiber reinforced composites, early from DCPD- with attempts Grubbs capsules, containing EPA to capsules, recent to on healable work composites on based blends. 2206-2 VOID MODELING FORMATION GROWTHAND MECHANISMS IN COMPOSITE PROCESSING Suresh Advani University of Delaware be will on focus The prediction of voids co-cure the during of honeycomb structures sandwich . in an autoclave Process models that describe face the sheet consolidation, adhesive bond line fillet bond and formation line porosity the during co-cure process be will presented. , , , The

2205 Advanced and manufacturing automation Meeting room 209 room Meeting 2205-1 INVESTIGATION ON THE MELTING OF THE WELD IN INTERFACE CONTINUOUS ULTRASONIC OF WELDING THERMOPLASTIC COMPOSITES Jongbloed Bram Delft University of Technology ultrasonic Continuous a new is welding high-speedpromising joining technique for thermoplastic composites. study This the relating at aims time welding optimum the to welding in static welding continuous speed. 2205-3 EFFECTS OF ENVIRONMENTAL CONDITIONS ON DEFECT FORMATION DURING AUTOCLAVE PROCESSING Christian Netzel Center for Advanced Composite Materials paper investigates This effectthe relative of humidity and on temperature prepreg uncured that characteristics, the to linked are qualityconsolidation of L-shaped parts during processing. autoclave 2205-2 CURVING PLY TERMINATION: SUPPRESSING DELAMINATION IN TAPERED COMPOSITES Shu Minakuchi University of Tokyo is Fiber orientation locallyat changed end of pliesterminal suppress stressto the at concentration ply edges. Suppression of delamination in composite ply drop-off and free- edge delamination successfullyis demonstrated. , - , Ecole , Tokyo , Tokyo

2204 Liquidcomposites moulding Meeting room 208 room Meeting Gyeongsang National University 2204-1 CURING BEHAVIOR OF ENDO-DICY CLOPENTADIENE DECELERATOR AND EFFECTSSOLUTION Choi Sung Woong 2204-3 A NEW SCALABLE METHODOLOGY PREDICT TO PERMEABILITY OF DEFORMED TEXTILES UNDER COMPRESSION Simone Bancora - Gem Nantes Centrale propose a We new method for mesoscalethe of areconstruction textile geometry based and on simple visual mechanical data acquisition by means of a pressure-sensitive film. 2204-2 EFFECT OF WETTABILITY ON MACROVOID IN FORMATION VISCOUS-FLUID IMPREGNATION FIBER WOVEN TO BUNDLES Yoshihara Kota University of Science Effect investigate We of wettability on formation macrovoid in viscous-fluid to impregnation fiberwoven bundles method by in VARTM research. experimental , Zhejiang , Beijing Institute , Beijing Institute , Harbin Institute , Harbin Institute

2203 Meta-composite Meeting room 206 room Meeting 2203-1 METACOMPOSITES ENABLED BY FERROMAGNETIC MICROWIRES Luo Yang University 2203-3 AND FABRICATION MECHANICAL PROPERTIES OF FIBER CARBON REINFORCED 3D AUXETIC CELLULAR STRUCTURES Li Ma of Technology 2203-2 WAVE BROADBAND POLARIZATION ENGINEERING WITH ANISOTROPIC ELASTIC METAMATERIAL Zhu Rui of Technology presentation This presents a design and realization experimental elastic of broadband which metamaterial can achieve complete mode separation wave well as and conversion unique negativeas reflection. , , , Luleå , Luleå

2202 Biocomposites 2202-1 PERCOLATED NETWORK OF BIOCARBON OF IN A BLEND 6 AND NYLON POLYPROPYLENE Amar Mohanty Bioproducts Discovery & Development Centre, Department of Plant Agriculture, Crop Science Building, University of Guelph foundBiocarbon was be selectivelyto in the distributed phase,nylon-6 in nylon-6/polypropylene due to blends similarities inthe effects The polarity. of and dispersion of the interaction biocarbon on thermal- mechanical properties systematicallywere studied. 2202-3 OF THE INFLUENCES ON SIZES PARTICLE OFPERFORMANCE BIODEGRADABLE PLASTICWOOD COMPOSITES MANUFACTURED FROM LINGO- CELLULOSIC AGRICULTURAL WASTE Nguyen Tung The Univeristy of Queensland objectiveThe of to was research this effects the evaluate of opening particle sizes and particle load performanceon the of wood plastic composites from made stalks cotton entire Biodegradable with polyhydroxyalkanoates (PHA) 2202-2 BIOMASS-DERIVED ELECTROSPUN CARBON NANOFIBER NETWORKS FOR HIGH- PERFORMANCE SUPERCAPACITORS Wei Jiayuan University of Technology High-performance carbon electrode for supercapacitors renewable derived from developed.lignin were electrodeThe materials were tested in both conventional two-electrode supercapacitors using liquid electrolyte as a solid-state as well supercapacitor. Meeting room 205 room Meeting -

- - - , - , - , National , National

Exhibition hall 2201 Nano-composites Coffee break 2201-1 MECHANICAL PROPERTIES OF PEEK/HALLOYSITE NANOTUBE COMPOSITES AT ELEVATED TEMPERATURES CallsenChristoph University of Bayreuth, Department of Polymer Engineering and fatigue Tensile propagation crack properties of PEEK/ HNT-nanocomposites beenhave at investigated temperatures. different ofA change reinforcingthe has mechanisms been detected when near are temperatures transition. glass the composite foam with carbon particles such carbonas black, graph eme and multi-walled carbon was nanotubes investigate to studied be relationship the tween foam formation decompositionduring of chemical blowing and crosslinkagent reaction of mol rubber ecules by sulphur. 2201-3 RE-FREE EXCHANGE COUPLED NANOCOMPOSITE MAGNETS Ovidiu Crisan for Materials Institute Physics Materials Engineering,Materials Faculty of Engineering, University,Burapha Thailand nano rubber Natural ICAL PROPERTYICAL OF RUBBER NATURAL NANOCOMPOSITE FOAM Charo Pollawat eythornkhajhornchai 2201-2 EFFECT OF CARBON TYPES- ON CURE BE - MORPHOL HAVIOR, MECHAN AND OGY Plenary 2 1110-1130 1110-1250 1040-1110 1150-1210 1130-1150 TUESDAY 13 AUGUST TUESDAY Time

SCIENTIFIC PROGRAM 46 SCIENTIFIC PROGRAM SCIENTIFIC 49 Fill Gesellschaft industry session Meeting room 219 room Meeting Fill Gesellschaft Fill Gesellschaft industry session only *invitation event* “4 X 4 STRATEGY” FOR- BASE AUTOMATION IN COMPOSITE MANUFACTURING Wilhelm Rupertsberger by Sponsored - - , , Unist , Seoul

P2314 Dynamic properties & fracture Meeting room 218 room Meeting 2214-5 FIRE POST AND FIRE PROPERTIES OF GLASS FIBER REINFORCED AND EPOXY POLYCARBONATE COMPOSITE: A COMPARATIVE STUDY Yousof Ghazzawi University of Queensland 2214-4 FIBER LONG MOLDING SPRAY-UP OF OPTIMIZATION GLASSCHOPPED REINFORCEDFIBER POLYDICYCLOPEN COMPOS TADIENE ITES Ji Ho Jeon UniversityNational Long FiberUsing molding Spray-up process fabricate to chopped GF/p-DCPD composites P2314-1 P2314-1 DEPENDENT RATE RESPONSE TENSILE OF A PLAIN TEXTILEWEAVE COMPOSITE Choi Taeseong dependent rate The of thebehavior polymer textile and the composite been has experimentally studied. experiment,From it is rate the concluded that ofdependent behavior compositethe material mainly determinedis material. by matrix the , , Carl , Australian , Australian

P2313 Smart composite structures Meeting room 217 room Meeting 2213-4 3D MULTISCALE OF INVESTIGATION ANGLE- IN DAMAGE INTERLOCKED MATRIX CERAMIC UNDERCOMPOSITE IN SITU LOADING Hrishikesh Bale Zeiss Microscopy Inc. here, present We test tensile in-situ results collected on x-ray a laboratory microscope which the demonstrate advantagesand capabilities of non- destructive testing of CMCs. Comparing consecutive 3D volumes the from digital test using in-situ volume correlation, fields canlocal strain be in 3D. evaluated 2213-5 ACCOUNTING FOR FRICTION IN UNDER CRACKS COMPRESSION SHEAR INAND ANISOTROPIC AN MODEL DAMAGE APPLICATION AND CMCS TO Emmanuel Baranger ENS Paris-saclay, LMT, CNRS, Université Paris- saclay An extension of an damage anisotropic theory proposed is for CMCs. Several complex mechanisms cracking to related described:are crack closure, friction, a priori damage unknown directions, non- proportional loadings. P2313-1 ANDHARMONIC TRANSIENT DYNAMIC OF A RESPONSE LAMINATED SMART STEPPED BEAMCOMPOSITE Saeed Fazeli UniversityNational , , Robert , Defence

P2312 Textile-based composites Meeting room 216 room Meeting 2212-4 FLOW A LOW-COST FRONT MONITORING SYSTEM Andreas Damm Bosch GmbH work, this In a MEMS networksensor is embedded in a textile detectto flow the of a resin transfer front molding process. Both acceleration and temperature and validated is data an applied to afterwards existing setup. 2212-5 CHARACTERISATION OF FIBRE REINFORCED COMPOSITES USING HIGH RESOLUTION DISTRIBUTED FIBRE OPTIC SENSORS Claire Davis Science and Technology Group paper describesThis an experimental the into investigation fibre ofuse continuous detect to and gratings material characterise inhomogeneity and in a range damage of fibre reinforced composite specimens. P2312-1 BEHAVIOR FATIGUE OF UN-NOTCHED NOTCHED AND 3D BRAIDED COMPOSITES Shuangqiang Liang University of British Coulmbia , , Rmit

P2311 Non-destructive evaluation Meeting room 215 room Meeting 2211-4 SELF- TOWARDS HEALING AND SELF-SENSING OPTICAL USING IN WAVEGUIDES MICROVASCULAR COMPOSITES William Martin North Carolina State University P2311-1 P2311-1 THERMOELASTIC ASSESSMENT OF COMPOSITE DELAMINATION BUCKLING Cedric Antolis University coupon A laminate containing an artificial is delamination subjected uniaxial to compressive loads induce localisedto buckling delamination and examined with stress thermoelastic analysis (TSA) low-cost using microbolometer technology. imaging , ETH, , American , U. S. Air Force

P2310 Civil and engineering composite materials: impact to route Meeting room 214 room Meeting 2210-4 4D PRINTING OF MULTIFUNCTIONAL MATERIALS Sampada Bodkhe Zurich serves3D printing an essentialas tool fabricating towards implantscustomized individual to catering needs. implant Where materials must stringent to conform compatibility norms, adding a different for each material function entails cumbersome and expensive testing, same time the and at and risk the increase discomfort user. the to 2210-5 GRADIENT MATERIALS FOR INTERFACE SENSOR HIGH-TEMP MODULES Ajit Roy LaboratoryResearch P2310-1 P2310-1 OF GFRP BEHAVIOR BARS SUBJECTED DYNAMIC TO LOADING AbedFarid University of Sharjah paper studiesThe of behavior GFRPthe bars under impact drop the loading using test.hammer tests The conducted onwere GFRP specimens with at diameters different loading rates. various , , Tay, National National Tay, Altair industry session Meeting room 213 room Meeting 2209-4 AN ENERGY- RATE-APPROACH FOR OPTIMIZED FREQUENCY FORSELECTION REPRODUCIBLE FATIGUE ASSESSMENT OF COMPOSITES Daniel Hülsbusch TU Dortmund University, Department of Test Materials Engineering (WPT) 2209-5 AN ADAPTIVE DISCRETE- SMEARED CRACK MODEL (A-DISC) Tong-Earn University of Singapore Altair industryAltair session RESEARCH MEETS - PRACTICE HOLISTIC ALTAIR’S APPROACH FOR THE COMPOSITE DESIGN, AND SIMULATION OPTIMISATION PROCESS Palanterä Markku ofDirector Global Composites Business Development by Sponsored - - - , - - , Kolon , The

P2308 Composite structures Meeting room 212 room Meeting 2208-4 VAPOR SOL-GEL TO MODIFICATION DEVELOP DURABLE SUPERHYDRO MICRO PHOBIC FOR CAPSULES SELF-CLEANING APPLICATION Luo Wenjun Hong Kong University of Science and Technology ap A well-established achieve to theproach self-clean long-lasting ing performance in synthetic mate coating incorporation the is rial of polymer-based microcapsules (MCs) double-layeredwith contain a that shells hydrophobicity agent polymer the into matrix. 2208-5 CYCLIC NOVEL OLEFIN COPOLYMER/ BLEND EPOXY FOR THERMAL OFMENDING IN CARBON EPOXY REINFORCEDFIBER COMPOSITES MahmoodHaroon University of Trento P2308-1 P2308-1 STIFFENED COMPOSITE RESIN BY PARTS PROCESSINFUSION FOR AIRCRAFT APPLICATION Oyoung Choi Dacc Composite

, , , University

P2307 Joints Meeting room 211 room Meeting 2207-4 A FINITE ELEMENT FORMODEL DISCONTINUOUS RANDOMLY- AND ORIENTED STRAND THERMOPLASTIC CFRP Sumiyama Takuya Center,Research CO.,TOYOBO LTD. objectiveThe of this propose a to is study simple finite element (FE) model without of the consideration of strands shape As results the explicitly. of FE analysis, the mechanical flexural agreed wellbehavior experimentalwith results for a variety of specimen. 2207-5 A DYNAMIC ELEMENT SPRING FORMODEL THE OFPREDICTION LONGITUDINAL OF FAILURE POLYMER COMPOSITES Rodrigo Tavares Faculty of Engineering of University of Porto A dynamic spring element model used is failure tensile study to in polymer composites and understand the processfibre clustering damage and the driving mechanisms failure. P2307-1 INVESTIGATION OF GEOMETRICAL COMPOSITEAND MATERIAL PARAMETERS FOR TENSION- BOLTED ABSORBING JOINTS HassanJazib of Limerick Development of a novel composite bolted namely, joint tension-absorbing joint, enhances that crashworthiness the of lightweight structure transportation bolt the by avoiding the and allow fracture extensive of crushing compositethe material. , Northwestern

P2306 and damage Fracture Meeting room 210 room Meeting 2206-4 SIMULTANEOUS IMPROVEMENTS AND OF STRENGTH INTOUGHNESS TOPOLOGICALLY INTERLOCKED CERAMICS , Mirkhalaf Mohammad The University of Sydney P2306-1 P2306-1 DUCTILE-BRITTLE FRACTURE OF SIMULATION IN-SITU TIB2/AL COMPOSITE Ma Yifan Polytechnical University microstructural The and characteristics mechanisms fracture TiB2/2024of in-situ composite were plastic The studied. properties of the obtained were matrix by reverse analysis. and damage The was behaviors fracture simulated. , , Shinshu

, RMIT University P2305 harvestingEnergy and storage Meeting room 209 room Meeting Hamburg UniversityHamburg of Technology compares work This conceptstwo control for automated honeycomb potting quality, to regard with repeatability and Potting stability. been has pressure be key the found to value. target 2205-4 TO DAMAGE FIBRESCARBON DURING RADIAL BRAIDING Jacquelynn Ting Xue Tian investigated We effectsthe theof radial automated processbraiding on the damage, shape, tensile and stiffnessstrength of carbon fibre tows. 2205-5 HIGH QUALITY AUTOMATED HONEYCOMB POTTING WITH PRESSUREACTIVE CONTROL Martin Harnisch P2305-1 MULTIFUNCTIONAL COMPOSITES FOR ENERGY HARVESTING Xiaoyu Guan University a prepare We multifunctional flexible nanofiber composite both has which piezoelectric and shape memory effect.This for an advantage is ofapplications energy harvesting in complex structures. - - , , Australian , Australian

P2304 Design and for manufacture multifunctionality ofand machining composites Meeting room 208 room Meeting 2204-4 EXPERIMENTAL DESCRIPTION OF DRAPING EFFECTS AND INFLUENCE THEIR ON STRUCTUAL OF BEHAVIOR REINFORCEDFIBER COMPOSITES Eckart Kunze Universität Technische Dresden - Institute of Lightweight Engineering and Polymer Technology ofComparison experimentally draping determined effects waviness(fiber and transverse shows compression) good with agreement simulation. draping simulation Structural results of specimen waviness with confirmed observed during failure mechanical testing. P2304-1 SUPERHYDROPHO FOR COATINGS BIC FIBRE ENHANCED - MATE COMPOSITE RIALS Puneet Garg UniversityNational polyPolyurethane methacrylate)(methyl interpenetrating polymer network and FSiO2 coatings fabricate to used were fibersuperhydrophobic reinforced composites. These fabricated coated substrates mate dewetting with reduced showed rial as absorption water uncoatedcompared to substrates. - , - - , , Pusan

P2303 structures Sandwich and materials Meeting room 206 room Meeting tion of impact pDCPD property cryogenic at and effect temperature of amount decelator National University National evalua Performance 2203-5 IMPACT CRYOGENIC PROPERTIES OF GLASS REINFORCED POLY-DICYCLOPEN COMPOS TADIENE ITES Jongmin Choi 2203-4 MECHANICAL PROPERTIES OF CHIRAL3D CROSS STRUCTURES VIA SELECTED LASER SINTERING Wang Qingsong Beihang University CompressiveThe mechanical properties of 3D cross chiral are structures the with investigated help of experiments, simulations numerical and theoretical analysis. University of Southern Queensland P2303-1 P2303-1 VELOCITYLOW RESPONSE IMPACT OF CORRUGATED CORE SANDWICH - EFFECT PANELS OF IMPACTOR GEOMETRY Epaarachchi Jayantha

, University of P2302 tolerance Damage creep durability, and aggressive environment P2302-1 P2302-1 MULTI-MODE VIBRATION DETECTION FOR DELAMINATION FIBRE OF CARBON PLATE COMPOSITE Jie Pu Chester Meeting room 205 room Meeting

, , Harbin Institute of Technology , Harbin Institute , DMTC Program Leader and Associate and , DMTC Leader Program Professor School the from of and Mining Mechanical Engineering University the at of Queensland , Tongji , Tongji

Jinsong Leng Jinsong DMTC lunch symposium - The potential for composite materials to achieve technology breakthroughs across the Australian defence sector and its Australian the across technology breakthroughs achieve to composite materials for lunch symposium - The potential DMTC chains. supply industrial Martin Veidt Plenary 2 APPLICATIONS BIOMEDICAL TO FROM COMPOSITES 4D PRINTING THE AEROSPACE TECHNOLOGIES: AND PLENARY LECTURE: MEMORY POLYMER SHAPE Plenary 2 sessions concurrent to Move P2301 and polymerCeramic compositesmatrix Queen’s UniversityQueen’s Belfast 2201-5 EFFECT OF CARBON BULKNANOTUBE ON MORPHOLOGY THE INTERLAMINAR FRACTURE OFTOUGHNESS LAMINATES CFRP Stephen C. Hawkins 2201-4 AND STRENGTHEND EPOXY TOUGHENED NANOCOMPOSITES Hongbo Gu Univerisity P2301-1 P2301-1 RESEARCH ON DEFECTS WAVES WINDING OF TAPE RESIN MATRIX COMPOSITES Xiaojingg, Wan Aerospace Research of & Materials Institute Processing Technology rate the Decreasing of heating, increasing of temperature the point,pressured and method bandage the without longitudinal fold can reduce waves. Lunch Exhibition hall Plenary 2 1445-1450 1210-1230 1350-1435 1435-1445 1445-1535 TUESDAY 13 AUGUST TUESDAY 1250-1350 1300-1345 1230-1250 Time

SCIENTIFIC PROGRAM 48 SCIENTIFIC PROGRAM SCIENTIFIC 51 Meeting room 219 room Meeting Fill Gesellschaft Fill Gesellschaft industry session only *invitation event* “4 X 4 STRATEGY” FOR- BASE AUTOMATION IN COMPOSITE MANUFACTURING Wilhelm Rupertsberger by Sponsored CONTINUED , , , Harbin Meeting room 218 room Meeting P2314-4 P2314-4 NUMERICAL OF SIMULATION IMPACT HAIL CHARACTERISTICS OF GLASS FIBER LAMINATES Xiaojun Yan Engineering University P2314-3 P2314-3 MODE II INTERLAMINAR FRACTURE BEHAVIOR OF ZANCHOR REINFORCED COMPOSITE UNDER LAMINATES LOW-VELOCITY LOADING IMPACT Sugimoto Wataru Ritsumeikan University mode the study, this In II impact fracture of thebehavior Zanchor composites experimentally was determine to studied effectivenessthe theof Zanchor reinforcement high loading rates. at P2314-2 P2314-2 EFFECTOF INTERMEDIATE ON STRAIN RATES SHEAR PLUGGING OF STRENGTH COMPOSITES ChoudhurySantanu of Indian Institute Bombay Technology and E glass/epoxy Carbon/epoxy composite laminates using prepared were technique VARTM the a UTM, in and tested at intermediate different for their rates, strain pluggingshear strengths. , Beihang , Harbin , Harbin Meeting room 217 room Meeting P2313-4 P2313-4 LASER INDUCED GRAPHENE ENABLED PAPERS FUNCTIONAL COMPOSITES FOR LIQUID MONITORING Wang Yanan University Laser induced paper based graphene was array liquid sensor the monitor applied to location of composite threatened is which organic by harmful solvents P2313-2 AND PREPARATION CHARACTERIZATION OF THE RADIATION CROSSLINKED MEMORY SHAPE EVA/HDPE LiangWei of Technology Institute HDPE paper, this In (high density polyethylene) and EVA (ethylene-vinyl acetate) raw the used as are prepare to materials memorya shape polymer and it has characteristics great memoryof shape gassingand space performance. P2313-3 A MORPHING WINGTIP STRUCTURE Jian Sun of Technology Institute describe a We wingletmorphing concept based which on active inflatable honeycombs and Shape Memory CompositePolymer (SMPC) in this skins work. , , UNSW r, Universityr, Meeting room 216 room Meeting Swinburne UniversitySwinburne of Technology P2312-2 PROPERTIES IMPACT OF HELICOIDAL STRUCTURE OF CARBON/EPOXY COMPOSITES PeerzadaMazhar P2312-3 RECONSTRUCTION OF MESOSCALE TEXTILE COMPOSITES USING &MICRO-CT IMAGE COMPUTER VISION ALGORITHM Congyuan Tao Sydney P2312-4 DEVELOPMENT OF DRAPING A FAST USING ALGORITHM MULTIFACTORIAL SHEAR LOCAL SIMULATIONS HoffeJacob of Ottawa , , , Meeting room 215 room Meeting P2311-2 P2311-2 AUTOMATED ANALYSIS IMAGE OF ULTRAFAST SYNCHROTRON TO CT SCANS EXPERIMENTALLY CHARACTERISE THE FIBREBREAK DEVELOPMENT DURING IN-SITU TESTS TENSILE Christian Breite Department of Engineering,Materials KU Leuven synchrotron By using to radiation perform µCT in-situ experiments combined InSegt the with fibre segmentation novelalgorithm 3D in the insight of structure micro composites under been load has tensile gained. P2311-3 SIMULTANEOUS MULTI-FREQUENCY DIELECTRIC OF THE ANALYSIS POLYMERIZATION PROCESS OF ANIONIC 6 POLYAMIDE Maximilian Eberhardt Igcv Fraunhofer of use aBy the new dielectric system measurement possibleit was to curing the monitor process of anionic polyamide-6 so far to unprecedented extend. P2311-4 PREDICTION EARLY OF CRACK DEVELOPMENT DIGITAL USING IMAGE CORRELATION Jesson David University of Surrey , Nihon , Matrix , Harbin Meeting room 214 room Meeting P2310-2 P2310-2 BEARINGRESIDUAL OF RC CAPACITY AFTERMEMBER EXPOSURE HIGH TO TEMPERATURE Lili Bai Engineering University P2310-3 IMPROVEMENT OF PENETRATION OF RESISTANCE CUREDAMINE RESIN FOREPOXY CONCRETE LINING ION EXCHANGE BY ZEOLITE UNDER SULFURIC ACID Sakai Tetsuya P2310-4 INTRODUCTIONAN SYNTACTIC TO – THREE FOAMS DIMENSIONAL COMPOSITE NETWORKS Jim Kingston Composites and Engineering Always Everything You Know About To Wanted Syntactic (*But Foams* Ask) To Afraid Were University study, this In ofimprovement resistancecorrosion of amine cured epoxy resin by zeolite additives under sulfuric was acid environment investigated. , Meeting room 213 room Meeting Altair industryAltair session RESEARCH MEETS - PRACTICE HOLISTIC ALTAIR’S APPROACHFOR THE COMPOSITE DESIGN, AND SIMULATION OPTIMISATION PROCESS Palanterä Markku ofDirector Global Composites Business Development by Sponsored CONTINUED , , , Nanjing Meeting room 212 room Meeting P2308-2 P2308-2 THE ENERGY- ABSORBING CHARACTERISTICS OF COMPOSITE TUBE-REINFORCED ALUMINUM UNDER FOAMS COMPRESSION Zheng Liu University of Science and Technology paper investigates This energy-absorbingthe of characteristics foams aluminum containing embedded carbon fibre reinforced epoxy tubes by quasi- compressionstatic tests. P2308-3 ON THESTUDY PROPERTY OF LIGHTWEIGHT BUILDING STRUCTURE Comfort Mensah Harbin Engineering University P2308-4 EFFECT OF LAYER INTERFACE DISLOCATION AND ON TANDEM HONEYCOMB MECHANICAL PROPERTY Hangjian Weng Jiaotong Shanghai University Research of influence of factor tandem honeycomb compressive property, for example, single layer dislocation, height in double layer tandem honeycomb, in a number and layer specific height. core , Japan , Toray , Toray , Paderborn Meeting room 211 room Meeting Aerospace Exploration Agency silica depositionThe realized high treatment for adhesion strength adhesively-single lap bonded joints and test piecescoating that to comparable conventional with treatment. P2307-4 JOINING AUXILIARY WITHELEMENT PIN INTEGRATED STRUCTURES FOR MECHANICAL JOINING OF FIBER- REINFORCED PLASTIC/METAL COMBINATIONS Per Heyser University research This project the shows development of a novel auxiliary joining integrated element with in pin structures the increase to order capacityload-bearing of mechanically joined plastic/ fiber-reinforced metal combinations. P2307-2 MECHANICAL ANALYSIS FOR WELDING OF TECHNOLOGY THERMOSET FRP Honma Masato P2307-3 DEPOSITION SILICA TREATMENT FOR IMPROVING ADHESION PROPERTIES OF BONDINGADHESIVE OF OR COATING AIRCRAFTS Yasuoka Tetsuo Industries, Inc. Performed andexperimental analysis fornumerical and a new material processing concept by of use Thermosetthe and Thermoplastic for CFRP multi-material bonded structure. , , Afrl , Harbin Meeting room 210 room Meeting P2306-4 P2306-4 EFFECTSIZE AND INTRALAMINAR FRACTURE OFTOUGHNESS FIBRE REINFORCED COMPOSITES Giuseppe Catalanotti UniversityQueen’s Belfast P2306-2 P2306-2 EVOLUTION OF FRACTURE PARAMETERS IN OF A CRACK A MICROPOLAR ELASTIC SOLID Hongjun Yu of Technology Institute P2306-3 A PRELIMINARY ASSESSMENT OF A NEW XFEM FRAMEWORK FOR PREDICTING COMPLEX FRACTURE BallardKeith , , Tokyo , Tokyo , Chonbuk Meeting room 209 room Meeting P2305-4 DEVELOPMENT NANO- OF SIC PARTICLE/MG2SI THERMOELECTRIC COMPOSITES Nakano Junki University of Science fabricated We SiC intragranular nano-particle/Mg2Si composites by sintering toughness improve to without reducing thermoelectric properties. As a result, intragranular composites have a positive effect on mechanical and thermoelectric properties. P2305-2 P2305-2 A REVIEW OF MULTIFUNCTIONAL COMPOSITE STRUCTURES WITH EMBEDDED LITHIUM-ION BATTERIES Pattarakunnan Koranat RMIT University P2305-3 ORGANIC FRAMEWORK DERIVED ULTRA- THIN COBALT IRON SULFIDE NANOSHEET FOR HIGH- ARRAYS PERFORMANCE SUPERCAPACITORS Lee Won Jae University National to A novel strategy simple andestablish cost-effectiveternary metal sulfide-based electrodes for and portablehybrid electronics.

, , RMIT RMIT , , Tongji , Tongji Meeting room 208 room Meeting P2304-4 OF FIBER DESIGN FORPREFORMS LARGESTWORLD’S FIBERGLASS COMPANY Peng Li University on Bridging Based Model and classical the theory, laminate predicted of values propertiesfiber fabric’s can pretty agree well experimental the with values. P2304-2 ELECTRONIC CIRCUITS INTO EMBEDDED COMPOSITE AEROSPACE MATERIALS Greg Beziuk University paper presentsThis a concept demonstrator for embedding a complex multi-layer frequency radio 4-way (RF) network switching an aerospace into composite material. P2304-3 MECHANICAL PROPERTY OF A CUBIC CORE-FILLED CREATED MODEL 3D PRINTING BY TECHNIQUE Jeongho Choi UniversityKyungnam on paper focus is This finding mechanical properties for hyper modelcubic by made direct metal3D printing (DMLS) sintering laser technique. Applied AlSi10Mg is material typepowder the with DMLS. , , Baylor i, Shanghai Jiaoi, Shanghai Meeting room 206 room Meeting P2303-4 P2303-4 FLEXURAL OF BEHAVIOUR COREDFOAM SANDWICH STRUCTURES WITH THROUGH- THICKNESS REINFORCEMENTS Ghilane Bragagnolo University of Surrey Experimental and study numerical of sandwich CFRP with panels through-thickness reinforcements under three-point bending. of Investigation modesfailure and debondingskin-core propagation. P2303-3 P2303-3 DAMAGE INPREDICTION QUASI-STATICALLY INDENTED SANDWICH COMPOSITE STRUCTURES USING A TWO-REGION MODEL PLATE Abhendra Singh University A model developed is for predicting depth, indentation and planar diameter area delamination sheet, face for thin honeycomb core compositessandwich subject quasi-static to loading. indentation P2303-2 P2303-2 NONLINEAR LOW-VELOCITY RESPONSE IMPACT OF SANDWICH BEAMS WITH FUNCTIONALLY GRADED NEGATIVE RATIO POISSON’S HONEYCOMB CORE Chong L University Tong Results revealed that can NPR core the remarkably reduce the thickness decrease beamsof sandwich subjected out-of- to impact,plane and the willFG configurations distinctly influence the impactresponse. , , , Beihang P2302-4 P2302-4 ATOMISTIC AN OF CREEP STUDY DEFORMATION IN FIBER/MATRIX INTERFACE Tam Lik-ho University Nanjing University of Aeronautics and Astronautics P2302-3 P2302-3 OF INFLUENCE DENT DEFECTS ON THE COMPRESSIVE OF STRENGTH COMPOSITE LAMINATES Wang Yuequan P2302-2 COMPARATIVE ONSTUDY THE DAMAGE OF TOLERANCE THERMOSET AND THERMOPLASTIC GLASS FIBER- REINFORCED COMPOSITES SchimmerFlorian for CompositeInstitute Materials study This experimentally compares damage the of quasi- tolerance GFRP plates isotropic an eopxywith and a polyamide66 matrix loading under LVI respecting different conditioning states before and during impacttesting. Meeting room 205 room Meeting

, , , Applied P2301-4 P2301-4 ELECTRICAL, AND THERMAL MECHANICAL PROPERTIES OF THERMOPLASTIC ELASTOMER COMPOSITES CONTAINING FILLERS CARBON Rajesh Theravalappil King University Fahd of Petroleum and Minerals and conductingSoft composites of ethylene-octene copolymers using carbon fillers were Electrical/ prepared. conductivitiesthermal and mechanical properties found improved without compromising hardness.increasing They can find as applications pressure/strain sensors. P2301-3 P2301-3 MACROSCOPIC MICROSCOPIC AND PROPERTIES OF RUBBERFABRIC COMPOSITE Xuefeng Yao Mechanics Laboratory, Department of Engineering Mechanics, University Tsinghua rubberComplex fabric composites with high-performance and special material widely inare used their due to aerospace excellent mechanical and sealing properties, of consist which material matrix the and the rubber with material reinforcement fabric. the with P2301-2 P2301-2 PHTHALONITRILE MODIFIED MULTI-HYDROXYL PHENOLIC: CURING SYNTHESIS, PROPERTIES AND Shuangshuang Xu of AerospaceInstitute andMaterials Processing Multi-hydroxyl phenolic with phthalonitrile different degreesubstitution The prepared. was chemical structure, behaviour, curing processability and stabilitythermal were studied. Plenary 2 1450-1455 1455-1500 TUESDAY 13 AUGUST TUESDAY 1500-1505 Time

SCIENTIFIC PROGRAM 50 SCIENTIFIC PROGRAM SCIENTIFIC 53 Meeting room 219 room Meeting Fill Gesellschaft Fill Gesellschaft industry session only *invitation event* “4 X 4 STRATEGY” FOR- BASE AUTOMATION IN COMPOSITE MANUFACTURING Wilhelm Rupertsberger by Sponsored CONTINUED , German Meeting room 218 room Meeting P2314-5 P2314-5 THE IMPROVING MATERIAL DYNAMIC CHARACTERISATION OF CARBON/EPOXY COMPOSITES AT INTERMEDIATE STRAIN RATES Yoo Sanghyun Aerospace Center (DLR) Experimental dynamic of investigations carbon/epoxy composites are performed at strain intermediate an using rates improved load techniqueintroduction in a high-speed servo-hydraulic testing machine. , , Tongji , Tongji , Meeting room 217 room Meeting University interfacialThe properties of wire SMA indented at and resin matrix temperature room which studied, were provided reference for engineering application. P2313-5 P2313-5 OF ANALYSIS INTERFACE AND STRENGTH MODE OF FAILURE INDENTED SMA COMPOSITESWIRE Zhu Tongzhou P2313-6 AN MODELLING NOL IMPROVED A RING TEST USING VOLUME REDUCED METHOD FOR THE CHARACTERISATION OF COMPOSITE CYLINDERS WidjajaMartinus Putra Für Bundesanstalt Materialforschung Und (bam)-prüfung ReducedThe Volume Method (RVM) the that shown has fibremultiscale break model can be used A efficiently. more been has comparison the ensure done to ofapplication this method. P2313-7 AND FABRICATION HYDROPHILIC CHARACTERIZATION OF NANOPARTICLES- POLYMER FILLED COMPOSITES Hanzawa Yuki School ofGraduate Materials Organic Science, Yamagata University hydrophilic The property of oxide nanoparticle wes Increasing evaluated. ofamount SiO2 in PMMA composite improved the propertyhydrophilic reducingwith the contact angle but thedecreased transmittance , , Beihang , IIT Bombay Meeting room 216 room Meeting P2312-5 P2312-5 STUDY NUMERICAL ON MECHANICAL PROPERTIES INFLUENCING IMPACT BALLISTIC OF BEHAVIOR FABRICS WOVEN CONSTANT USING TOUGHNESS APPROACH Sagar Ingle Results that indicate low with material modulus longitudinal strain and high failure bestis for combination projectilemaximum absorption.Alsoenergy fabrics woven all the show under study in energy increase in (decrease absorption residual velocity) with in interlayer increase coefficient of friction certainupto threshold energy that after value decreases.absorption P2312-6 BUCKLING PROPERTY OF PLAIN WEAVE COMPOSITE FABRIC LAMINATE CONSIDERING INTRALAMINAR INHOMOGENEITY Sugiyama Kazushi of Institute Kanazawa Technology propertyBuckling of fabric weave plain composite laminate investigated is intralaminar considering inhomogeneity caused structure by weave the yarns. of constituent P2312-7 EFFECT OF ON TACKIFICATION SHEARIN-PLANE OF BEHAVIOURS WOVEN BIAXIAL IN BIAS FABRICS EXTENSION TEST Zhao Xiaoran University shear in-plane The ofbehaviours tackified investigated were fabric Based thoroughly. andon experimental results,numerical a Deformation Gradul proposed. Model was - - - - - , , Faser ,

Meeting room 215 room Meeting IC TESTING Michael Koerdt e. Bremen institut V. for prepara Methods tion and characteri ofzation porosity and in com delaminations posites presented, are can help towhich for a mock-up realize wave guided ultrasonic testing accepted by industry. aircraft the P2311-5 P2311-5 FABRICATION - CHARAC AND OF TERIZATION DISCONTINUITIES IN AIRCRAFT COMPOSITES AS REFERENCE FLAWS FOR GUIDED WAVE ULTRASON BASED P2311-6 MEASUREMENT OF MOISTURE DIFFUSION OFCOEFFICIENT USING WOOD TERAHERTZ WAVE Oh Gyung-hwan UniversityHanyang diffusion Moisture process wood in balsa investigated was an image through terahertzusing technique. The betweenrelationship intensity pulse THz the content and moisture quantitatively was defined. P2311-7 INVESTIGATION OF DELAMINATED COMPOSITES BY DIC METHODS AE AND Hliva Viktor Department of Polymer Engineering, UniversityBudapest and of Technology Economics location ofThe the zone delaminated clearly identifiedwas field and strain in the resultsthe correlated AE the with well localization results. , , Deakin , Korea Meeting room 214 room Meeting P2310-5 P2310-5 OF EVALUATION THERMOELECTRIC PROPERTIES OF GRAPHENE- ENABLED REINFORCED POLYMER COMPOSITES: A PROFICIENT TOWARDS MOVE ADVANCED STRUCTURAL APPLICATIONS Azadeh Mirabedini UniversitySwinburne of Technology P2310-6 ON HEAT A STUDY EFFECTTRANSFER SINK OF HEAT FOR DIFFERENT COMPOSITE MATERIALS Meehye Oh Automotive Technology Institute P2310-7 UNDERSTANDING STRESSRESIDUAL CURED IN RAPIDLY FIBRE CARBON REINFORCED COMPOSITE Saman Ghadi University research, this In residual stress in carbon fast-curing fibre composite, which in hurdle a major is manufacturing the process been has by preciseinvestigated ofmeasurements temperature. stress-free , Meeting room 213 room Meeting Altair industryAltair session RESEARCH MEETS - PRACTICE HOLISTIC ALTAIR’S APPROACHFOR THE COMPOSITE DESIGN, AND SIMULATION OPTIMISATION PROCESS Palanterä Markku ofDirector Global Composites Business Development by Sponsored CONTINUED , , , Indian Meeting room 212 room Meeting P2308-5 P2308-5 THERMO- MECHANICAL OF BEHAVIOUR MICROWAVE- CURED CARBON NANOTUBES- POLYMER BASED COMPOSITES Arora Gaurav of Technology Institute (IIT) Mandi work present The effect the investigates on the of temperature modulus and elastic toughness offracture microwave-cured the carbon nanotubes polymer based (CNTs) composites. P2308-6 TTT CURE DIAGRAM FOR AMBIENT AN TEMPERATURE CURING EPOXY- THERMOSETAMINE Shanelle Fernando University of Queensland P2308-7 DETERMINATION OF MODE II INTERLAMINAR FRACTURE TOUGHNESS OF ENHANCEMENT UNIDIRECTIONAL FIBER- CARBON REINFORCED MATRIX COMPOSITES WITH GRAPHENE MULTI- AND CARBON WALLED NANOTUBES Nongyue Gao Northwestern Polytechnical University Carbon fibre-reinforced composites nano with MWCNTs materials, and graphene, used as are which canreinforced agent obtain an obvious toughness fracture under anenhancement adding densityoptimal of 1.0g/m2. , Korea , Shanghai , Shanghai , Academy Meeting room 211 room Meeting University effectThe surface of roughness on the life offatigue carbon steel-CFRP joints was lower The studied. surface roughness fatigue the increases life same under the stress level. P2307-7 AXIAL TENSILE ADHESIVELY BONDED PERFORMANCE WOUNDOF CFRP TUBESCOMPOSITE UNDER ROOM- AND TEMPERATURE LOW-TEMPERATURE CIRCULATION Haibo Luo of Opto-electronics, Chinese Academy of Sciences P2307-5 P2307-5 ONA STUDY THE FATIGUE CHARACTERISTICS LAPOF SINGLE JOINT BETWEEN FIBER CARBON REINFORCED PLASTIC/CARBON STEEL Kang Byunghyun P2307-6 TENSILE PROPERTIES OF STITCHED 3D-WOVEN- COMPOSITES/ SINGLE- TITANIUM LAP JOINT Lu Yi-rong University Tong Jiao effectThe of several parameter stitch of the on strength composites/3D-woven titanium single-lap joint in this presented is Performance paper. was of sutures the observed the during failure the show test to mechanism. , , Korea , Meeting room 210 room Meeting P2306-7 P2306-7 DIC DEFORMATION MEASUREMENT IN CRACKED CFRP CROSS-PLY LAMINATES FikryM.j. Mohammad University ofTokyo Science Digital Image (DIC) Correlation method employed is strain the measure to the at distribution macroscopic level test, a tensile during to CFRP cross- a cracked ply laminates. P2306-5 P2306-5 EFFECT OF CARBON NANOTUBE CONTENTS ON FRACTURE PROPERTIES OF THERMALLY DEGRADED NANOCOMPOSITE VIA THE FILMS ESSENTIAL WORK OF FRACTURE TEST Min-Seok Choi University A final goal of this construct to is study an underbody shield essential is which protect a batteryto adequatepack with Asplastic. basic study, for this research the investigated we propertiesfracture of degraded thermally PETG/CNT nanocomposite films CNT various with contents. P2306-6 FRACTURE MECHANISM STRENGTH AND OFPREDICTION IN-SITU TIB2/AL COMPOSITE Duan Min’ge Northwestern Polytechnical University A ductile-brittle model isdamage proposed by combining homogenization technique, Statistical model anddamage metal plasticityPorous model. - - - - , Beijing , Chester , Hefei University Meeting room 209 room Meeting P2305-7 P2305-7 ANDDESIGN OFPRODUCTION FILAMENT WOUND SLEEVES FOR HIGH FLYWHEEL SPEED ROTORS Zu Lei of Technology Filament-wound flywheel sleeves were designed ultra- using high fiber The tensions. is research present a useful provide able to for productiontool of composite sleeves for high-speed flywheel rotors. P2305-5 VIBRATIONAL ENERGY HARVESTING OF MULTIFUNCTIONAL BLADECOMPOSITE FOR OFFSHORE TURBINEWIND Tao Wen University P2305-6 COM SULFIDE WITH APOSITE LARGE SPECIFIC AREA SURFACE - FOR HIGH-PERFOR ALL-SOLID- MANCE PSEUDOCA STATE PACITORS Sailong Xu University of Chemical Technology Large-specific-sur face-area NiS2/ isCoS2/3D graphene pseudo as prepared capacitor electrodes, delivers an capacitance 1 A at of F g−1 2451 all-solid-state The g−1. device achieves a capacitance retention 5,000 after of 97.2% cycles 20 at A g-1. , The , Aerospace , Beihang Meeting room 208 room Meeting P2304-7 EPI-FLUORESCENT OF MICROSCOPY TRIMMEDEDGE FIBRE CARBON REINFORCED AN POLYMER: TO ALTERNATIVE CT-SCANNING Sam Ashworth University of Sheffield milling ofThe composites can induce sub-surface damage. toA novel metric machining measure induced defects epi-fluorescentthrough optical microscopy an as presented is x-ray to alternative computed tomography. P2304-5 ON THESTUDY ANDPROCESS PROPERTIES OF NANOTUBE CARBON CURINGFILM FIBER CARBON COMPOSITES Zhiwei Liu P2304-6 MACHINED SURFACE TOPOGRAPHY IN ANALYSIS ULTRASONIC VIBRATION END ASSISTED GRINDING OF SICP/ COMPOSITESAL Zheng Wei of Institute Research & ProcessingMaterials Technology Universitiy , UNIST , Wuhan , Wuhan , Harbin Meeting room 206 room Meeting P2303-7 P2303-7 IMPACT REPEATED OFRESPONSES HONEYCOMB PANELS SANDWICH LiYinggang University of Technology P2303-6 P2303-6 MODIFIED DCB TESTS FOR MEASURING MODE I FRACTURE AT TOUGHNESS THE INTERFACE OF SANDWICH STRUCTURES Sooyoung Lee DCB standard The modifiedtest is to Mode I pure trigger at behavior fracture interface skin/core the panelsof sandwich analysisand image utilizedis quantify to interfacialthe fracture property. P2303-5 P2303-5 OF AS4/ RESPONSE COMPOSITE PEEK LATTICE STRUCTRUES UNDER THE ANDCOMPRESSION VELOCITYLOW LOADING IMPACT Jiqiang Hu Institute of Technology Institute A new fabrication process of AS4/PEEK was structure lattice proposed, and the compression and velocitylow impact ofbehaviors the studied were structure work.in this , , , Mitsui P2302-7 P2302-7 EXTENDEDAN THICKNESS- DEPENDENT MOISTURE ABSORPTION FORMODEL UNIDIRECTIONAL CARBON/EPOXY COMPOSITES King Jye Wong Universiti Teknologi Malaysia uses a study This thickness-dependent model characterise to non-Fickian the absorption moisture of carbon/behaviour epoxy composites. non-Fickian The are parameters and fitted. normalised P2302-6 P2302-6 LIFE STATISTICAL OFPREDICTION UNIDIRECTIONAL UNDER TAPE CF/PP TENSION CREEP LOAD Isaki Takeharu Chemicals Inc examines study This prediction of the life time forstatistical newly developed CF/ UD sheetPP under loading. tension creep P2302-5 P2302-5 FUEL EFFECT ON THE TENSILE STRENGTH EVOLUTION OF FIBERSCARBON UNDER DIRECT FLAME ATTACK GómezPablo Chávez Polytechnique Montréal tow-based A hybrid involving approach tensile simultaneous load and open flame been used has attack carbon on PAN-based fibres. morphology The strength and tensile evolution assessed. are Meeting room 205 room Meeting

, Deakin , Aerospace , Yamagata , Yamagata P2301-7 P2301-7 HIGH-TEMPERATURE AND THERMAL MECHANICAL PROPERTIES OF AEROGEL/FIBROUS ZIRCONIA CERAMIC COMPOSITES Jingjing Sun of Institute Research & ProcessingMaterials Technology microstructure, The and thermal mechanical properties temperatures high at of aerogel/fibrous the ceramic zirconia composites were The investigated. that results showed the impregnating after thermal aerogel, the properties improved, but compressive the high- at strength decreased. temperature P2301-6 P2301-6 PREPARATION MECHANICAL AND PROPERTIES OF FLAKEMETAL PARTICLES/RESIN COMPOSITE Sako Yutaro University A composite of flakesaluminum and epoxypowder resin improved the and bendingtensile modulus. It exhibited reinforcement the efficiency0.36 factor of modulus.in tensile P2301-5 P2301-5 STRUCTURAL COMPOSITE FORBATTERIES AUTOMOTIVE APPLICATIONS Jaehoon Choi University Plenary 2 1505-1510 1510-1515 1515-1520 TUESDAY 13 AUGUST TUESDAY Time

SCIENTIFIC PROGRAM 52 SCIENTIFIC PROGRAM SCIENTIFIC 55 ,

2415 Metal matrix Composites Meeting room 219 room Meeting 2415-1 2415-1 THE STRAIN RATE SENSITIVITY OF AN CNT-REINFORCED MATRIX METAL AL COMPOSITES Jianghua Shen Northwestern Polytechnical University Fill Gesellschaft Fill Gesellschaft industry session only *invitation event* “4 X 4 STRATEGY” FOR- BASE AUTOMATION IN COMPOSITE MANUFACTURING Wilhelm Rupertsberger by Sponsored CONTINUED ,

2414 Dynamic properties, and ceramic fracture compositesmatrix Meeting room 218 room Meeting 2414-1 2414-1 MODELLING OF A POLYMER COMPOSITE TUBE CRUSHING UNDERPROCESS HIGH STRAIN RATE CONDITIONS Sina Eskandari University of Oxford A model for composite under materials is rate high strain developed. It considers viscoelasticity failure Drop and damage. tests for tubestower out carried andare thecompared to simulation. ,

2413 matrix Ceramic composites Meeting room 217 room Meeting 2413-1 AND PREPARATION CHARACTERIZATION OF A TERNARY EUTECTIC AL2O3-ZRO2- Y2O3 CERAMIC COMPOSITE Guoqing Chen Dalian University of Technology presentation This devotedis to eutectic the investigate solidification behavior and microstructural evolution of Al2O3/ the ZrO2(Y2O3) pseudo- binary eutectic system. , Wuhan , Wuhan

2412 health Structural monitoring Meeting room 216 room Meeting 2412-1 MONITORING CURE-INDUCED AND TEMPERATURE STRAINS IN LARGE COMPOSITES WITH FBG SENSORS Anxin Ding University of Technology , , University

2411 Computation and electronics Meeting room 215 room Meeting P2311-8 P2311-8 COMPOSITE PROPERTY DETECTION “WEAK”USING FORMULATION LOCAL BASED SPECIFIC STIFFNESS IDENTIFICATION Zhang Chao Nanjing University of Aeronautics and Astronautics paper presentsThis a vibration-based local specific stiffness identification method. an enhancedBy using “weak” the formulation, accuracy noise and immunity capability is improved. 2411-1 NEUROMORPHIC NETWORK BASED ON CARBON NANOTUBE COMPOSITES FOR LEARNING Chen Yong of California Los Angeles ,

2410 3:Actuation of activeformation composites Meeting room 214 room Meeting 2410-1 INSTABILITY- PATTERN INDUCED IS FORMATION SOFT COMPOSITES FOR MECHANICAL METAMATERIALS Rudykh Stephan University of Wisconsin Madison , ,

2409 and damage Fracture Meeting room 213 room Meeting Altair industryAltair session RESEARCH MEETS - PRACTICE HOLISTIC ALTAIR’S APPROACHFOR THE COMPOSITE DESIGN, AND SIMULATION OPTIMISATION PROCESS Palanterä Markku ofDirector Global Composites Business Development by Sponsored CONTINUED 2409-1 IN-SITU FULL FIELD OUT OF PLANE DISPLACEMENT STRAINAND MEASUREMENTS THE MICRO- AT IN SINGLE SCALE REINFORCEMENT COMPOSITES UNDER TRANSVERSE LOAD Ilyass Tabiai Polytechnique Montréal fiberThe / matrix damage inter-facial of fiber- mechanisms reinforced composites for four investigated are different composites containing a single fiber or bundle of fibers load under transverse digital micro using correlation image quasi- in-situ during testsstatic of single- dogbonereinforcement specimens. , , Insa , National , National

2408 Textile-based composites Meeting room 212 room Meeting P2308-8 P2308-8 ON TRUSSSTUDY TYPE SEGMENTAL COMPOSITE STRUCTURE FOR TEMPORARY RESCUE BRIDGE Yeh Fang-Yao Center On for Research Earthquake Engineering typeA truss segmental composite temporary is bridge rescue proposed, and a 50-m asymmetricspan self-anchored truss type segmental cable-stayed bridge designed,is and experimentally improve to validated stiffnessthe of a longer bridge. span P2308-9 PREPARATION OF THE PVDF/ COMPOSITE PAR BY MATERIALS HIGH SHEAR RATE PROCESSING Seung Goo Lee Chungnam National University 2408-1 RATIO POISSON 12 IN TO EQUAL LONGITUDINAL COMPRESSION DURING MESO- FE ANALYSIS OF COMPOSITE TEXTILE REINFORCEMENTS Philippe Boisse Lyon , , Rmit University

2407 Computational and finite element methods Meeting room 211 room Meeting In this work, this In comprehensive andexperimental studies numerical been carried have the out investigate to impact of behaviour flax fibre-reinforced polypropylene (PP) composites. The impact response predicted by the modelnumerical the with agreed well andexperimental results 2407-1 A NUMERICAL TO MODEL THE SIMULATE RESPONSE IMPACT OF FLAX- POLYPROPYLENE COMPOSITES Raj Das P2307-8 P2307-8 EVALUATION METHOD OF JOINING STRENGTH OF CFRTP MANUFCTUED BY INJECTION HYBRID PROCESS MOLDING Matsumoto Fumiya Kindai University we study, this In proposed a evaluation method joining for the of hybrid strength injection molded products woven using laminates CF/PA66 and short CF/PA66, and verified its effectiveness. , The

2406 Scott White symposium Meeting room 210 room Meeting 2406-1 MODELING OF MODULUS EVOLUTION FOR PROCESS SIMULATION Anoush Poursartip University of British Columbia matrices Thermoset liquid to from transform solid during to rubber processing. Many composites processing researchers simulation used Young’s have and Poisson’s Modulus describe to theRatio transformation. matrix argue we Here bulkthe that strongly moduli are and shear and appropriate much correct properties to and use. characterize , Harbin , RMIT ,

2405 Additive manufacturing Meeting room 209 room Meeting 2405-1 BIODEGRADABLE SYNTHETIC POLYMER-CERAMIC COMPOSITE VIA MATERIALS ADVANCED VARIOUS MANUFACTURING TECHNIQUES AlizadehMona Osgouei P2305-8 BI-STABLE PIEZOELECTRIC COMPOSITE LAMINATE FOR ENERGY HARVESTING Dai Fuhong of Technology Institute , , , University of , University of

2404 Modernising composites regulations Meeting room 208 room Meeting Welcome and Welcome of introduction speakers Professor Janice Barton University UK of Bristol, for Certification design: Reshaping pyramid testing the a compositewith aero-structures perspective Professor Ole Thomsen University & of Bristol CompositesNational Centre, UK Professor Richard Butler Bath, UK Composites – a cross regulations sector perspective exampleswith of challenges current to and routes mitigation Professor Simon Quinn Southampton, UK and member of the Regulations, Codes workingand Standards undergroup the Composite Leadership Forum (CLF), UK , , University

2403 Smart composites Meeting room 206 room Meeting 2403-1 STRUCTURAL HEALTH OFMONITORING POLYMER- SMART COMPOSITE MATRIX DURING CYCLIC USING LOADING IN-SITUAN PIEZOELECTRIC SENSOR Corentin Tuloup Université de de Technologie Compiègne - RobervalLaboratoire FRE UTC-CNRS 2012 P2303-8 P2303-8 OFADHESION DISSIMILAR POLYMER-METAL COMPOSITE BY MATERIAL MECHANICAL INTERLOCKING LinHarrison of Toronto Development of a new ofclass polymer-metal composites strong with interfacial adhesion by mechanical interlocking of polymer metal with matrix micro-pores. ,

2402 Biocomposites The University of Queensland investigated work This feasibilitythe of a fire-manufacturing fibre natural retardant ply be in liquid used to composite moulding. a readily Using product waste available bagasse, - sugarcane and common fire- compounds,retardant a rudimentary process develop to used was ply. a fire retardant Composite panels these plies from made characterised were TGA,using cone and four- calorimetry, point bending. 2402-1 DEVELOPMENT OF RETARDANT FIRE IN FOR PLIES USE FIBRE NATURAL COMPOSITE MANUFACTURE Asanka Basnayake Meeting room 205 room Meeting

, , National , National , Kookmin

2401-1 DEVELOPMENT OF MULTISCALE TOUGHENING TO TECHNIQUE ADDRESS THE MICRO-CRACKING OF PROBLEM COMPOSITES CRYOGENIC AT TEMPERATURE Islam Mohammad The University of New South Wales interlaminar The propertiesfracture of angle-ply carbon- epoxy and nanosilica- carbon-epoxy compositeslaminated RT at investigated were temperature and LN2 for addressing problem microcracking of composites for cryogenic applications. P2301-9 P2301-9 SIC/SIC COMPOSITES BY FABRICATED ELECTROPHORETIC DEPOSITION COMBINED WITH POLYMER INFILTRATION PYROLYSIS AND PROCESS Honglei Wang University of Defense Technology the improve to order In conductivitythermal of SiC/SiC composites by Polymer fabricated and Infiltration Pyrolysis (PIP) process, SiC/SiC composites fabricated were by Electrophoretic Deposition (EPD) combined PIP with process. University Carbon-carbon composite desirable is materials for candidate and of insulation heat high temperature However, heater. disadvantage the of carbon-carbon composite low is at resistance oxidation and high temperature resistance. wear lower studyTherefore, this oxidation investigates and indentation ofresistance Cf-C composites evaluate to indentation oxidation resistance. P2301-8 P2301-8 AND OXIDATION INDENTATION OF RESISTANCE CARBON-CARBON BY COMPOSITE CARBIDE SILICON COATING Kee Sung Lee Exhibition hall 2401 Nano-composites Coffee break Plenary 2 1610-1630 1520-1525 1525-1530 TUESDAY 13 AUGUST TUESDAY 1610-1830 1530-1610 Time

SCIENTIFIC PROGRAM 54 SCIENTIFIC PROGRAM SCIENTIFIC 57 , , Deakin Li, Key Lab State Meeting room 219 room Meeting 2415-3 MANUFACTURING OFPROCESS GRAPHENE REINFORCED AL ANDCOMPOSITE PROPERTIESTHEIR Choi Yongbum School ofGraduate Engineering, Hiroshima University 2415-4 EFFECTS OF ULTRASONIC ON TREATMENT MICROSTRUCTURE MECHANICAL AND PROPERTIES OF HYBRID PARTICULATES REINFORCED MATRIX AL-ALLOY COMPOSITES Jianyu of Processing Materials and Die & Mould Huazhong Technology, University of Science China and Technology, 2415-2 TO WASTE SUPERWEALTH: CARBON HARD MICROTUBE DERIVED FROM COTTON WASTE FOR COMPOSITE APPLICATIONS ShirvaniKamyar Moghaddam University , Chair , , The Ohio Meeting room 218 room Meeting 2414-3 HIGH STRAIN TESTING RATE OF FIBROUS COMPOSITE THE SPLIT USING BAR HOPKINSON WITHTECHNIQUE DIC Amos Gilat UniversityState Hopkinson split The isbar technique for high strain used testing of T800/ rate compositeF3900 in compression and Digital image tension. used for is correlation strain the measuring surfaceon the of the specimen. 2414-4 PRESSURE DURING INFLUENCE CURING ON THE MECHANICAL PROPERTIES OF RESIN EPOXY COMPOSITES AT HIGH STRAIN RATES Moritz Kurkowski of Plastics Technology, TU Dortmund University a shows study This significant pressure influence curing during impacton the strength of epoxy resin and mechanicalon the properties of carbon fibre plastics reinforced rates. strain high at 2414-2 ULTRA-HIGH USING IMAGING SPEED IDENTIFYTO THE MATERIAL PROPERTIES OF COMPOSITES AT HIGH STRAIN RATES Lloyd Fletcher University of Southampton displacement Full-field are measurements differentiated spatially fields. obtain strain to differentiation Temporal gives acceleration the related fieldsare which applied the load. to Combining these givesmeasurements response material the of composite. the , , Harbin , University of Meeting room 217 room Meeting 2413-3 MECHANICAL PERFORMANCE, RESIDUAL STRESS AND MICROSTRUCTURAL OF ANALYSIS CERAMIC MULTIPLE COMPOSITE MATRIX SYSTEMS Forna- Joachim-Paul Kreutzer Bristol mechanicalThe performance, the of microstructure matrix multiple ceramic composites were under investigated different conditions service. to relevant it present the to Up observedwas that a high degree of variability found in is of microstructure the these systems resulting in high variability of the mechanical properties. 2413-4 MICROSTRUCTURE, MECHANICAL PROPERTIES OXIDATION AND OF RESISTANCE C/C-SIC-ZRB2 COMPOSITES Han Wenbo of Technology Institute 2413-2 THE IMAGING OF LIFE-CYCLE HIGH- USING CMCS RESOLUTION X-RAY MICRO-COMPUTED TOMOGRAPHY Peter Creveling University of Utah utilizes study This X-ray capture µCT to imaging life-cycle entire the of a CMC specimen, to manufacturing from Results failure. ultimate bewill presented methods toon the and quantifyimage evolutionthe of microstructure the thethroughout process.manufacturing , Queen , University , Beihang Meeting room 216 room Meeting 2412-3 ULTRASENSITIVE STRAIN SENSORS FOR STRUCTURAL HEALTH USING MONITORING ALIGNED A HIGHLY NANOTUBE CARBON WEB Sandeep Kumar University Belfast 2412-4 DETECTION OF DIFFERENT MECHANICAL FORCES BY MULTIDIRECTIONAL SENSORS Shuhua Peng of New South Wales 2412-2 LASER-INDUCED FIBERGRAPHENE FORSENSORS STRUCTURAL HEALTH MONITORING OF POLYMERIC COMPOSITES MeihongHe University ofA new fabrication freestanding graphene fiber bysensors laser- induced graphene technology was Based demonstrated. resistanceon the embedded the variation, fiber sensorgraphene highly demonstrates in life-longvaluable SHM of composite laminates. - - - , , , MIT , Meeting room 215 room Meeting 2411-3 COMPUTATIONAL MECHANICAL METAMATERIALS Hopkins Jonathan University of California, Los Angeles (UCLA) 2411-4 CAPTURING- AR OF MAGNETIC RAYS COM BEADS USING HETEROPOSITE STRUCTURES WITH PERPENDICULAR MAGNETIC ANISOT ROPY (PMA) Lynch Christopher University of California, Riverside 2411-2 STRUCTURAL ELECTRONIC COMPONENTS ONBASED POLYMER NANOCOMPOSITES Wardle Brian componentsElectronic including resistors, inductors, capacitors using created are polymer structural compositesnano and evaluated. , , , Air Force Meeting room 214 room Meeting 2410-3 ELASTOMER- GRANULAR FLUID COMPOSITES FOR VARIABLE COMPLIANCE IN ROBOTIC APPLICATIONS BakarichShannon Cornell University stiffnesshas Variable been successfully in demonstrated – granular elastomer fluid composites. In want we research this the investigate to of thesefluidic nature materials granular and consider them a newas medium for in force transferring actuators. pneumatic 2410-4 DEVELOPMENT OF FIBERADAPTIVE REINFORCED PLASTICS OPEN BY WEAVING REED TECHNOLOGY AshirMoniruddoza Universität Technische Dresden FRPAn adaptive was developed shape with memory alloy being integrated structurally fabrics reinforcing into open using reed technology. weaving a subsequent step, In thermomechanical the of characterization FRPadaptive was executed. 2410-2 TUNING MECHANICAL IN INSTABILITIES MAGNETO-ACTIVE ELASTOMER COMPOSITES Abigail Juhl LaboratoryResearch , University , Department , Northwestern Meeting room 213 room Meeting 2409-3 ANALYSIS FAILURE OF FIBRE METAL JOINTS LAMINATE Du Yong Polytechnical University paper aims This failure the study to and failure strength mode of Fiber Metal in single-Laminates bolted single-lapped joint. 2409-4 STRESSBIAXIAL TESTS FOR UNIDIRECTIONAL LAMINATES CFRP Goto Keita of Aerospace Engineering, Nagoya University stress testsBiaxial of unidirectional CFRP laminates performedwere to failure investigate fiber under criteria tensile- longitudinal fiber transverse compressive biaxial stress state. 2409-2 THE INFLUENCE OF NONWOVEN INTERLEAF ARCHITECTURES ON THE IMPACT OFPERFORMANCE COMPOSITES Rhys Archer of Manchester an is Presented of the investigation influence of the properties ofstructural interleaves non woven damage on the and damage resistance toughness of CFRP composites, evaluated impact andthrough compression tests. Results that show resistance damage the with increases of areal the increase density of interleaf. the , Institute , Institute , Donghua , INSA de Meeting room 212 room Meeting 2408-3 HYSTERETIC BEHAVIOUR OF MODELLING FABRIC WOVEN UNDER LARGE STRAIN Yvan Denis Lyon at student PhD LaMCoS laboratory completing in France finalthe year of its studies. Currently on material working modelise to behaviour new composite forming as such strategy processes.incremental 2408-4 ONSTUDY AND BIAXIAL TENSILE CYCLIC PROPERTIES OF FEVE REINFORCED MEMBRANES Jinhua Jiang University 2408-2 NUMERICAL OF MODELLING CARBON BIAXIAL BRAIDSFIBER CONSIDERING PROCESS VARIBILITIES CzichosRuben of Design, Aircraft University of Stuttgart , , The , Ecole Meeting room 211 room Meeting 2407-3 MULTISCALE DAMAGE OF SIMULATION UNDER LOW CFRP VELOCITY IMPACT Akinori Yoshimura Nagoya UniversityNagoya Des Mines 2407-4 NUMERICAL ASSESSMENT OF CAPILLARY PRESSURE BY FLOW IN A SIMULATION MEDIUMFIBROUS Hong Vo Nhan 2407-2 DEVELOPMENT OF FINITEPARALLEL METHODELEMENT FOR ANALYZING PROGRESSIVE FAILURE INTERFACE OF LARGE-SCALE MODELSCFRP Yamaguchi Taichi University of Tokyo developed parallel We finite element analysis (FEA) that software, failure can simulate of large-scale CFRP models including interfaces. We software the validated double by simulating cantilever beam (DCB) experiments. , , , Meeting room 210 room Meeting 2406-4 SELF- TOWARDS REGULATING DENTAL COMPOSITES Yourdkhani Mostafa Colorado State University A novel method for enhancing longevitythe of restorations dental developedis via deliverysustained of bioactive compounds dentin-resin the to interface using sustained-release polymermicrocapsules. 2406-3 NANO: MULTIFUNCTIONAL FIBERS AND COMPOSITES FROM (ALMOST) NOTHING Erik Thostenson University of Delaware A novel electrophoretic deposition process for multifunctionalcreating textiles and fibers introduced. is inApplications health structural and flexiblemonitoring for human sensors motion detection will be discussed. 2406-2 FROM THE MICROFABRICATION OF MICROVASCULAR NETWORKS TO THE ADDITIVE MANUFACTURING OF MULTIFUNCTIONAL COMPOSITES Daniel Therriault Polytechnique Montréal presentation This covers select scientific achievements of Prof. team Therriault’s mainly on additive of manufacturing multifunctional composites while into insight providing from contributions the with and interactions team. White’s Prof. , University , Texas A&m , Texas , Mcgill Meeting room 209 room Meeting 2405-4 ENHANCING MECHANICAL PROPERTIES OF 3D PRINTED PARTS SPRAYING BY CELLULOSE NANOCRYSTALS Amir Asadi University 2405-3 DESIGN, MANUFACTURE TESTINGAND OF 3D PRINTED CONTINUOUS FIBRE REINFORCED LUG COMPOSITE STRUCTURES Peng Zhuo of Nottingham 2405-2 HIGHLY STRETCHABLE 3D-PRINTED COMPOSITE STRUCTURES Yazdani Hamidreza Sarvestani University & National CouncilResearch Canada , , , Meeting room 208 room Meeting National CompositesNational Centre, UK Composite – regulations challenges and opportunities Mr Rodney Thomson Engineering Manager, Advanced Composite Australia Structures Pty Ltd This workshop will run for 2 hours between 1600 and 1830 Composites and regulations processes for and validation certification - an industry perspective Jevons Dr Matthew MT Aerospace AG, Germany Partnership between academia and industry on composite improving and regulations certification processes Dr Enrique Garcia - , , Inegi , RMIT RMIT , Meeting room 206 room Meeting 2403-4 ANDDESIGN MANUFACTURE OF MULTISCALE FIBRE CARBON REINFORCED (CFRP) POLYMER COMPOSITES FOR MULTIFUNCTION ALITY Raquel Santos of Science- Institute In and Innovation andMechanical Engineering Industrial 2403-3 GRAPHENE- SMART ENABLED COMPOSITE Mojdeh Reghat Swinburne UniversitySwinburne of Technology Composite structures in high-performance are applications exposedoften to externaldamaging impacts, deformations and changes in environmental conditions during service. Smart composites structural multifunctionalare materials structural capable of are which stress, damage strain, sensing. or temperature 2403-2 VIBRATION ACOUSTIC AND PROPERTIES OF MULTIFUNCTIONAL SANDWICH COMPOSITES WITH EMBEDDED LITHIUM-ION POLYMER BATTERIES Joel Galos University paper presentsThis an experimental study and numerical effect the into of embedding (LiPo) sandwich into batteries on thepanels and acoustic vibration properties. , , Univ. , Univ. , Lulea , Lulea 2402-4 THE EFFECT OF ON SEAWEED MECHANICAL PROPERTIES OF JUTE FIBER/VINYL ESTER COMPOSITES Jaecheol Kim National Changwon University Additives are using manufactured environmentally friendly materials, mechanicaland the properties of natural fiber composites are improved by using additives and analyzed by SEM image. 2402-3 ALIGNED POLY(LACTIC ACID)-BASED NANOCOMPOSITES REINFORCED WITH IN-SITU DISPERSED CELLULOSE NANOCRYSTALS Shiyu Geng University of Technology work present The reports strong alignedand tough poly(lactic acid)-based nanocomposites well-dispersedwith cellulose nanocrystals achieved by the ofcombination three novel processing methods, i.e. emulsion in-situ polymerization, liquid- extrusionassisted and drawing. solid-state 2402-2 THERMO-HYGRO- MECHANICAL OF BEHAVIOUR NONWOVEN BIOCOMPOSITES UNDER VARIOUS ENVIRONMENTAL CONDITIONS GagerVictor Sud, Bretagne UMR IRDL CNRS 6027, Meeting room 205 room Meeting

, MIT , , , 2401-4 INTERLAMINAR SHEAR REINFORCEMENT OF UNIDIRECTIONAL AEROSPACE LAMINATES WITH RADIALLY CARBON ALIGNED NANOTUBES LiRichard Massachusetts Institute of Technology 2401-3 CAPILLARY- ENHANCED NON-AUTOCLAVE COMPOSITE MANUFACTURING ONBASED NANOPOROUS NETWORK Lee Jeonyoon capillary-drivenThe manufacturing presentedtechnique enableshere autoclave- traditional prepregrequired be processedto under vacuum-only conditions without or any an autoclave modifications the to system. prepreg 2401-2 OF FABRICATION HIERARCHICAL POLYMER NANOCOMPOSITES WITH CAPILLARY- ALIGNED DENSIFIED NANOTUBE CARBON REINFORCEMENT Ashley Kaiser Massachusetts Institute of Technology process-This of study structure polymerhierarchical nanocomposites millimeter-tall (here capillary- patterned, densified aligned carbon nanotubes in aerospace-grade epoxy) presents multi-scale structural to characterization high- investigate density nanotube confinement effects on nanotube-polymer interactions. Plenary 2 1630-1650 1710-1730 1650-1710 TUESDAY 13 AUGUST TUESDAY Time

SCIENTIFIC PROGRAM 56 SCIENTIFIC PROGRAM SCIENTIFIC 59 , Indian Institute , Indian Institute Meeting room 219 room Meeting 2415-5 CHARACTERIZATION REINFORCEDOF SIC AZ91 MAGNESIUM COMPOSITES ALLOY USING PRODUCED IN-SITU MICROWAVE CASTING Apurbba Kumar Sharma Roorkee of Technology , , , University Meeting room 218 room Meeting 2414-6 CHARACTERIZATION OF MODELING AND SILICON WOVEN TUBULARCARBIDE COMPOSITES Subhash Ghatu University of Florida 2414-7 IN SITU OBSERVATION OF CRACK IN A FORMATION ALUMINA-ALUMINA COMPSOITE AT 1200°C Dong Liu of Bristol 2414-5 FLEXURAL IMPACT PROPETIES FRACTUREAND OF BEHAVIORS CONTINUOUS AND DISCONTINUOUS RANDOM REINFORCED THERMOPLASTIC CFRP Yano Fumiaki Corporation Shimadzu , , Southwest , Northwestern Meeting room 217 room Meeting 2413-5 REACTION ASSISTED FLASH OFSINTERING AL2O3-YAG EUTECTIC COMPONENT CERAMIC Jinling Liu UniversityJiaotong mixed Al2O3-Y2O3 The can bepowders flash 800 °C at sintered appliedunder the electrical field of 900 V/ the It demonstrate cm. feasibility of employing sintering flash the fabricate to technique oxide eutectic ceramic. 2413-6 STIFFNESS SICF/SIC PREDICTION, RESIDUAL THERMAL STRESS AND PROGRESSIVE DAMAGE BY SIMULATIONS MICRO-MECHANICS MODEL Bin Liu Polytechnical University on predictingFocusing macro-stiffnessthe residual and thermal stress for SiCf/ SiC composites, 3D finite micro-structure element analysis appliedmethods to are volume representative elements and the progressive damage simulation. 2413-7 MICRO-SCALE OF ANALYSIS PROGRESSIVE IN DAMAGE MATRIX CERAMIC COMPOSITES Riccardo Manno University of Bristol aims work This the investigate to behaviour damage of CMCs the at Micro-Scale through employmentthe of representative elementary volumes singlelocated within tows. fibrous , The , Institute , Institute , The Meeting room 216 room Meeting 2412-5 NANO-ENGINEERED POLYMER GRAPHENE COMPOSITES WITH SELF-HEALTH MONITORING Pengyu Zhou Hong Kong Polytechnic University 2412-6 ELECTRICAL RESISTIVITY OF THIN-PLY COMPOSITES Liyong Tong University of Sydney 2412-7 STRUCTURAL HEALTH MONITORING DEMONSTRATION OF PRESET-DAMAGE MICROWIRE ENABLED ARRAYS COMPOSITES BASED ON MICROWAVE PROPERTIES Xuefei Zheng for Composites Science (InCSI),Innovation Zhejiang University array Microwire modified by 5 wt.% can detectsilane local1mm diameter 1 is damage, which the from mm away in the microwire nearest composite to attributed of alteration marked the due structure domain improved stress the to by evaluating transfer its and absorption reflection coefficients, promising is which health in structural applications. monitoring , Meeting room 215 room Meeting 2411-5 MWCNT REINFORCED BIO-BASED BENZOXAZINE/ EPOXY WITH COPOLYMERS NIR ACTUATION CAPABILITY Rimdusit Sarawut Chulalongkorn University high NIR to Due efficiency,absorption carbonmulti-walled (MWCNTs) nanotubes in incorporated were biobased benzoxazine/ epoxy shape memory polymers reinforcement,as the endowing copolymers NIR with capabilityactuation under ambient atmosphere. , , Air Force Meeting room 214 room Meeting 2410-5 RAPID DESIGN PROTOTYPING AND OF ADAPTIVE COMPOSITE ARTICULATING CYLINDERS Jeffery Baur LaboratoryResearch 2410-6 ORGANIZED HYBRID NANOCOMPOSITES FOR ROBUST STRETCHABLE SENSORS AND FLEXIBLE MICROLASERS Vladimir Tsukruk of Georgia Institute Technology discuss We organized how bionancomposites enhancedwith mechanical and performancesensing can be constructed biopolymersfrom fiibroin silk as such and synthetic carbon flexible such materials 2D graphenes. , , , Shanghai Jiao , Shanghai Meeting room 213 room Meeting 2409-5 STUDY NUMERICAL OF THE FORMATION OF LEAKAGE THROUGH PATHS LAMINATES CFRP FOR CRYOGENIC PROPELLANT TANKS Hitoshi Hamori University of Tokyo finite study, this In element models experimentalusing propertiesmaterial and constructed, are influencethe of the difference of ambient and the temperature usefulness of thin-ply numerically are layers verified. 2409-6 DELAMINATION IN FAILURE MMB TEST WITH PERIDYNAMICS Yile Hu University Tong 2409-7 FRACTURE TOUGHNESS OF GRAPHENE SHEET ESTIMATED COUPLING BY OF BOUNDARY ANDELEMENT FINITE ELEMENT Hwu Chyanbin Cheng Kung National University ofA new approach multi-scale simulation couplingvia of boundary element and finite element is proposed predict to the toughness offracture sheet.graphene , , Meeting room 212 room Meeting 2408-5 AND EXPERIMENTAL STUDY NUMERICAL OF TRIAXIALLY BRAIDED UNDERCOMPOSITE AND QUASI-STATIC IMPACT HIGH SPEED LOADINGS Zhang Chao Northwestern Polytechnical University multi-scaledThe mechanical failure of triaxially behavior compositebraided under quasi-static and high-speed impactloadings investigated are experimentally and numerically. 2408-6 TOLERANCE IMPACT OF THERMOPLASTIC THERMOSETAND CARBON EPOXY TEXTILE COMPOSITES CarvelliValter Politecnico Di Milano impactThe performance of carbon textile reinforced highly polymerized epoxy thermoplastic and studied is thecompared to thermoset counterpart, the considering imparted damage impact after and the compression strength , , , Deakin Meeting room 211 room Meeting BoeingR&T - Australia testing using In-Situ non-destructive inspection techniques micro-CT as such and tomography neutron (NT) assisted have in understanding composite failure. access However, these bitsto of test equipment have to actedbarrier a as Afurthering research. this bridge to means presented. is gap 2407-7 FIBRE CARBON PROSTHETIC AND DESIGN FOOT: MANUFACTURING PROCESS LiuChao University 2407-5 PREDICTING MULTISCALE IN TEXTILEFAILURE COMPOSITES REALISTIC USING REPRESENTATIVE ELEMENTS VOLUME ChowdhuryNayeem 2407-6 A REPRESENTATIVE ELEMENT VOLUME FORMODEL ULTRA HIGH MOLECULAR WEIGHT POLYETHYLENE COMPOSITE Dimitrios Kempesis Imperial College London , McGill Meeting room 210 room Meeting 2406-5 OF RECYCLING TURBINEWIND BLADES FOR FILAMENTFUSED FABRICATION FEEDSTOCK Larry Lessard University , , USQ Meeting room 209 room Meeting University of Waikato is Thermography proposed for the assessment of short fibre 3D reinforced filamentsprinter quality provide to and assurance variation reduce the of properties and by printsfailed caused fibre during bunching manufacture. 2405-5 THERMOGRAPHIC ASSESSMENT OF FIBRE REINFORCED 3D PRINTING FILAMENT Tighe Rachael 2405-6 TOUGHENING OF POLYLACTIC ACID/BAMBOO FORBIOCOMPOSITE DEPOSITION FUSED MODELING Xianglian Xiao toughening Two beenagents have in PLA/investigated bamboo powder biocomposite for 3D application. printing effectThe toughnessof modification on the toughness properties, behavior, viscoelastic processability, filament quality evaluated. were Meeting room 208 room Meeting Modernising Composites Regulations session continues This workshop will run for 2 hours between 1600 and 1830 , , Xi’an Meeting room 206 room Meeting 2403-6 EXPERIMENTAL ONSTUDY TORSIONAL STIFFNESS OF A TURBINEWIND BLADE THROUGH COMBINED LOADING Mareen Tiedemann University ofTechnical WindDenmark - DTU Energy 2403-5 THE PHYSICAL TO FIELDS MICROHOLES IN PROBLEM FLEXOELECTRIC SOLIDS Xinpeng Tian Jiaotong UniversityJiaotong the paper, this In complete explicit solution of physical fields a micro-hole to is solvedfor flexoelectric are which solids since accurate more accounting for the gradient, the strain gradient,polarization flexoelectricthe and reversethe flexoelectric effects simultaneously. ,

, Delft Delft , 2402-6 SUSTAINABLE BIOCOMPOSITES FROM A SUPER NANO- TOUGHENED MATRIX BLEND FOR INDUSTRIAL APPLICATIONS Misra Manjusri 2402-5 FIRE PERFORMANCE OF BIOPOLYMERS RECOVERED FROM AEROBIC WASTE GRANULAR SLUDGES Lin Yuemei University of Technology sludgeBoth activated granular and aerobic biopolymers showed effective formation char their protein due to and phosphate components. self- The extinguishment ofthe biopolymer flax coated the indicated fabric fire-resistant behaviour of biopolymer the substance. University of Guelph different Three compostable fillers, i.e. agriculture fiber, natural residues, and mineral talc, added into were a novel biodegradable nano-blend matrix. Biocomposites with excellent mechanical- propertiesthermal the to in comparison existing counterparts created. were Meeting room 205 room Meeting

, Jan , Beihang Universit 2401-6 HYDROTHERMAL OF SYNTHESIS CO3O4@CF_RGO COMPOSITES AND THE EXCELLENT MICROWAVE ELECTROMAGNETIC PROPERTIES Shuang Li 2401-5 BATTERY PROTOTYPE WITH BASEDA CELL ON CARBON NANOSTRUCTURES Wojciech Ciesielski Dlugosz University In Czestochowa Student PartyStudent South Wharf - Munich Wunderbar ICCM VIP only) Dinner (invitation Plenary 2 1730-1750 1750-1810 TUESDAY 13 AUGUST TUESDAY 1810-1830 1900-2300 1915-2230 Time

SCIENTIFIC PROGRAM 58 SCIENTIFIC PROGRAM SCIENTIFIC 61 , , Sunchon , Harbin

Meeting room 219 room Meeting 3115 Metal matrix Composites 3115-1 DEFORMATION OF BEHAVIOR ALUMINUM MATRIX ALLOY COMPOSITES REINFORCED WITH FEW-LAYER GRAPHENE Seeun Shin University National 3115-2 COMPOSITE CASTINGS TICREINFORCED BY PARTICLES Łukasz Szymański University of Science in and Technology Innerco sp.Cracow; o.o. z authors presentedThe methods different three fabrication of in situ the of metal matrix composite casting via process: composite local composite layer, and cast reinforcement composite reinforced by TiC. 3115-3 INVESTIGATION ON NI-MN-GA PARTICLES/CU COMPOSITES PREPARED POWDER BY METALLURGY METHOD Bing Tian Engineering University phase Microstructure, and transformation mechanical property of particles/CuNi-Mn-Ga composites prepared pressureless by method are sintering in the investigated work.present , Pprime , Monash , Monash , Inspire

Meeting room 218 room Meeting 3114 Fatigue 3114-2 EXPERIMENTAL NUMERICAL AND DETERMINATION OF THE MODE II FRACTURE TOUGHNESS OF WOVEN COMPOSITES Healey Rowan University A three-dimensional finite element model developedwas the determine to mode II fracture toughness of a woven composite, validated by and an experimental comparison numerical a unidirectionalusing specimen. 3114-1 LIFE FATIGUE ESTIMATION OF A SHORT GLASS FIBERS REINFORCED THERMOPLASTIC: OF OPTIMIZATION ENERGETICAN CRITERION AND CORRESPONDING VOLUME INTEGRATION FOR MULTIAXIAL APPLICATIONS Caroline Goutal / Solvay Institute 3114-3 CONTROLLED STRAIN RESONANCE FREQUENCY TEST FATIGUE FOR CFRP BENCH Eduard Relea - ETHAG Zurich of a ram iron cast The BRUDERER BSTA-200 redesigned in was CFRP fatigue and the of CFRPbehavior had be in a very tested to high cycle test fatigue bench. , , Korea , Kyoto

Meeting room 217 room Meeting 3113 compositesHybrid 3113-1 IONIC CONDUCTIVITY AND MODULUS YOUNG’S POLYMER OF SOLID FOR ELECTROLYTES SUPERCAPACITOR Suk Jin Kwon of Materials Institute Science 3113-2 INVESTIGATION FOR CONTINUOUS MOLDING HYBRID FORPROCESS LONG MEMBER Akio Ohtani of Technology Institute 3113-3 MECHANICAL PROPERTIES AND FRACTUREMICRO OFPROCESS COMPOSITE HYBRID WITH MATERIAL SHEETSCF WITH GLASSMICRO BALLOON Omura Takuto School ofGraduate universityFukushima , The , , Shimadzu

Meeting room 216 room Meeting 3112 methods Testing 3112-1 EXPERIMENTAL INVESTIGATION ABOUT FLEXURAL PLASTIC AND FRACTURE OF BEHAVIOR MAT-TYPE CF THERMOPLASTIC COMPOSITES Kamei Yuki Corporation 3112-2 OF COMPARISON PICTURE FRAME DEVICES AND OF ANALYSIS ANGLE LOCKING WITH FOR FABRICS DIFFERENT CROSS- ANGLES PLY Benedikt Lux UniversitySwinburne of Technology includes study This ofa omparison established and novel testing devicesshear and an investigation of fabrics non-crimp different with fiber for orientations the automating of stiffeningpreforming elements. 3112-3 RELATIONSHIP BETWEEN FLEXURAL AND COMPRESSIVE OF STRENGTHS UNIDIRECTIONAL THERMOPLASTIC CFRP Matsuo Tsuyoshi University of Tokyo authorsThe proposed a new method test flexural for unidirectional CFRP. thermoplastic strength flexural The correlation a strong has compressive the with strength. ,

, Centro , Harbin

Meeting room 215 room Meeting 3111 Biomedical 3111-1 IN VITRO EVALUATION OF SURFACE ROUGHNESS ON INITIAL RESPONSES OF OSTEOBLASTS ON A NEWCELLS AL2O3/CE-TZP NANOCOMPOSITE Antonio Díaz Luis Rodríguez en de Investigación Y Nanomateriales (CINN-Nanotecnología CSIC-UNIOVI-PA) 3111-2 MECHANICAL, SHAPE MEMORY AND ANTIBACTERIAL PROPERTIES OF GRAPHENE OXIDE/PLCL NANOCOMPOSITES Xili Lu Engineering University g-GO/PLLAThe nanocomposites show good memory shape effect and antibacterial properties, which these that suggest nanocomposites may bepotentially usefulfor a variety of biomedical applications. 3111-3 EFFECT OF CROSS- LINKING CONDITION ON MECHANICAL PROPERTIES OF OSTEONECTIN- HAP/ COATED COLLAGEN Tanaka Mototsugu of Institute Kanazawa Technology , The ,

Meeting room 214 room Meeting 3110 Defence 3110-1 EXPERIMENTAL INVESTIGATION MESOSCALE AND MODELING OF TEXTILE COMPOSITES UNDER HIGH- VELOCITY IMPACT Hongxu Wang University of New South (Canberra) Wales focuses work This effectson the of rigiditymatrix on resistance,penetration absorption,energy extentand damage of UHMWPE textile composites subjected high-velocityto impact steelby a spherical projectile. 3110-2 EXPERIMENTAL OPTIMISATION FOR MILITARY OUT- AEROSCARF OF-AUTOCLAVE SCARF REPAIRS Riley Mitchell University of Southern Queensland , , , Beihang

Meeting room 213 room Meeting 3109 and damage Fracture 3109-1 EXCEPTIONS TO THE ASSUMPTION UNDERLYING THE SO-CALLED BASED PHYSICALLY THEORIES FAILURE Shuguang Li The University of Nottingham 3109-2 AND STRENGTH MODES FAILURE IN RESISTANCE WELDED THERMOPLASTIC JOINTS:COMPOSITE EFFECT OF FIBER– ADHESION MATRIX LiXuekuan University focus work This influenceon the of stainless mesh steel size failure on the modes of resistance thermoplastic welded composite joints. 3109-3 EVALUATION FAST OF THE LONGITUDINAL FAILURE TENSILE IN STATISTICS UNIDIRECTIONAL COMPOSITES ACCOUNTING FOR MATERIAL VARIABILITY MalgioglioFabio Siemens Industry Software NV longitudinal The propertiestensile of unidirectional composites and their predicted are scatter a multi-scalewith model, including the variability. material A simple Machine inspired Learning enables verystrategy computations.fast , , , Harbin

Meeting room 212 room Meeting 3108 Textile-based composites 3108-1 A NUMERICAL OF THESTUDY EFFECT OF DRAPING ON THE MECHANICAL PROPERTIES OF 3D WOVEN COMPOSITES Ioannis Topalidis University of Bristol (ACCIS) A modelling framework developedis and compared to data experimental the capturing towards effectthe on of draping mechanical properties of layer-to- 3D woven composites.layer 3108-2 CHARACTERISATION OF THE WRINKLING OF A BEHAVIOUR NON-CRIMP BIAXIAL DURING FABRIC FORMING Viisainen Verner University of Cambridge wrinkling The of abehaviour NCFbiaxial over four benchmark geometries characterised is forming through experiments with and it shown is 3D-DIC angle alone shear that cannot predict NCF wrinkling. 3108-3 MULTI-SCALE FORMODELING THEPREDICTING VISCOELASTIC OF BEHAVIORS 3D BRAIDED COMPOSITES Zeng Tao University of Science and Technology A new alternative procedure calculation to presented was the characterize time-dependent behaviorsviscoelastic of 3D resin-based compositesbraided perspective the from of macroscopic, mesoscopic and microscopic scale. , , Civil Aviation , Indian

3107 modellingMultiscale Meeting room 211 room Meeting 3107-2 COMPUTATIONAL CONTINUA MODELS OF COMPOSITE CURVED BEAMS Dinghe Li University of China 3107-1 MODIFIED MORI-TANAKA METHODS FOR DAMAGE OF MODELLING FIBRESHORT REINFORCED COMPOSITES Jain Atul of Technology Institute Kharagpur 3107-3 PROCESS-INDUCED MICROSTRUCTURE DURING COMPRESSION OF HIGHMOLDING VOLUME FIBER FRACTION SHEET MOLDING COMPOUND Mahe Francois University of Delaware is A new formulation proposed describe to evolvingthe multi- scale microstructure flow viscous and the SMC during behavior compression molding. , Swinburne University,, Swinburne Australia , Korea , Bronwyn Fox Bronwyn , Univeristy of

3106 Composite structures Meeting room 210 room Meeting 3106-2 DYNAMIC OF RESPONSE CARBON HYBRID FIBRE LAMINATE UNDERBEAMS IMPACT BALLISTIC Liu Tao Nottingham 3106-1 TORSIONL PROPERTIES OF A STIFFENED TUBECOMPOSITE Sung Joon Kim Aerospace Research Institute 3106-3 HIERARCHICAL THERMOPLASTIC COMPOSITE LATTICE STRUCTURE: AXIAL COMPRESSIVE PROPERTY LiuHouchang Chongqing University , , , Chalmers University (Meeting 213) room , Leibniz

3105 Additive manufacturing Meeting room 209 room Meeting 3105-2 3D PRINTED CONTINUOUS FIBRE COMPOSITES: OF VALIDATION & ANALYSIS DESIGN METHODS Joosten Mathew Deakin University successThe of study present the first the demonstrates in establishing step design tools validated forward facilitate to facing simulations the optimise to topology of 3D printed composites fully to exploit design the flexibility of this technology. emerging 3105-1 ADDITIVE MANUFACTURING OF COMPOSITE PANELS SANDWICH FOR BROADBAND SOUND ABSORPTION Filippo Iervolino Polytechnique Montréal presents work This single and multi- Fused material Deposition Modeling (FDM) of sandwich featuring panels multiple Helmholtz allow that resonators sound absorption of range over a wide frequencies. 3105-3 ADDITIVE MANUFACTURED FORCE METALLIC IN TRANSMISSIONS FIBRE REINFORCED THERMOPLASTICS Arne Kunze for Materials Institute Engineering , , , Pusan

3104 Liquid composites moulding Meeting room 208 room Meeting 3104-2 TOOL SELF-SEALING CONCEPT FOR RTM- PROCESSES Tim Stallmeister Universität Paderborn 3104-1 UNDESIRED FIBER OF DEFORMATION A MULTI-LAYERED PREFORMFIBER IN COMPOSITELIQUID PROCESS MOLDING Dong Gi Seong National University National A simple and efficient analytic scheme was proposed predict to of adeformations fibermulti-layered by comparingpreform forcesthe applied to in a mold preform the of liquid composite molding. 3104-3 OF INFLUENCE GASSES DISSOLVED RESIN ON IN EPOXY RESIN INFUSION QUALITYPART Sam Oosterom van Center for Advanced Composite - Materials University of Auckland , , Fac

3103 Resin and polymers Meeting room 206 room Meeting Technology 3103-2 OFTOUGHNESS POLYMERS EPOXY HIGH CURED AT RATES Declan Carolan 3103-1 ORGANIC RADICAL THERMOSET EPOXY Jaworski Capricho UniversitySwinburne of Technology report the We development of stable a as radicals organic polymeric framework for functional conductive materials. , Universita (Meeting degi 219) room di Studi Padova

, KU Leuven (Meeting 212), KU Leuven room , University (Plenary 2) Science & Technology

Meeting room 205 room Meeting , , MECHANICAL PROPERTIES AND FRACTURE RESISTANCE OF THREE-DIMENSIONAL GRAPHENE/POLYMER COMPOSITES GRAPHENE/POLYMER OF THREE-DIMENSIONAL FRACTURE PROPERTIES AND MECHANICAL RESISTANCE Jang-Kyo Kim Jang-Kyo STRUCTURES AEROSPACE COMPOSITE LAMINATED OF AFTER COMPRESSION AND IMPACT DAMAGE OF IMPACT MODELING University Michigan Davidson, Paul (Meeting 211) room IN THE FRAMEWORK IN FIBRE REINFORCED COMPOSITES MODELLED OF FINITE DAMAGE REGIONS ELEMENTS WITH EMBEDDED INTERFACIAL Stepan Lomov OF STRUCTURAL MODELLING COMPOSITES AND Lief BATTERY Asp CHARACTERISATION AN INTEGRATED APPROACH TO DESIGN AND MONITOR COMPOSITE STRUCTURES UNDER IN-SERVICE FATIGUE LOADINGS STRUCTURES COMPOSITE FATIGUE MONITOR AND DESIGN UNDER IN-SERVICE TO APPROACH INTEGRATED AN Marino Quaresimin

, Universiti

Day 3 Welcome & Announcements 3 Welcome Day IMDEAMaterials Institute is presentation The focused on CNT fibres and multifilament and thefabrics betweenrelationship CNT and alignment mechanical and for reinforcing potential composites.structural 3101-2 ANDALIGNMENT REINFORCING OF POTENTIAL MULTIFILAMENT FABRICS CNT Anastasiia Mikhalchan 3101-1 THERMAL PROPERTIES OF UNSATURATED POLYESTER COMPOSITES WITHFILLED MODIFIED SILICA AEROGEL AziziMuhamad Yajid Mat Malaysia Teknologi polyester Unsaturated widely are (UPR) resins in building andused industries construction panels, wall as such and flooring. For designthe of these thermal structures, properties as such conductivitythermal and stability among are importantthe criteria. KEYNOTE 1: PLENARY LECTURE: CHAIN FUTURE FOR FIBRE COMPOSITES: A JOURNEY CARBON CHALLENGES THROUGH THE VALUE Plenary 2 sessions concurrent to Move 3101 Nano-composites KEYNOTE 2: KEYNOTE 3: KEYNOTE 4: KEYNOTE 5: Move to concurrent sessions concurrent to Move 3101-3 SYNERGETIC ENHANCEMENT OF THERMAL CONDUCTIVITY ALUMINA BY INNANOWIRES COMPOSITESEPOXY CONTAINING FILLERS MICRO Kazuaki Sanada Prefectural Toyama University Plenary 2 Exhibition hall Coffee break 0800-0805 0805-0850 0900-0930 0850-0900 0900-1040 0930-0940 0940-1000 WEDNESDAY 14 AUGUST WEDNESDAY Time 1000-1020 1020-1040 1040-1110

SCIENTIFIC PROGRAM 60 SCIENTIFIC PROGRAM SCIENTIFIC 63 , , Bristol , Bristol , Boeing , MT Industry-Academia Industry-Academia Platform Discussion Meeting room 219 room Meeting Mobility between andAcademia Industry Isabelle Paris Bombardier gap the Bridging between education and employment Belcher Tony Modernising Composites Regulations Ole Thomsen University access for Increasing international to SMEs research Jevons Matt Aerospace sessionThis aims topics debate to cross betweenthat and industryacademia in a close and less environment. formal Come an join our we as animators keydiscuss topics and identify forward. ways will Each animator and a topic represent visitors can move between individual topics with or stay particularlyone that interests them. , , Indian ,

P3214 Metal matrix composites and meta-composites Meeting room 218 room Meeting P3214-2 P3214-2 WEAR AND MECHANICAL CHARACTERISTICS OF AL-SI/TIB2 COMPOSITES KarloopiaJimmy of Technology Institute Roorkee P3214-3 THE MAGNETIC AND ELECTROMAGNETIC PROPERTIES OF FECONISIXAL0.4 HIGH ENTROPY POWDERS ALLOY Duan Yuping Dalian University of Technology P3214-1 P3214-1 THE ENHANCING MECHANICAL PROPERTIES OF TIB2 REINFORCED MAGNESIUM COMPOSITES USING CASTING STIR METHOD Anbuchezhiyan Gnanasambandam Valliammai Srm Engineering College , Altair industry workshop Meeting room 217 room Meeting Altair industryAltair workshop RESEARCH MEETS PRACTICE - APPLYING MULTISCALE AND MODELING OPTIMIZATION IN COMPOSITES ENGINEERING Palanterä Markku ofDirector Global Composites Business Development run will workshop This for 90 minutes by Sponsored , , Harbin , Harbin

P3212 Bio-inspired composites green and fibre and natural composites Meeting room 216 room Meeting P3212-3 BONE TISSUE SCAFFOLD BASED MEMORY ON SHAPE POLYMER Wei Zhao of Technology Institute paper details anThis ofapplication SMP on bone tissueporous Comparedscaffold. bone traditional with the scaffold, tissue based onscaffold possesses SMP advantages of cost, low easy assembly and andeasy adjustment. themost importantly, bone tissueadaptable to will adapt scaffold best the keep fixed state. P3212-1 ANDDESIGN CONSTRUCTION OF BIO-INSPIRED MATERIALS SMART WITH REVERSIBLE ADHESION Ying Chu of Technology Institute P3212-2 AND PREPARATION - CHAR ELECTRICAL ACTERIZATIONS OF MAN-MADE NACRE-LIKE COMPOSITES Yingbang Yao Guangdong University of Technology ,

- ,

, Institute of , Institute

P3211 Defence and biocomposites Meeting room 215 room Meeting P3211-1 P3211-1 DIC ANALYSIS OF SHRINKAGE BEHAVIORS OF DENTAL COMPOSITES DURING DENTAL RESTORATION Choi Nak-Sam Hanyang UniversityHanyang changes ofThe polymerization distribution shrinkage compositein the resin part examined were by DIC methodthe during for restoration dental two types of composite resins. maximum The strain shrinkage centerhappened the at Clearfil for be -0.56% to for and -0.44% AP-X Filtek P90. TI-PENETRATION TI-PENETRATION OFPERFORMANCE TARGET SANDWICH OF THINMADE AND PLATES STEEL AGAINST WOOD BULLET 7.62MM Liling He Systems Engineering, China Academy of Engineering Physics limit Ballistic 1. velocities of thin the fitted are plates steel Recht- according to Ipson Model. 2. Dynamic compressive ofstrengthes and transverse wood longitudinal fittedare according dynamic the to cavity expansion model. tranverse 3. The betterwood has anti-penetration performance that than of longitudinal the wood. P3211-3 COMPUTATIONAL MULTISCALE MODELLING OF CERAMIC FOR MATERIALS NEEDS DEFENCE Meredith Mahoney Department of Defence new Historically, protective materials and composite systems developedwere mainly trial laborious through in However, and error. a multiscale work this computational the using approach, ofapplication ab initio to methods through continuum validated models, provide will through a framework understand to which and predict the performance of protective materials. allow also It will be tailored to materials new and counter to evolving threats. P3211-2 P3211-2 EXPERIMENTAL ON AN STUDY , , McGill , Nanjing

P3210 andAerospace Automotive Meeting room 214 room Meeting P3210-1 WARPAGE OF BEHAVIOUR DISCONTINUOUS THIN CF/PEEK PLATES Batista Natassia University strand different Two comparedsizes were warpage through Formeasurements. an strands, small the was grid alignment proposedalso better to their orientation. control P3210-3 CF/MODIFIED-PEEK COMPOSITES FOR AIRCRAFT Hayashi Takahiro Mitsubishi Chemical Corporation developed We modified-PEEK resins, resulted which than 20°C higher Tg PEEKs.conventional In showed we study, this some properties of modified-PEEK carbon fibermatrix composites, as such mechanical property temperature, high at fluid and resistance flammability. P3210-2 P3210-2 EXPERIMENTAL ON INTER-STUDY FRICTION YARN CHARACTERISTICS OF STF-KEVLAR WITH FABRICS DIFFERENT MASS CONCENTRATIONS Chen Wei University of Aeronautics and Astronautics paper, current the In typesThree of STF was suspension using prepared SiO2 spherical particles of 650 nm in differentdiameter concentration weight the impregnate to Kevlar49 fabrics. The rheological properties were of STF different investigated. , Harbin , Harbin , Indian P3209 compositesHybrid Meeting room 213 room Meeting P3209-1 INVESTIGATION OF LOW-VELOCITY CAI AND IMPACT OF BEHAVIOR SANDWICH HYBRID COMPOSITES Alex Osei Bonsu Engineering University P3209-3 EFFECT OF FIBER DISTRIBUTION ON COMBINED COMPRESSION- TORSIONAL RESPONSE OF HYBRID COMPOSITES Bhushan Sneha Cheryala of Technology Institute Bombay objectiveThe of work current the role the study to is of fiber distribution combinedin the loading response of glass/ hybrid carbon composites finiteusing element analysis. in change The varying with response fiber is distribution takingpresented into account of different the fiber location in the volume representative element (RVE). P3209-2 P3209-2 AND ROBUST CONDUCTIVE BASED HYDROGEL ON CARBON NANOTUBE/ARAMID FORNANOFIBER STRUCTURAL STORAGE ENERGY Wenxin Cao of Technology Institute , , The ,

P3208 analysis and Structural optimisation Meeting room 212 room Meeting P3208-1 ASYMPTOTIC AN SOLUTION DENSITYTO DISTRIBUTION OF GRADED CELLULAR A WITH MATERIALS IMPACT CONSTANT LOAD Baixue Chang University of Science of and Technology China P3208-3 OFDESIGN SEMI-COMPLEX USING PARTS ANISOTROPIC FIBER CARBON CARD WEB REINFORCED THERMOPLASTICS Furuta Yasuyuki University of Tokyo it was study, this In first verified that mechanicalthe properties of CWT can from be calculated fiberthe orientation (FOD) bydistribution Netting Theory. P3208-2 P3208-2 VIRTUAL CALCULATION OF THE B-BASIS ALLOWABLES OF NOTCHED COMPOSITE LAMINATES Carolina Furtado University of Porto , Polymer , US , School

P3207 Repair and tribology and fatigue Meeting room 211 room Meeting P3207-1 NEW MATERIAL TOOLS REMOVAL TO PROCESSES AND EXPEDITE SAFELY MAINTENANCE ON COMPOSITE STRUCTURES James Mazza Air Force Research Laboratory efficientMore and nonmetallic durable of a for removal tools variety of materials, including sealants, coatings, elastomeric adhesives, caulks and tapes, developed, were for useevaluated on composites and commercialized. P3207-3 P3207-3 BONDED COMPOSITE UNDER REPAIRS DRY/COLD HOT/WETAND ENVIRONMENTAL CONDITIONS RöperFlorian Competence Center Leoben Gmbh focuses work This influenceon the of °C and -30 testing at 100 cyclestesting after between °C and 70 -30 on repair h. °C / 85 % r. specimens. P3207-2 AND FAILURE RELIABILITY OF IN- ANALYSIS REPAIRED SERVICE COMPOSITES Feng Wei of Aeronautics, Northwestern Polytechnical University paper performedThis andexperimental works on thenumerical of in-servicebehavior compositesrepaired scarfvia method. and reliability analysis was conducted predicted to at strengths failure safe reliability different and confidence levels. - , , Hanyang , Hanyang , Swinburne

P3206 Nano-composites Meeting room 210 room Meeting P3206-1 OXIDE/ GRAPHENE POLYMER-BASED NANOCOMPOSITE FORHYDROGEL BIOMEDICAL WITH APPLICATIONS ANTIMICROBIAL PROPERTY Chang Won Lee UniversityHannam the presented We of GO/fabrication polymer composite flexibility,hydrogel with soft, antimicrobial, enhanced mechanical Itsproperty. hydrogel expected have that enhanced mechanical properties by GO the role playing physical cross-linker. P3206-3 CONDUCTIVE NANOPARTICLE ENHANCEMENTS FOR STRUCTURAL DIELECTRIC CAPACITORS KY Chan University of Technology P3206-2 P3206-2 HIGH-EMISSIVITY NANO-COMPOS ITE FOR FILM EUV PELLICLE IN APPLICATIONS SEMICONDUCTOR FABRICATION PROCESS Jinho Ahn University - , , , Tokyo , Tokyo

P3205 Liquidcomposites moulding and fibre automated placement Meeting room 209 room Meeting P3205-1 NUMERICAL SIMULATION OF RESIN FLOW THROUGH 3D FIBROUS REINFORCEMENT AT MULTISCALE ChenChaozhong CRRC Academy Metropolitan UniversityMetropolitan Permeability measurements conducted forwere one-dimensional flow unsaturated on carbon woven epoxy using fabric reduce To resin. scatter, experimental and preparation fabric arrangement materials methods were examined. P3205-3 PERMEABILITY IN EVALUATION VACUUM-ASSISTED RESIN TRANSFER - OF CAR MOLDING REIN BON FIBER FORCED PLASTICS Isono Fumiya P3205-2 P3205-2 A TWO PHASES FREECOUPLING FLOW POROUS AND MUL- METHOD AT OF LCM TI-SCALES PROCESS Arthur Cantarel Clément Ader Institute (ICA) , Rise , , Chiba

P3204 Additive manufacturing and advanced and manufacturing automation Meeting room 208 room Meeting P3204-1 INSTRUMENTED BEHAVIOR IMPACT OF PANELS PRODUCED ADDITIVEBY MANUFACTURING Whitney Thomas University of Dayton P3204-3 FLEXURAL FATIGUE OF STRENGTH 3D-PRINTED CONTINUOUS FIBER CARBON REINFORCED THERMOPLASTIC LAMINATES Morihumi Inaba Technology Institute P3204-2 OPTIMIZATION OF PROCESS FOR PARAMETERS FILAMENTFUSED FABRICATION PATH TOOL USING REVERSING Hayagrivan Vishal Sicomp A novel method to optimize process the for fused parameters fabrication filament (FFF) additive (an manufacturing istechnique) developedpaper. this in GCode instructions byused FFF the analysed is machine and a FE model of the partmanufactured is built. FE model The is optimize the to used process parameters FFF the governing process.manufacturing

MSC Software industryMSC Software workshop Meeting room 206 room Meeting MSC Software MSC industry workshop only *invitation event* MULTI-SCALE MATERIAL WITHMODELING SPEED- TO DIGIMAT UP INNOVATION IN COMPOSITE AND MATERIAL DESIGN PART Soumik Chakrabarty Emilie Storms run will workshop This for 90 minutes by Sponsored , , IRT Jules Verne , IRT , Key

P3202 Composite structures and SHM P3202-1 P3202-1 MANUFACTURING PARAMETERS OPTIMIZATION FOR MAXIMIZING STRUCTURAL PERFORMANCE AND QUALITY OF COMPOSITE PRESSURE VESSEL Seungmin Jeong Agency for Defense Development P3202-3 P3202-3 A NUMERICAL FORMODEL HYGRO- COUPLING MECHANICAL PHENOMENA IN COMPOSITE MATERIALS AbdoulMamadou Mbacke P3202-2 A TRISTABLE CROSS-SHAPED UNSYMMETRIC FIBER-REINFORCED CROSS-PLY LAMINATES: EXPERIMENTAL SIMULATION AND METHODS Li Yang Laboratory of E&M (Zhejiang University of Technology) paper presentsThis a novel cross-shaped unsymmetric fiber- reinforced cross-ply is which laminates, square- from different unsymmetricshaped fiber-reinforced cross-ply laminates stable three and has configurations. Meeting room 205 room Meeting - , WMG , , School

Polymer matrix matrix Polymer materials P3201 of Chemistry and Chemical Engineering, Hefei University of Technology Macromolecular compatibilizer POE-g- modifyGMA to used is composites.EVA results related The obvious showed improvements in the interfacial interactions, attributed was which improved the to filler dispersion and strengthened interfacial bonding induced by POE-g- GMA. A modified structure interphase accordingly was proposed and related mechanical the to performance. P3201-1 AND PREPARATION CHARACTERIZATION OF HIGH STRENGTH HIGH OILAND FLAMERESISTANT EVA RETARDANT COMPOSITES FOR CABLE Yiyang Zhou P3201-3 POLYMER TAILORED NETWORKS BY THI SEQUENTIAL - PHOTOPOL OL-ENE YMERIZATION Sergio Cespedes polymer PEG-co-TEG networks were photosynthesized in a two-step process obtain alternating to Their network structure. mechanical properties compared against were their uncontrolled counterparts. P3201-2 P3201-2 EFFECT OF ANDGRAPHENE ITS AND MWCNTS ON MODEDOSAGE I INTERLAMINER FRACTURE OFTOUGHNESS CFRP Shuanghui Cao School of Aeronautics Northwestern Polytechnical University paper to is The theenhance toughness interlaminar of unidirectional bycomposite laminate supplying graphene the into or MWCNTs a at middle interlaminar inexpensive way! Plenary 2 1110-1115 1110-1240 WEDNESDAY 14 AUGUST WEDNESDAY 1120-1125 Time 1115-1120

SCIENTIFIC PROGRAM 62 SCIENTIFIC PROGRAM SCIENTIFIC 65 , , Bristol , Bristol , Boeing , MT Meeting room 219 room Meeting Mobility between andAcademia Industry Isabelle Paris Bombardier gap the Bridging between education and employment Belcher Tony Modernising Composites Regulations Ole Thomsen University access for Increasing international to SMEs research Jevons Matt Aerospace sessionThis aims topics debate to cross betweenthat and industryacademia in a close and less environment. formal Come an join our we as animators keydiscuss topics and identify forward. ways will Each animator and a topic represent visitors can move between individual topics with or stay particularlyone that interests them. CONTINUED ′/ , , Beijing , Hiroshima Meeting room 218 room Meeting P3214-5 EFFECT OF TA ADDITION ON MICROSTRUCTURES ROOMAND TEMPERATURE FRACTURE OFTOUGHNESS THE NB-16SI-20TI- ULTRAHIGH 5AL TEMPERATURE ALLOY Long Wenyuan Hangkong Nanchang University P3214-6 SIMULATION OF THERMAL CONDUCTIVITY FOR TITANIUM BORIDE PARTICLE DISPERSED ALUMINUM COMPOSITES Gen Sasaki University P3214-4 OPTIMIZING THE MICROSTRUCTURE MECHANICAL AND OF BEHAVIORS IN-SITUΓ TIC- NI COMPOSITES SUBSEQUENTBY THERMAL TREATMENT Hu Wenqiang UniversityJiaotong , Meeting room 217 room Meeting Altair industryAltair workshop RESEARCH MEETS PRACTICE - APPLYING MULTISCALE AND MODELING OPTIMIZATION IN COMPOSITES ENGINEERING Palanterä Markku ofDirector Global Composites Business Development run will workshop This for 90 minutes by Sponsored CONTINUED - - , Korea , Indian , Harbin Meeting room 216 room Meeting P3212-4 FIBRE NATURAL HYBRID BASED POLYPROPYLENE COMPOSITES: INSIGHT AN THERMAL INTO PROPERTIES GogoiRupam of Technology Institute Roorkee, India (IIT Roorkee) Polypropylene composites(PP) by prepared were shortincorporating bamboo fiber (SBF) hollow and treated microspheresglass (HGM)and their thermo- thermal, mechanical and water behaviourabsorption analysed. were P3212-5 THE EFFECT OF NA CORE-SHELL ON NOPARTICLES STRENGTHENING TOUGHENING AND - OF POLYLAC JUTETIDE AND REINFORCEDFIBER COM POLYLACTIDE POSITE Hailing He Engineering University P3212-6 THE FABRICATION OF POLYLACTIC (PLA) /ACID CELLULOSE (CNF) NANOFIBER NANOCOMPOSITES WITH PLASTICIZER AS DISPERSING AGENT Jung Bich Nam University / Korea of Industrial Institute Technology Polylactic study, this In acid (PLA) / CNF nanocomposites were by meltprepared mixing method with (TEC) citrate triethyl as plasticizer. , , Department , Harbin Meeting room 215 room Meeting P3211-4 THE DEFORMATION FAILURE AND OF RESPONSE ULTRA-HIGH MOLECULAR WEIGHT POLYETHYLENE TO COMPOSITE LOCALIZED BLAST LOADING NguyenLong Defence Science and Group Technology Experiments were theconducted study to ofresponse UHMW-PE composite localised to The loading. blast threshold, rupture and deformation mechanisms failure was of material the in this investigated work. P3211-5 AND ANALYTICAL EXPERIMENTAL ON HIGH- STUDY TEMPERATURE HIGH-VELOCITY LIMIT FOR IMPACT C/C COMPOSITE Yang Fan of Technology Institute cloud debris The of c/c distributions composites subjected high-temperature to high-velocity oblique impacts been has analytically investigated and experimentally might test data and the design general provide guidelines for thermal protection shields. P3211-6 ABIOCHAR: POTENTIAL COMPOSITE CONSTITUENT Oisik Das of and Polymer Fibre KTH Royal Technology, of Technology Institute - - - , School , Nagoya , Nagoya , Universidad Meeting room 214 room Meeting P3210-4 EFFECTS OF PRO CESS CONDITIONS ON AEROSPACE GRADE EPOXY/ FIBRE CARBON PROP COMPOSITE ERTIES Jennings Matt of Engineering, Deakin University found that It was isostatic using when curing when pressure composites,aerospace interlaminar the and strength shear and internal the surface porosity comparable was cured Autoclave to samples. P3210-5 OBTENTION OF - A CARBON-CAR BON COMPOSITE FOR ITS MATERIAL IN EXPANDING USE NOZZLES FOR- AER VEHICLES OSPACE Liliana Maricarmen Lopez Aeronautica en Queretaro P3210-6 MINIMIZATION OF THE OUT-OF- PLANE THERMAL OF DEFORMATION REFLECTORSCFRP STACKING BY OPTIMI SEQUENCE ZATION Shun Tanaka University effectsThe of altering and optimizing the stacking sequence of as CFRP laminates a method mitigate to out-of-plane the deformation thermal fiberdue to orientation of space-basederror CFRP reflectors was investigated. , , , Beijing Meeting room 213 room Meeting P3209-4 PROPERTIES FAILURE AND OFPREDICTION HYBRID INTERPLY COMPOSITES OF GLASS AND SELFREINFORCED POLYPROPYLENE Farzaneh Hassani UniversityQueen’s Belfast P3209-5 OF IMPACT CELLULOSE FILAMENTS ON INTERLAMINAR PROPERTIES, FLAMMABILITY THERMAL AND DEGRADATION OF BEHAVIOUR MATRIX POLYMER COMPOSITES Félix Lessard Polytechnique Montréal A fibre reinforced thermoplastic composite material composed of polyamide 6 with additivefire-retardant fibre, glass (PA6-FR), and cellulose fibre was in for application tested cabin interior. aircraft P3209-6 HYBRID NANOCOMPOSITE OF ZIF-67 AND COBALT-NICKEL DOUBLE LAYERED AS HYDROXIDE ELECTROCATALYST FOR HIGHLY OXYGEN EFFICIENT EVOLUTION REACTION Feng Li University of Chemical Technology A three-dimensional CoNiAl-LDH/ZIF- nanocomposite67 exhibited excellent oxygen evolution reaction activity, due unique hierarchical to with architecture increased largely electrochemical active multi- surface area, framework,porous interfacialand intimate coupling effect. , , - , Harbin Meeting room 212 room Meeting P3208-4 ANDREDESIGN OF OPTIMIZATION PRO THERMAL TECTION SYSTEM FOR ATMOSPHERIC REENTRY Guokai Han of Technology Institute work, this In thermal of abehavior carbonlightweight and phenolic ablator thermal a hybrid has protection structure been analyzed based establishedon the model. mathematical P3208-5 EXPERIMENTAL SIMULATION AND OF GFRPSTUDY FIBRE WITH LOCAL DEFLECTION UNDER BEARING LOADS Lars Hefft Thorsten UniversityClausthal of Technology P3208-6 DAMPING OPTIMIZATION OF LAMINATED BASED PLATES ON COMPLEX MODULUS APPROACH Masaki Kameyama Shinshu University paper deals This damping the with characteristics of symmetrically plates. The laminated concept of complex ofmodulus and that parameters lamination where introduced, are complexthe stiffness newly are invariants proposed paper. in this - - , , , Sardar Meeting room 211 room Meeting Srinakharinwirot Srinakharinwirot University addition ofThe short carbon fiber wt% 25 at polybenzoxazinein the composite showed friction optimal the coefficientiswhich for personalsuitable car and significant of flexuralimprovement properties. ICAL PROPERTYICAL Jubsilp Chanchira P3207-6 LIFE FATIGUE OFPREDICTION COATING EPOXY ON COMPOSITES TO SUBJECTED WATERDROP IMPACT Ameya Kaore National Vallabhbhai of Technology, Institute Surat paper presentsThis a finite element model to lifepredict fatigue the of epoxy the coating on S-glass/epoxy composite against impact.raindrop for data rainfall The region in India Mumbai the simulate to used is This loading. fatigue model can be used predict fatigue to the life of turbine wind subjectedcoatings to erosion. rain P3207-4 P3207-4 NON-ASBESTOS POLYBENZOXAZINE COMPOSITES: FRIC- MECHAN TION AND P3207-5 WEAR PROPERTIES PITCH- AND OF PAN- CARBON BASED REINFORCEDFIBER PLASTICS WITH SIC-NANOPARTI CLES Shigenori Inoue Doshisha university testsFriction and SEM observations conducted to were wear the investigate of characteristics and pitch-based PAN- carbon fiber reinforced SiC- with plastics nanoparticles. , The , , University Meeting room 210 room Meeting P3206-6 PHOSPHATE FUNCTIONALIZED OXIDE GRAPHENE AS ADSORBENT FOR THE REMOVAL FROMOF PB(II) AQUEOUS SOLUTION Daniel Gang of At Louisiana Lafayette P3206-4 NANO-ENABLED MANUFACTURING OF AEROSPACE- GRADE THERMOPLASTIC COMPOSITES Daso Frederick Massachusetts Institute of Technology presents work This firstthe of application Out-of-oven (OoO) producing to heating carbon fiber reinforced thermoplastic specimens, which or comparable are theirbetter than conventionally producedhot-press laminates. P3206-5 MULTIFUNCTIONAL COMPOSITES WITH MODIFIED CARBON FIBERS FOR LIGHTNING STRIKE PROTECTION Anchalee Duongthipthewa Hong Kong Polytechnic University strike New lightning protection (LSP) fabricated system was GNPs- by integrating on fuzzycoated fiber composites. The damages lightning in composites with/ without LSP system predicted also were numerical the using model offering an for material alternative LSP applications. , , Tokyo , Tokyo Muthuvel, Meeting room 209 room Meeting P3205-6 A PARAMETRIC FLOW VISUALISATION OF THE WETSTUDY COMPRESSION MOULDING PROCESS Balaji University of Auckland P3205-4 ANALYSIS LINKAGE OF PERMEABILITY MECHANICAL AND EXPERIMENTS FOR CFRP Seonghun Kwak Gyeongbuk Hybrid Institute Technology time saved study This and money because carry able to it was out permeability the coefficient experiment mechanicaland the property experiment We in a lump sum. if hope future that data experimental will we accumulates, minimizebe able to cost bythe of failure many with data sharing people. P3205-5 EFFECT OF WETTABILITY ON IMPREGNATION OFPROCESS FLUID VISCOUS FIBER WOVEN TO BUNDLES Atsuki Mizuno University of Science the investigated We effectwettability of on processimpregnation of fluid viscous to fiberwoven bundles on molding resin transfer method. , - - - , Xi’an , Xi’an Meeting room 208 room Meeting P3204-6 DEVELOPMENT OF FORA TEST BENCH FILAMENTFUSED FABRICATION Alexander Matschinski Universität Technische München P3204-4 3D PRINTING OF CONTINUOUS SIZED FIBER CARBON REINFORCED PA6 COMPOSITES Liu Tengfei UniversityJiaotong A sizing treatment process successfully is the improve applied to interfacial performance and mechanical properties of 3D continuous printed carbon fiber reinforced nylon composites. P3204-5 BOND INTERLAYER OF ING BEHAVIORS 3D PRINTED CON CARBON TINUOUS REINFORCEDFIBER COMPOSITESPEEK Meng Luo UniversityJiaotong bonding interlayer The behavior by imple process the menting of pre-impregnation and was preheating laser for CCF/PEEKstudied composites extrusion avoid to AM fabrication obvious delamination.

Meeting room 206 room Meeting CONTINUED MSC Software MSC industry workshop only *invitation event* MULTI-SCALE MATERIAL WITHMODELING SPEED- TO DIGIMAT UP INNOVATION IN COMPOSITE AND MATERIAL DESIGN PART Soumik Chakrabarty Emilie Storms run will workshop This for 90 minutes by Sponsored - - - - , , IIT , Beihang

P3202-6 P3202-6 EFFECT OF LAYING METHOD ON PROP MECHANICAL ERTIES OF CON GLASSTINUOUS REINFORCEDFIBER POLYPROPYLENE PANELS SANDWICH Yiliang Sun University glass Continuous fiber reinforced polypropylene composite corrugated with panels sandwich laminates different in this prepared were effects The of paper. and panels different on the materials core mechanical properties sandwich of corrugated studied. were panels P3202-5 P3202-5 MICRO-MECHAN FAILURE ICAL OF A ANALYSIS UNI-DIRECTION COMPOSITEAL – COHSEIVE PLY ELEMENTS & A FRACTUREDUCTILE APPROACH Akash Sharma Indore of behavior failure The a uni-directional (UD) carbon fiber reinforced epoxy composite ply subjected to tension, transverse compression and shear studied was loads computationalusing micro-mechanics.In the capture to order plastic epoxy matrix and the deformations subsequent damage, a ductile fracture used was criterion within combination linear extendedthe Drucker-Prager plasticity model. P3202-4 P3202-4 NONLINEAR FINITE ELEMENT ANALYSIS OF COMPOSITE LAP-JOINTS BOLTED VS : EXPERIMENTAL TESTS. NUMERICAL Benoit Montagne Clément AderInstitut Meeting room 205 room Meeting , The , Beihang , Institute of , Institute P3201-6 OF THE INFLUENCE DIFFERENT POWDER IMPREGNATION ONPROCESSES THE PROPERTIES OF L-SHAPED FABRIC WOVEN REINFORCED PEEK COMPOSITES STAMP HOT BY FORMING LiuHansong University University of Tokyo effectsThe of moisture on the and temperature propertiesfexural of carbon fiber reinforced polyamide 6 materials researched in this were study. P3201-5 THE EFFECTS OF MOISTURE AND ON TEMPERATURE THE FLEXURAL PROPERTIES OF FIBER CARBON REINFORCED PAPER THERMOPLASTICS/ 6 POLYAMIDE Xiangdong He P3201-4 AND PREPARATION CHARACTERIZATION OF MODIFIED POL- ALCOHOL/ YVINYL ALGINATE SODIUM HYDROGEL Jianle Gong ProcessingMaterials and Intelligent Manufacturing, Harbin Engineering University Plenary 2 1125-1130 WEDNESDAY 14 AUGUST WEDNESDAY 1135-1140 Time 1130-1135

SCIENTIFIC PROGRAM 64 SCIENTIFIC PROGRAM SCIENTIFIC 67 , , Bristol , Bristol , Boeing , MT Meeting room 219 room Meeting Mobility between andAcademia Industry Isabelle Paris Bombardier gap the Bridging between education and employment Belcher Tony Modernising Composites Regulations Ole Thomsen University access for Increasing international to SMEs research Jevons Matt Aerospace sessionThis aims topics debate to cross betweenthat and industryacademia in a close and less environment. formal Come an join our we as animators keydiscuss topics and identify forward. ways will Each animator and a topic represent visitors can move between individual topics with or stay particularlyone that interests them. CONTINUED , , State , Huazhong , Huazhong Meeting room 218 room Meeting P3214-8 OF PREPARATION IN-SITU AND SICNP HYBRID MG2SI PARTICULATES REINFORCED MATRIX AL-CU COMPOSITES Wu Shusen Key Lab of Materials Processing and Die & Mould Technology, University Huazhong of Science and Technology P3214-9 W/TIN/ A NOVEL COMPOUND TA CHARGE SHAPED LINER ZiZhi Yan P3214-7 P3214-7 OF EVALUATION INTERFACIAL THERMAL OF RESISTANCE AL-ALN PARTICLE DISPERSED COMPOSITES USING BY IMAGE-BASED CALCULATION Kenjiro Sugio Hiroshima University Interfacial thermal Al- in resistance AlN composites by evaluated was thecomparing thermal measured conductivity and the thermal calculated conductivity. University of Science & Technology and his Yan Mr devoted have team themselves the to of tougheningstudy technology of tungsten composites for years,many hoping the promote to ofapplication tungsten in industry. , Meeting room 217 room Meeting Altair industryAltair workshop RESEARCH MEETS PRACTICE - APPLYING MULTISCALE AND MODELING OPTIMIZATION IN COMPOSITES ENGINEERING Palanterä Markku ofDirector Global Composites Business Development run will workshop This for 90 minutes by Sponsored CONTINUED , , Javanshour, Javanshour, Meeting room 216 room Meeting P3212-7 EVALUATION OF TENSILE PROPERTIES AND ABSORPTION WATER FIBER OF ABACA THERMOPLASTIC COMPOSITE FIBER TO RELATIVE TYPELENGTH, AND OF MATRIX ADDITIVES Marissa Paglicawan Department of Science and Technology- Technology Industrial Development Institute Effects shortof abaca fibers, milled fiber fabric,and woven treatment,NaOH anhydride maleic and nanoprecipitated calcium on carbonate properties tensile the absorption and water of composites the was studied. P3212-8 ELABORATION MECHANICAL AND CHARACTERISTICS OF FLAX-PCL COMPOSITES AND SANDWICHES BizetLaurent Université Havre Le Normandie compositesFlax have been manufactured polycaprolactonewith (PCL) to in order matrix obtain biodegradable composites. Flax fibers assembled in unidirectional fabrics and flax shives have been different used as reinforcements. P3212-9 AND THERMAL MECHANICAL OF BEHAVIOUR FLAX YARNS MODIFIED WITH OXIDE GRAPHENE Farzin University Tampere work, this In the of graphene potential to oxide treatment flax-epoxyimprove inadhesion, increase stability thermal the of flax fibres and their mechanical properties over 200 °C processing are temperatures studied. - - , , Beuth , Beijing Meeting room 215 room Meeting P3211-7 P3211-7 ADVANCED QUALIFICATION AOF COMBOO - BAMBOO BASED CORE MATERIAL Andreas Loth P3211-8 STUDY FACTORIAL AND OF MATERIAL PARAM PROCESS ETERS ON FIRE MECHANICAL AND PROPERTIES OF WHEAT AND WOOL COMPOS GLUTEN ITES Kim Kyeun Nam Centre for Advanced Composite Materials, Engineering Mechanical Department, The University of Auckland has research The the investigated conditionsdesirable and of material manufacturing enhance to parameters andfire resistant mechanical properties of and gluten wool composites.based P3211-9 BAMBOO BASED BIO-COMPOSITES UNDER DAMAGED UNDAMAGED AND FRACTURE LiuWen Forestry University University of Applied Science , Beihang , The , Hefei University Meeting room 214 room Meeting P3210-7 P3210-7 VIBRATION FREQUENCY STUDY AND DESIGN OF COMPOSITE FUSELAGE STRUCTURE Kaijian Wang University P3210-8 ANDDESIGN OF ANALYSIS FILAMENT-WOUND COMPOSITE PRESSURE VESSELS ON MESH BASED THEORYWINDING Xu Hui P3210-9 A COMPUTATIONALLY EFFICIENT APPROACH FOR THE ANALYSING ONSET OF FAILURE IN AEROSPACE COMPOSITE STRUCTURES Shibo Yan of Technology University of Nottingham , , , Institute of , Institute Meeting room 213 room Meeting P3209-7 P3209-7 GAMMA-RAY SHIELDING PROPERTY OF TUNGSTEN/BASALT REINFORCEDFIBER MATRIX EPOXY COMPOSITES BY FABRICATED TWO TUNGSTEN WAYS HYBRID Ran Li Aerospace and Material Technology P3209-8 EFFECT OF ARAMID ON CLOTH FIBER CARBON/ARAMID REINFORCEDFIBER THERMOPLASTICS Hisaki Matsuda Department of Systems TheInnovation, University of Tokyo Carbon/aramid hybrids interlayer continuous with were cloths aramid and manufactured and dynamicstatic carried tests were out. aramid The improved the cloths toughness of CFRTP and dynamicin flexural tests. P3209-9 THE SPRAYING HOW OF GRAPHENE NANOPLATELETS CHANGES MECHANICAL PROPERTIES OF FIBRE CARBON REINFORCED POLYMER? Marzena Pawlik University of Derby investigates study This effectsthe of graphene nanoplatelets, sprayed carbonon the fibre fabric, and on flexural propertiesinterlaminar of CFRP composites. , , Nanjing , University of Meeting room 212 room Meeting P3208-7 P3208-7 CLASSIFICATION PROPERTIESAND OF THREE- DIMENSIONAL TEXTILE PREFORMS Ma Zhenyu University of Aeronautics and Astronautics the paper, this In 3D textile preforms classified,were and representative three unitsgeometric proposed, were (RGUs) namely orthogonal unit,geometric skew unitgeometric and curved geometric unit. Other units were andcombinations of thesederivations RGUs. three P3208-8 LIGHTWEIGHT OFDESIGN BODY COMPOSITE FOR ELECTRIC MICROBUS Pongpat Sirisobrana King Mongkut’s University of Thonburi Technology (KMUTT) paper presentsThis designthe and optimization of structure sandwich of and glass consisting carbon fiber/epoxy for and foam core face electric microbus. P3208-9 BUCKLING OF ANALYSIS MULTILAYERED BEAMS WITH SOFT RIGID AND INTERFACES An Le Sydney Technology , Shanghai , Shanghai , Harbin Institute , Harbin Institute Meeting room 211 room Meeting of Technology researchs work This behavior fatigue the of laminate, bistable gives critical load the changes the with ofnumber cycles and presents a creep model the explain to of range attenuation critical load. the P3207-9 P3207-9 MODEL A CREEP FOR THE FATIGUE OF BEHAVIOR BI-STABLE HYBRID LAMINATE Li Yanqi P3207-7 TRIBOLOGICAL CHARACTERISTICS OF MICROWAVE KENAF/ PROCESSED COMPOSITESHDPE UNDER DRY SLIDING WEAR Manoj Singh, Kumar of Indian Institute Mandi Technology behaviour Tribological of microwave processed kenaf/ HDPE composites assessedwere a using tribometer. pin-on-disc effectThe sliding the of observedspeedwas coefficienton the of friction and specific rate. wear P3207-8 THE INFLUENCE ON THE OF FABRIC WEAR-RESISTING PROPERTY OF SELF-LUBRICATING COMPOSITS Mingming Yu University ------, , Meeting room 210 room Meeting P3206-8 EFFECT OF CARBON NANOTUBES CONTENT ON THE FRACTURE OF PP/ BEHAVIOR EPDM/MWCNT BLEND-NANOCOM POSITES UNDER QUA AND DYNAMIC LOADING SI-STATIC Mehrdad Khodabandelou, Sahand University of Technology of increase The MWCNT content a contradictoryhas effect the fracture of toughness under dynamic loading and loading. quasi-static demonstrated It was contradiction this that different from originates toughening dominant PP in the mechanisms under both test matrix conditions. P3206-9 COPPER COBALT ENCAPSU ALLOYS MOS2/N- BY LATED GRAPHENE DOPED NANO-HETERO STRUCTURES FOR ORR APPLICATION HoonNam Kim Chonbuk National University work, this In a hybrid containing cobalt-cop per alloys encapsulated 2D-molybdenum di sulfide/nitrogen-doped (CuCo@2D- graphene MoS2/N-Gr) syn is thesized by a simple treatment thermal a as and investigated catalyst for oxygen re duction reaction (ORR) in alkaline solution. P3206-7 P3206-7 PERCOLATION LOW OFTHRESHOLD POLYPROPYLENE SPECIALLY DESIGNED GRAPHENE NANOCOMPOSITES Karolina Gaska Chalmers University of Technology presents work This relevant industrially systemmelt-mixed of polypropylene and speciallyhierarchically designed reduced oxide.graphene Exceptionally low electrical percolation been has threshold study. in this presented , , Nihon , Meeting room 209 room Meeting P3205-9 PEFORMANCE AND MONITOR OF APREDICTION LOADED BIAXIALLY THIN COMPOSITE TUBE Md Shamsuddoha University of New South Wales Compressive loading in conjunction with oftorsion hollow composite is tube plastic critical due to buckling formed micro helically around study This tube. the investigate to aims of hollowbehaviour composite tubes with hole underround combined and torsion compression loads, and compared with finite element analysis. P3205-7 P3205-7 EFFECTOF FLAME RETARDANT THE ON FILTRATION FIRE PERFORMANCE FIBRE OF CARBON REINFORCED EPOXY COMPOSITES MADE RESIN TRANSFER BY MOULDING Ákos Pomázi UniversityBudapest and of Technology Economics effectThe of flame on filtration retardant fire performancethe in investigated was ofcase carbon fibre reinforced low-viscosity epoxy composites bymade liquid composite moulding techniques, as such moulding. resin transfer P3205-8 OF EVALUATION MECHANICAL PROPERTIES FOR IN CFRTP USING SITU-POLYMERIZING THERMOPLASTIC URETHANE RESIN Sugita Tsuyoshi University newly developedThe in situ-polymerizing urethane thermoplastic excellentresin has moldability like resin,thermosetting and CFRTP it has using excellent mechanical properties. - - , , Deakin , Department Meeting room 208 room Meeting University of New South Wales re-meltingApply laser process the to additive manufactuing Metal of Ti-Ni_C CompositesMatrix and investigate improvement the of microstructure, hardness and mechanical properties. P3204-9 EFFECTS OF CURE PRESSURE CYCLE AND PROFILE ON RATE HEATING PROPERTIES OF OUT-OF-AUTOCLAVE CURED RAPIDLY FIBRE CARBON COMPOSITES Sima Kashi University P3204-7 THE IMPROVING STIFFNESS OF HIGH RESOLUTION DLP STEREOLITHO GRAPHIC MATERIAL Chow-Shing Shin of Mechanical Engineering, National University Taiwan modulus Young’s The of stereolitho DLP can material graphic markedlybe increased theby decreasing thickness layer curing and adding suitable of CNTconcentration particles.or alumina P3204-8 EFFECT OF LASER RE-MELTING ON THEPROCESS MICROSTRUCTURE MECHANICAL AND PROPERTIES OF ADDITIVELY MANUFACTURED MATRIX METAL COMPOSITES Jianshen Wang

Meeting room 206 room Meeting CONTINUED MSC Software MSC industry workshop only *invitation event* MULTI-SCALE MATERIAL WITHMODELING SPEED- TO DIGIMAT UP INNOVATION IN COMPOSITE AND MATERIAL DESIGN PART Soumik Chakrabarty Emilie Storms run will workshop This for 90 minutes by Sponsored , , Indian Zhou, Nanjing

P3202-9 P3202-9 STATIC QUASI COMPRESSIVE OF CFRP RESPONSE HONEYCOMB CORE FILLERS WITH FOAM Hao University of Science and Technology CFRP honeycomb PMIwith foam fillers proposed as was sandwich a hybrid static quasi The core. compressive response of was core the analyzed numerically. P3202-8 P3202-8 INVESTIGATION 3D PRINTINGINTO USING OF CFRP COVERING YARN COMPOSITE Yoshizawa Takato Doshisha University aimed we study, this In the understand to influence of molding usingconditions when CFRP covering with incomposite yarn on resin 3D printer andimpregnation mechanical properties. P3202-7 P3202-7 KINKING INMECHANICS COMPOSITES UNDER COMBINED LOADING Sachin Vankar of Technology Institute Bombay An analytical approach been developedhas for kinking mechanics under combined compression- loading fortorsion unidirectional carbon fibercomposite. A unit single fiber-matrix by considered is using a fiber deformation with representation fiber andamplitude fiberrotation. Meeting room 205 room Meeting , Ioffe , Xi’an , P3201-9 LINEAR AND NONLINEAR ELASTIC PROPERTIES OF POLYSTYRENE- BASED NANOCOMPOSITES SemenovaIrina Institute Polystyrene-based composites filled with particles of different type were and shape by meltfabricated Their technology. linear and nonlinear propertieselastic were estimated. P3201-8 OF COMPARISON CARBON SHORT POLY(P- AND PHENYLENE-2,6- BENZOBISOXAZOLE) FIBERS ON THE PROPERTIES OF POLYESTER THERMOPLASTIC ELASTOMERS Adam Pearson University of Toronto Thermoplastic been have elastomers shortreinforced with carbon and PBO fibers. fibers the While base similar have mechanical properties of the strength the compositesPBO is carbon to superior reinforcement. P3201-7 P3201-7 DEFORMATION MECHANISM INVESTIGATION BYFOR EPOXY IN-SITU MECH- ELETRIC COUPLING MEASUREMENT MiaoYinggang Jiaotong UniversityJiaotong Epoxy modified is with CNT reinforces which conductivitythe of composites. mech-electricThen of measurement compositesthe performedare for analysing the deformation potential the at mechanism peak stress of epoxy materials. Plenary 2 1140-1145 WEDNESDAY 14 AUGUST WEDNESDAY 1150-1155 Time 1145-1150

SCIENTIFIC PROGRAM 66 SCIENTIFIC PROGRAM SCIENTIFIC 69 , , Bristol , Bristol , Boeing , MT Meeting room 219 room Meeting Mobility between andAcademia Industry Isabelle Paris Bombardier gap the Bridging between education and employment Belcher Tony Modernising Composites Regulations Ole Thomsen University access for Increasing international to SMEs research Jevons Matt Aerospace sessionThis aims topics debate to cross betweenthat and industryacademia in a close and less environment. formal Come an join our we as animators keydiscuss topics and identify forward. ways will Each animator and a topic represent visitors can move between individual topics with or stay particularlyone that interests them. CONTINUED , Southwest Meeting room 218 room Meeting P3214-10 P3214-10 STRENGTHENING OF PURE MATRIX AL IN- COMPOSITES BY SITU SYNTHESIZED NEEDLE AL-O NANO PHASE Xinxin Zhu UniversityJiaotong Al matrix in-situ The composites were synthesized by mechanical milling by oscillatoryfollowed press sintering, producing an excellent mechanical properties and ambient both at temperatures. elevated , Meeting room 217 room Meeting Altair industryAltair workshop RESEARCH MEETS PRACTICE - APPLYING MULTISCALE AND MODELING OPTIMIZATION IN COMPOSITES ENGINEERING Palanterä Markku ofDirector Global Composites Business Development run will workshop This for 90 minutes by Sponsored CONTINUED , , , , ETRI Meeting room 216 room Meeting P3212-10 ANDGREEN FIBRE NATURAL COMPOSITES PANEL FROM BAMBOO-A OF THE MATERIAL FUTURE Nagammanavar Uday IPIRTI IPIRTI developed has ofnumber bamboo structural based products Bamboo like (BMB), Board Mat to alternative as plywood, Bamboo Sheet Corrugated Mat (BMCS) alternative as roofing corrugated to sheets,Bamboo Tiles,BambooFlooring Boards. Particle/Fibre P3212-11 ONE-STEP EXTRACTION OF CELLULOSE NANOCRYSTALS USING ONLY HIGH-PRESSURE HOMOGENIZER Park Nae-man A simple and green process produce to cellulose nanocrystals by only using a high homogenizerpressure proposed. Itsis yield is about 80%. P3212-13 TUBE FROM MADE POLYLACTIC AND YARN ACID BY YARN SILK FILAMENT WINDING TECHNIQUE Srisawat Natee UniversityRajamangala of Technology Thanyaburi P3212-12 P3212-12 RESEARCH ON COMBUSTION OF BEHAVIOR COMPOSITE HYBRID FIRE BY DYNAMICS SIMULATOR Hee Park Yoon National Changwon University As a result, some errors but the generated, are behavior combustion Research is similar. is needed accurately to factorsimplement that and surroundings affect ignition time and to in order behavior reduce errors. , Meeting room 215 room Meeting P3211-10 CHARACTERIZATION THERMAL AND EFFECTON MECHANICAL PROPERTIES OF BIOMATERIAL- REINFORCED- POLYPROPYLENE Anh Dung Ngo École De Technologie Supérieure , , , Gifu , Kyoto Meeting room 214 room Meeting P3210-10 AND SIMULATION EXPERIMENTS FOR MECHANICAL PROPERTIES THE DOMINATING PRESS MOLDING CFRTP USING PREFORMS Yuji Abo University pressThe molding CFRTPusing attracts reduce to attention production times. pull-outThe and propertyshear of CFRTP preforms examined,were and models for preforming made. were simulation P3210-11 DEVELOPMENT OF BENDING FORPROCESS THERMOPLASTIC COMPOSITE DURING PIPE PULTRUSION PROCESSMOLDING Asami Nakai University P3210-13 ANDDESIGN OF ANALYSIS COMPOSITE FIBER CARBON REINFORCED ANTI- BEAM COLLISION ON ANSYS BASED ACP Chuanxiang Zheng Zhejiang University P3210-12 PRESS AND HYBRID INJECTION OF GF/ MOLDING HAT-SHAPED PP AND MEMBER OF ITS EVALUATION PROPERTYBENDING Tanaka Kazuto Doshisha University bending propertiesThe of molded hybrid GF/PP hat-shaped member were and FEMevaluated carried analysis was out clarify to the betweenrelationship cost and material mechanical properties. , Paderborn Meeting room 213 room Meeting P3209-10 CFRP-STEEL WITH HYBRIDS AGEING IMPROVED RESISTANCE THROUGH ZINC - NANORODS OXIDE OF INVESTIGATION MECHANISMS BASIC Jan Striewe University on Investigations modethe of action and influence of wet- an innovative chemical surface of steel pre-treatment on the substrates ageing of resistance of made steelhybrids and carbon fibre- reinforced plastic. Meeting room 212 room Meeting , , Technische , Technische , Xi’an Jiaotong Meeting room 211 room Meeting P3207-10 SHORT-TIME APPROACH FOR LIFE FATIGUE OF ESTIMATION MULTIFUNCTIONAL COMPOSITES Sebastian Backe, TU Kaiserslautern A newly developed forshort-timeapproach life estimationfatigue of multifunctional composite laminates based on single load tests isincrease introduced. P3207-11 LIFE FATIGUE FOR WIND ANALYSIS TURBINE GEAR SHAFT WITH OXIDE INCLUSION Ran Liu University Technical University ofTechnical Denmark of compositeUsage cruciform specimens for planar-biaxial testing are fatigue finite using evaluated element analysis for their uniformity in the strain stress and the in their biaxial state zones. P3207-12 P3207-12 INVESTIGATION ON HOMOTHETIC FAILURE IN ENVELOPES THE LAYER-BASED ANALYSIS FATIGUE OF CFRP MöllerMarc Köln Hochschule paper present The withmainly deals designthe of homothetic fatigue envelopesfailure cyclicunder multiaxial stresses for residual based fatigue strength analyses. P3207-13 CRUCIFORM DESIGNS SPECIMEN FOR PLANAR FATIGUE BIAXIAL TESTING IN COMPOSITES Aakash Moncy - - - , , Hiroskai , Kobe , Xi’an Meeting room 210 room Meeting P3206-10 COBALT PHOSPHIDES COPPER COATED NANOROD OXIDE FOR ARRAYS ENHANCED WATER OVERALL SPLITTING Joong Hee Lee Chonbuk National University report we Herein, cost-effectivethe of cobaltfabrication phosphides coated copper oxide nanorod supportedarrays 3D foam (Co2P@CuO NR/CF) an efficient as electrocatalyst for in splitting water overall alkaline condition. P3206-11 ELECTROMAGNETIC PROPERTIES OF KH560/RGO@ FE3O4/TIO2/ WAX PARAFFIN IN 0.5- COMPOSITE FREQUENCY GHZ 18 Li Yuexuan UniversityJiaotong Si-modified KH560/ RGO@Fe3O4/TiO2 composite successful is synthesized by a facile reaction. hydrothermal Its RL maximum value optimized -20.9 is to a with GHz dB 8.6 at thickness of 6 mm. P3206-12 OF ANALYSES MECHANICAL REINFORCEMENT FOR CELLULOSE NANOFIBERS/CLAY NANOCOMPOSITES X-RAY USING DIFFRACTION Shunichi Mori University employed We cellulose nanofiber (CNF) as a matrix and montmorillonite (MMT) then a filler, as CNF/MMTprepared nanocomposites. mechanicalThe effectreinforcement based-on interfacial betweeninteraction CNF and MMT was by “X-rayinvestigated diffraction method”. P3206-13 OF PREPARATION END- FLUOROALKYL OLIGOMER/ CAPPED MAGNETITE NANOCOMPOSITES – APPLICATION WATER/OIL TO SEPARATION Hideo Sawada University end-cappedFluoroalkyl vinyltrimethoxysi oligomer/magnet lane composites,ite which by prepared were composite reaction of oli corresponding the magnetite,gomer with effectivelycan adsorb oil on droplets spread interface water the under a magnetic field. , , University of Meeting room 209 room Meeting P3205-10 INTRA-LAMINAR INTER-AND LAMINAR PROGRESSIVE ANALYSIS FAILURE COMPOSITEOF AFP LEVEL ON A TOW Xie Li New South Wales levelA tow numerical modelling technique been to introduced has precisely more capture progressivethe failures of AFP composite inclusion the with of process-induced defects. P3205-11 AND SIMULATION TEST VERIFICATION OF PREPREG PEEL FOR PLACEMENT PROCESS Xianzhao Xia Hefei University of Technology , - , Gifu , Kindai Meeting room 208 room Meeting P3204-10 AUTOMATED HIGLY MANUFACTURING OF LARGEPROCESS AIRPLANE CFRP STRCTURES Malecha,Marcin German Aerospace Center automated present We forapproach of large manufacturing made structures aircraft of dry non-crimped carbon from fabrics logistics material bagged vacuum to in a singlepreform smart process. P3204-11 CONTINUOUS TAPE MOLDING LAYUP OF BEHAVIOR NEAR-CFRTP USING INFRARED HEATING INDUCTIONAND HEATING Naoki Nakata University layup study, this In process of CF/ tape prepreg to PA6 predict optimum the processing condition for carbon fiber tape layup continuous molding equipment developed in. P3204-12 P3204-12 IMPREGNATION IN OPEN PROCESS METHODMOLDING MULTI- USING FILAMENT WINDING Otake Kazuma University heater the study, this In position and the temperature heating and changed, were impregnated the of moldsstates the compared and were byevaluated observing crossthe section, and condition heating the examined. was P3204-13 PROGRESS IN STRUCTURAL POLYMER TAILORED INSERTS; TRENDS STRATEGIES AND FUNC- TOWARDS POLYMERIC TIONAL REIN INTER-PLY FORCEMENTS Sithila Theminimulla Deakin University of smart world The offers a materials progress towards intelligent a more design materials work This philosophy. examines progress utilisationin the of modified thermoplastic additives as multifunctional strain elements.sensing

Meeting room 206 room Meeting CONTINUED MSC Software MSC industry workshop only *invitation event* MULTI-SCALE MATERIAL WITHMODELING SPEED- TO DIGIMAT UP INNOVATION IN COMPOSITE AND MATERIAL DESIGN PART Soumik Chakrabarty Emilie Storms run will workshop This for 90 minutes by Sponsored - - - - - , - , , , Harbin

P3202-11 P3202-11 VISUAL DAMAGE SYSTEM INDICATION FOR POLYMER COMPOSITE STRUCTURES Bulderberga Olga University of Latvia new conceptThe health of structural formonitoring polymer composites is bypresented damage indication visual concept The system. colour on the based is place in the change of applied the over load. thresholding P3202-10 P3202-10 ELECTROMECHAN OF RESPONSE ICAL MULTIFUNCTIONAL PIEZOELECTRIC COMPOSITES Krishna Challagulla UniversityLaurentian work present The extends previous the by authors the study on piezoelectric foam multifunc to structures compositetional struc by enclosingtures the with foam structures symmetric interconnect (acts ofmade PZT-7A within first as phase) piezoelectric materials second(acts as phase); titanate (i) barium and relaxor (BaTiO3), ferroelectrics (PMN- 33%PT) (ceramic-ce piezoelectricramic composites), and (ii) polyvinylidene fluoride (PVDF) (ceramic-pol ymer piezoelectric composites). P3202-13 P3202-13 MECHAN SMART OLUMINESCENT MEMORY SHAPE FORFILM FLEXIBLE STRESS SENSING He Yang of Technology Institute P3202-12 P3202-12 EXPERIMENTAL CHARACTERIZATION MODELLING AND OF MECHANICAL OF BEHAVIOR IN MICROCAPSULES COMPOSITES Andrey Aniskevich University of Latvia behaviorMechanical of single microcapsule and embedded in polymer matrixes investigated was experimentally and modelled analytically and numerically. Meeting room 205 room Meeting , , Beijing P3201-11 P3201-11 COMPRESSION PROPERTIES OF MULTIFUNCTIONAL LAMINATES CFRP WITH EMBEDDED LITHIUM-ION POLYMER BATTERIES Pooneh H.M Attar RMIT University Institute of Astronautical Institute Systems Engineering P3201-10 HIGH TEMPERATURE COMPRESSION PROPERTIES OF CFF/PPS COMPOSITE LAMINATES BY FABRICATED STACKING FILM TECHNIQUE Shixun Wang Plenary 2 1155-1200 WEDNESDAY 14 AUGUST WEDNESDAY Time 1200-1205 1205-1210 1210-1215

SCIENTIFIC PROGRAM 68 SCIENTIFIC PROGRAM SCIENTIFIC 71 , , Bristol , Bristol , Boeing , MT Meeting room 219 room Meeting Mobility between andAcademia Industry Isabelle Paris Bombardier gap the Bridging between education and employment Belcher Tony Modernising Composites Regulations Ole Thomsen University access for Increasing international to SMEs research Jevons Matt Aerospace sessionThis aims topics debate to cross betweenthat and industryacademia in a close and less environment. formal Come an join our we as animators keydiscuss topics and identify forward. ways will Each animator and a topic represent visitors can move between individual topics with or stay particularlyone that interests them. CONTINUED Meeting room 218 room Meeting , Meeting room 217 room Meeting Altair industryAltair workshop RESEARCH MEETS PRACTICE - APPLYING MULTISCALE AND MODELING OPTIMIZATION IN COMPOSITES ENGINEERING Palanterä Markku ofDirector Global Composites Business Development run will workshop This for 90 minutes by Sponsored CONTINUED Meeting room 216 room Meeting Meeting room 215 room Meeting Meeting room 214 room Meeting Meeting room 213 room Meeting Meeting room 212 room Meeting Meeting room 211 room Meeting - - , , Inje , Inje , Hanam , Hanam , Beijing Meeting room 210 room Meeting P3206-18 IN VITRO OF STUDY BIOFUNC - A NOVEL FOR TIONALIZATION SCAFFOLD 3D PDMS MODI VIA SURFACE FICATION Baek Ji Hun University PDMS fabricated We nanosheets using Then,electrospinning. nanosheetsPDMS modifiedsurface were a biocompatiblewith stimulates that material and cell proliferation differentiation. P3206-16 MELT ELECTROSPINNING: ECO-AN OF WAY FRIENDLY AND NANOFIBER GRAPHITIZED FIBRE PREPARATIONS USING NANOCELLULOSE Haoyi Li Chemical Technology University P3206-17 MULTILEVEL RESISTIVE IN SWITCHING SILVER NANO INCORPORATED THIN CHITOSAN FILMS Sreedevi Vallabhapurapu P3206-14 DOT/ CARBON POLYPYRROLE NANOPARTICLE COMPLEXES AS MULTIFUNCTION THERANOSTICAL AGENTS Kim Eun Tae University carbon study, this In dots combined are polypyrrole the with nanoparticles make to a novel PTT-imaging agent. complexes The can be utilized as agents bytheranostic time. in real monitoring P3206-15 QUANTUMCARBON USING DOTS POLYPHENOL COMPOUNDS:SKIN ANTI-AGING SeokWon Park University carbon study, this In dotsquantum synthesizedare polyphenolusing compounds. We confirmed the applicability of carbon dots an as quantum substance. anti-aging University of South Africa silverNano incorporated Chitosan films thin by prepared were coating. simple spin carefulOur I-V shows measurements multilevel switching of the characteristics chitosan and silver film for one layer. Meeting room 209 room Meeting Meeting room 208 room Meeting

Meeting room 206 room Meeting CONTINUED MSC Software MSC industry workshop only *invitation event* MULTI-SCALE MATERIAL WITHMODELING SPEED- TO DIGIMAT UP INNOVATION IN COMPOSITE AND MATERIAL DESIGN PART Soumik Chakrabarty Emilie Storms run will workshop This for 90 minutes by Sponsored , , , , University

P3202-17 MULTIFUNCTIONAL STRUCTURAL STORAGE ENERGY COMPOSITES Feng Huang of New South Wales New structural concepts for composite be will batteries developed store to electrical energy, without sacrificing mechanical strength and stiffness. Examples include designing new storage energy cores for sandwich either using structures orsupercapacitor batterylaminated techniques. P3202-16 P3202-16 OF STRAIN SENSING RESIN USING EPOXY CARBON POROUS NANOTUBE/ GRAPHENE COMPOSITE BUCKYPAPER Guangming Yang University Tongji Carbon Porous nanotube/Graphene Buckypapers are for strain fabricated ofsensing epoxy resin. obtained strain The exhibitedgauges a high high GF of 10.83, linearity (R2 =0.987) and good cycle stability. P3202-15 P3202-15 INFLUENCE OF OPTICAL SENSOR FIBER PLACEMENT ON LAMINATES CFRP FOR PROCESS STRUCTURALAND HEALTH MONITORING Helena Rocha P3202-14 P3202-14 DAMAGE DETECTION USING DIRECT-WRITE PIEZOELECTRIC TRANSDUCERS LAMBAND WAVES IN COMPOSITE MATERIALS Marilyne Philibert IMRE, A*STAR, Singapore objectiveThe to is apply direct-write on CFRP transducers for active sensingplate of by impact damage non-ceramic using an with P(VDF-TrFE) for electrode patterned mode selection. University of Minho the studied We influence of embedded optical fibers on the mechanical properties of CFRPs. FBG OF with used for were sensors and monitoring cure detection of barely impactvisible damage. Meeting room 205 room Meeting Plenary 2 1215-1220 WEDNESDAY 14 AUGUST WEDNESDAY Time 1220-1225 1230-1235 1225-1230 1235-1240

70 SCIENTIFIC PROGRAM SCIENTIFIC PROGRAM SCIENTIFIC 73 , Korea , Tokyo , Tokyo , Southwest 3315 Metal matrix composites Meeting room 219 room Meeting 3315-1 3315-1 STRENGTH EVADING DUCTILITYAND TRADE-OFF IN BIO-INSPIRED HIERARCHICAL MAGNESIUM-BASED NANOCOMPOSITE Xi Luo UniversityJiaotong propose an We structure inverse-nacre flaky the soft which embedded are phases matrix,in a hard to trade-offevade the andbetween strength ductility. 3315-2 3315-2 INJECTION METAL OF CU/CF MOLDING COMPOSITES Osada Toshiko UniversityMetropolitan compositesCu/CF fabricated were MIMthorough process. Effects of fiber contents and fiber orientation mechanicalon the properties were investigated. 3315-3 QUANTITATIVE OF ANALYSIS REINFORCEMENT IN DISPERSION MATRIX METAL COMPOSITES Byeongjin Park of Materials Institute Science An automated analysisdispersion istechnique proposed quantify to reinforcement in metaldispersion compositesmatrix minimizedwith interruption human by integrating processing,image analysis,statistical and computational intelligence. , , , Shanghai , Shanghai 3314 Fatigue Meeting room 218 room Meeting 3314-1 3314-1 A NEW CONSTANT DIAGRAMLIFE FORMODEL UD LONGITUDINAL FATIGUE LiFangfang Polytechnic University A new life constant model (CLD) diagram asymmetric featuring bilinear constant-life curves proposed was better describeto longitudinal the of behavior fatigue unidirectional laminae (UD) under a wide of stress ratios. range Technical University ofTechnical Denmark 3314-2 3314-2 EXPERIMENTAL INVESTIGATION OF THE DAMAGE THE TIP OF AT TUNNELING CRACK IN GLASS FIBRE COMPOSITES Ashish Bangaru Kumar 3314-3 OFDESIGN COMPOSITE STRUCTURE UNDER VARIABLE AMPLITUDE FATIGUE USING LOADS LAMINATE LOCAL PREDICTIONS LIFE Subbareddy Daggumati IIT Indore damage Fatigue analysis of composite under laminates amplitude variable presented is loads twousing analyticaldifferent methodologies, namely: i) Piecewise Constant Life (PCLD) Diagrams within combination damage Miners ii) PCLD asum; with progressive damage obtainedmodel. The analytical results are thecompared with spectralexperimental results.fatigue , , Bristol , Bristol , UTC

3313 tolerance Damage Meeting room 217 room Meeting 3313-1 COMPRESSION AFTERSTRENGTH ANALYSIS IMPACT DISCRETE USING MODELING DAMAGE Jeffrey McQuien atUniversity of Texas Arlington Research Institute Regularized- The Extended Finite Method Element perform used to was damage discrete modeling of impact- induced delamination cracks and matrix scopein the of compression after impact analysis. 3313-2 AN ENERGY- EQUIVALENT LAW COHESIVE FOR MODELLING Z-PINNED COMPOSITE LAMINATES Antonio Melro Institute Research 3313-3 THROUGH- Z-PIN THICKNESS ENHANCEMENT OF A COMPOSITE LAMINATE WITH VARIABLE THICKNESS Joël Serra Composites - University of Bristol A multi-scale been has framework developed for the modelling ofnumerical composite laminates z-pins reinforced with to and submitted delaminations several of mode- different mixities. , , York , York , Kaist

3312 methods Testing Meeting room 216 room Meeting 3312-1 OF EVALUATION MECHANICAL PROPERTIES OF COMPOSITE PRESSURE VESSELS A SEGMENT- USING TYPE RING BURST TEST DEVICE Kim Woetae verify stability the To of vessel, pressure this thepaper with deals development of a new segment-type ring test device.burst 3312-2 A REVIEW OF MECHANICAL TESTING OF COMPOSITE LAMINATES McEnteggartIan Instron A review of the test typesmain and fixtures associated determine to used bulk propertiesthe of composite laminates. 3312-3 FULL STRAIN FIELD MEASUREMENT OF BRAIDED COMPOSITE STRUCTURES Garrett Melenka University compositesBraided of continuous consist fibers embedded in a matrix. Full-field measurement strain approaches Three DigitalDimensional 3D Correlation- Image DIC and Digital Volume Correlation-DVC asseswill braided composite structures. , , Defence , Nanjing

3311 Defence Meeting room 215 room Meeting 3311-1 INTEGRATED CERAMIC/ HYBRID S2-GLASS FIBRE REINFORCED COMPOSITE ARMOUR Ali Daliri Science and Group Technology evaluated study This ballistic the performance of a range of polymer ceramic/S2- systems; armour Glass polymercomparing face strike ceramic and embedding the within powder ceramic FRP a phenolic matrix composite. 3311-2 PROTECTION PROPERTIES OF BI-CORRUGATED SANDWICH STRUCTURES UNDER HYPER- VELOCITY IMPACT: NUMERICAL SIMULATION Guo Rui University of Science and Technology 3311-3 3311-3 OBSERVING THROUGH- THICKNESS TIMELINE DAMAGE IN THICK-SECTION MONOLITHIC COMPOSITES UNDER IMPACT LOAD Perez Vidal Ignacio University ofTechnical Denmark , , National , National , University 3310 Design and integration Meeting room 214 room Meeting 3310-1 MULTIFUNCTIONAL COMPOSITES FOR SENSING, ACTUATION, COMPUTATION STRUCTURALAND FORCE AIR POWER: PERSPECTIVE Dan Inman of Michigan 3310-2 CURRENT AND FUTURE TRENDS IN MULTIFUNCTIONAL COMPOSITES A RESEARCH: SCIENCE NATIONAL FOUNDATION PERSPECTIVE Siddiq Qidwai Science Foundation 3310-3 3310-3 DISTRIBUTED SENSING, AND ACTUATION, IN SOFTPOWER COMPOSITE MATERIALS Robert Shepherd Cornell University , ,

3309 and damage Fracture Meeting room 213 room Meeting 3309-1 DAMAGE CHARACTERISATION OF COMPOSITE COMPONENTS FULL- USING IMAGING FIELD TECHNIQUES Irene Jimenez Fortunato, University of Southampton Stress Thermoelastic Analysis (TSA) and Digital Image (DIC) Correlation full-field imaging techniques applied are simultaneously on a complex composite subjected substructure cyclicto loading to a damage provide parameter. 3309-2 EXPERIMENTAL OFSTUDY LIGHTNING DIRECT EFFECTS UNDERON CFRP ATMOSPHERIC PRESSURE AIR REDUCED AND PRESSURE AIR KamiyamaShintaro University Tokyo of and Agriculture Technology examined study This damage strike lightning ofbehaviours CFRP under atmospheric air andpressure reduced pressure the evaluate air to effect atmospheric of on environment damage lightning behaviour. 3309-3 3309-3 OFTHE ROLE HOMOGENEOUS AND HETEROGENEOUS TOUGHENING IN MECHANISMS DGEBA FRACTURE Leslie Lamberson Drexel University presents study This dynamic fracture investigations innate exploring oftoughening DGEBA resins (epoxy-based) heterogeneousvia and homogeneous additives for inimprovement high performance composite systems. , , , College

3308 Textile-based composites Meeting room 212 room Meeting 3308-1 3308-1 OF THESTUDY EFFECT OF IN- PLANE BRAID ON DISTORTIONS THE MECHANICAL PROPERTIES OF BRAIDED COMPOSITES STOCHASTIC USING AND TOOLS FINITE ELEMENT MODELLING Gautam Mayank University of Manchester typesThree of braided composites each in-plane different with distortions, a with angle of mean braid angle have 45° braid been produced, the to effect the study of in- distortionsplane on the (in behaviour tensile of braid axial direction) composites. 3308-2 OF INFLUENCE RESIN ON INTRAPLY SHEAR BEHAVIOR FABRIC IN PREPREG FORMABILITY Khan Muhammad WMG, The University of Warwick 3308-3 3308-3 INFLUENCES OF PROJECTILE MATERIALS ON IMPACT OF 2D RESISTANCE TRIAXIAL BRAIDED COMPOSITES Liu Lulu of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics paper, current the In typesthree of projectile, including cylinder projectile,gelatin CFRP blade-like projectile and titanium alloy projectile, were employed conduct to impactballistic tests on braided 2D triaxial the composites figure to out influences the of on projectile materials pattern damage the absorptionand energy behavior. , Fac ,

3307 modellingMultiscale Meeting room 211 room Meeting 3307-2 A MESHFREE- MODELLING BASED APPROACH FOR PREDICTING THE EFFECTIVE PROPERTIES OF COMPOSITE AP-PLY LAMINATES Chen Yanhong University of Oxford presentation The a with deals micromechanical homogenisation of effectivethe elastic properties of AP-PLY composites using baseda meshfree modelling approach. 3307-1 MICROMECHANICAL OF MODELLING PACKED DENSELY FOAM SYNTACTIC COMPOSITES Declan Carolan Technology , , UC San , The

3306 Composite structures Meeting room 210 room Meeting 3306-2 3306-2 EFFECT OF SPREAD FIBER CARBON ON THE TOW MECHANICAL PROPERTIES OF THE CF/NANO-PET COMPOSITES Hwang Yeon-Taek UniversityHanyang on sprayed CNT was andCF tow spread mechanical properties of CF/Nano-PET composites was enhanced. 3306-1 3306-1 EXPERIMENT AND OF IN- PREDICTION PLANE LOCALISED CRUSHING OFRESPONSES COMPOSITE CF/EP SANDWICH UNDER PANELS A SEMICIRCULAR INDENTER Chen Yuan University of Sydney investigates study This localised in-plane the responses crushing of carbon fibre reinforced epoxy composite(CF/EP) panels sandwich under a semi-circular subjectedindenter to and both quasi-static dynamic loadings. 3306-3 3306-3 NDE GUIDED WAVE RESIDUAL AND OF STRENGTH PANELS COMPOSITE WITH STIFFENER DAMAGE IMPACT KimHyonny Diego Stringer-stiffened composite panels assessed by ultrasonic show guided waves to correlation strong as features damage byimaged NDE other CT, techniques (x-Ray as well as ultrasonic), residual strength. to , State , School of , University

Peter Middendorf, University of Stuttgart, Germany 3305 Additive manufacturing Meeting room 209 room Meeting 3305-2 CHARACTERISATION OF FUSION QUALITY BETWEEN FILAMENTS FDM USING BY ESSENTIAL WORK OF FRACTURE HeQinghao Aerospace, Mechanical and Mechatronic Engineering andProposed a investigated methodpractical to fusion characterize quality of 3D printed polymer composites, conduct to DENTi.e. thetests determine to specific essential work of single of fracture film. layer 3305-1 AT FIBRE LENGTH DIFFERENT STAGES OF ADDITIVELY MANUFACTURED FIBRESHORT REINFORCED COMPOSITES Lizhe He of Ningbo Nottingham China 3305-3 3305-3 ON 3DSTUDY PRINTING AND PROPERTIES OF COMPOSITE CARRIERS CATALYST WITH BIOMIMETIC POROUS STRUCTURE Cunbao Huo Key Laboratory of SystemsManufacturing Engineering, Xi’an UniversityJiaotong a paper, this In biomimetic porous catalystceramic prepared was carrier bedby powder fusion technology. , , , Institut , Institut

3304 Liquid composites moulding Meeting room 208 room Meeting 3304-2 KEY ASPECTS IN MANUFACTURING MULTI-SCALE COMPOSITES USING RFIOOA Robitaille Francois University of Ottawa 3304-1 SCALE MULTI OF SIMULATION IN DRYFLOW PLACEMENTFIBER PREFORMS Oliver Rimmel Verbundwerkstoffe für GmbH work present The application with deals of a numerical random solver to fibre arrangements micro determine to permeability transverse fibre orientation, the to in meso- use for later scaledand macro models. 3304-3 BASEDMODEL OF PROCESSING RTM PARTS HYBRID Ralf Schledjewski Montanuniversität Leoben A one-shot-hybrid RTM process for hybrid multi material parts to basis the is a strategy demonstrate data generate to how for models for used an inline process optimization. - , Toyama , Toyama , Howon , Hong Kong

3303 Self-healing Meeting room 206 room Meeting University study, this In aerodynamic and design of the structural composite propeller for a regional blade is aircraft turboprop performed. self- The healing concept for developed propeller studied. was Prefectural UniversityPrefectural Three-dimensional finite element analysis performedwas using a representative volume element model predict to progressiondamage of spread behavior carbon fiber/epoxy containing laminates microcapsules. 3303-2 OFDESIGN COMPOSITE PROPELLER BLADE OF TURBOPROP AIRCRAFT ON CONSIDERING HEALINGSELF Hyunbum Park 3303-1 DAMAGE PROGRESSION OF SELF- ANALYSIS HEALING POLYMER COMPOSITES CONTAINING MICROCAPSULES Nassho Yasuka University of Science and Technology ENCAPSULATION: ENCAPSULATION: TO A DIRECT PATH - MULTIFUNC NOVEL MATERIALS TIONAL Jinglei Yang 3303-3 3303-3 MICRO METALLIC , , Institute , Institute

3302 Biocomposites 3302-2 MECHANICAL PROPERTY CHARACTERIZATION AND TRANS-SCALE FORMODELING NACRE SongJingru of Mechanics Chinese Academy of Sciences hierarchical The of nacre structures observedare and a model is trans-scale describe to used its mechanical behavior by nanoindentation the test and fracture toughness test. 3302-1 INVESTIGATION FIREOF NOVEL RETARDANT POLYFURFURYL (PFA) ALCOHOL BIO-COMPOSITE MATERIAL Sharif, UniversityTahir of Derby Polyfurfuryl alcohol bioresin is (PFA) a biological and sourced sustainably polymerthermosetting excellent natural with fire resistance. This the investigates study mechanical, thermal and fire retardant properties of this composite as material, prepreg, in autoclave and oven cure processes. 3302-3 3302-3 POTENTIAL OF APPLYING PULTRUSION FOR THE MANUFACTURING OF BIO-BASED COMPOSITE PROFILES USING FIBRE CELLULOSE ALIPHATIC AND POLYURETHANE Sebastian Strauss IGCVFraunhofer Meeting room 205 room Meeting , NETZSCH Germany Analyzing and Testing, , , , Advanced Cluster Fibre , TU Delft , NETZSCH Australia Analyzing and Testing, , Victorian Chief, Victorian Engineer , RMIT , , A*STAR , University of

Lunch Exhibition hall 3301-2 3301-2 FIELD LOW MICROWAVE ABSORPTION MAGNETO AND IN RESISTANCE NANO PANI-FE FIBRE COMPOSITES Srinivasu Vijaya Vallabhapurapu University of South Africa Low field microwave absorption in various (LFMA) systems, namely, Superconductors, and magnetic materials polymer composites totally different.is here reportwe LFMA on the particlein Fe nano (Nps) embedded PANI fibers.nano Jennifer Conley Meeting 212 room Chiara Bisagni Chiara Stefanie Feih Andrew Gillen MANUFACTURING PLENARY LECTURE: AUTOMATED COMPOSITES FROM TO 4.0: DESIGN 3301-1 PERFORMANCE OF GRAPHENE/ DIAPHRAGM EPOXY HEADPHONES Hsien-Kuang Liu Collette Burke MichelleGee Manufacturing of Composite Challenges and Future NETZSCH - Current roundtables Industry only event"*invitation Alexander Chaloupka Dept. of Mechanical and Computer Aided Engineering, Feng Chia University oxide paperGraphene headphone(GOP) possesses highest SPL 98 dB firstvalue at frequencyresonant 430 Hz, GOP the while composite headphone SPL smoother has curve in higher frequency range. ICCM22 Women in Composites Leadership Forum Leadership Forum in Composites ICCM22 Women Plenary 2 rooms concurrent to Move 3301 Nano-composites 3301-3 3301-3 DEVELOPMENT OF DIELECTRIC ELASTOMER NANOCOMPOSITES AS STRETCHABLE ACTUATING MATERIALS Lizhi Sun California, Irvine Dielectric elastomers a new(DEs) type are of smart materials promising showing functionalities as harvestingenergy as well as materials for materials actuating applications potential artificial as such muscles, implanted medical devices, robotics, and micro- electro-mechanical theirsystems due to high electromechanical efficiency, stability, lightweight, cost, low and easy processing. Plenary 2 1440-1500 1240-1345 1250-1340 1300-1345 1345-1430 1430-1440 1440-1600 WEDNESDAY 14 AUGUST WEDNESDAY Time 1500-1520 1520-1540

72 SCIENTIFIC PROGRAM SCIENTIFIC PROGRAM SCIENTIFIC 75 , University of Meeting room 219 room Meeting 3315-4 3315-4 COST-EFFECTIVE OF SYNTHESIS COPPER/DIAMOND WITHCOMPOSITE ACCEPTABLE THERMOPHYSICAL PROPERTIES Fei Yang Waikato and feasible It is cost-effectiveuseto induction plus heating produce to forging copper/diamond composites with acceptable thermal conductivity, meeting critical application ofrequirements future electronic high-power device. , Meeting room 218 room Meeting 3314-4 3314-4 BEHAVIOR FATIGUE OF UN-NOTCHED OPEN-HOLE AND QUASI-ISOTROPIC PSEUDO-DUCTILE CARBON/ THIN-PLY GLASS HYBRID LAMINATES Meisam Jalalvand University of Strathclyde , Meeting room 217 room Meeting 3313-4 EXPERIMENTAL ON EXAMINATION THE HIGH-SPEED IMPACT BALLISTIC BEHAVIOR FAILURE OF LAMINATED TEXTILEAND COMPOSITE PANELS Zhang Chao Northwestern Polytechnical University high-speedThe impact ofbehavior composite laminates, compositeswoven braided and triaxially composites were experimentallystudied and systematically thecompared, with ofintroduction digital correlation, image CT C-scan and X-ray characterizations. , Meeting room 216 room Meeting 3312-4 EXPERIMENTAL DETERMINATION OF STATISTICAL CORRELATION BETWEEN FRP ELASTIC PROPERTIES Shufeng Zhang UniversityNational of Defense Technology A methodology proposedis to experimental of determination correlation statistical between FRP elastic properties by a ofcombination digital and correlation image virtual field methods. Meeting room 215 room Meeting , CSIRO Meeting room 214 room Meeting 3310-4 3310-4 MECHANICAL PROPERTIES OF MULTIFUNCTIONAL SANDWICH COMPOSITES WITH EMBEDDED LITHIUM-ION POLYMER BATTERIES Adam Best , Meeting room 213 room Meeting 3309-4 3309-4 IN SITU MICRO- OF CT IMAGING COMPRESSION CARBON LOADED FIBRE REINFORCED POLYMER SPECIMENS AND WITH VOIDS WRINKLES Abhiram Ramesh University of Auckland CFRP specimens extracted curved from containingregions and wrinkles voids a using tested were novel compression fixture, for in allowing µ-CT scans X-ray situ loadunder several the determine to steps type and evolution of damage. Meeting room 212 room Meeting Meeting room 211 room Meeting

, Denmark Meeting room 210 room Meeting 3306-4 3306-4 EFFECTOF MATRIX CRACKS ON THE STIFFNESS DEGRADATION OF LAMINATED BEAMS COMPOSITE Oscar Gerardo Castro Ardila , Meeting room 209 room Meeting 3305-4 3305-4 HIGHDEVELOPING TEMPERATURE – HIGH PERFORMANCE GF/PEKK THERMOPLASTIC PREPREGS Zhongwei Guan University of Liverpool been has rig A test developed produce to fibre/PEKKglass prepregs. Through resin bath the can be nanomaterials impregnate added to fibre. fibrethe Also can becontent controlled. , Meeting room 208 room Meeting 3304-4 PROPERTIES OF POLYAMIDE-6 COMPOSITES USING THERMOPLASTIC RESIN TRANSFER MOULDING James Murray University of Edinburgh Thermoplastic composite laminates ~53% fibrewith volume fraction, volume~1% voids and excellentfraction mechanical properties produced a using were bespoke TP- low-cost RTM system 5 within minutes onlyusing a 4 bar injection pressure. Meeting room 206 room Meeting ,

3302-4 3302-4 BIO- TOUGH CERAMIC INSPIRED COMPOSITES FOR HIGH AND AMBIENT TEMPERATURE APPLICATIONS Behnam Ashrafi Research National Council Canada work This a how demonstrates bio-inspired approach based on architectured designs and lamination could address the ofbrittlest ceramic structures. Meeting room 205 room Meeting - -

, University of TION OF MXENE: EFFECTIVE FLAME ANDRETARDANT REINFORCEMENT FOR THERMOPLAS TIC POLYURETHANE ELASTOMER Yang Wei New South Wales 3301-4 3301-4 AND EXFOLIATION FUNCTIONALIZA Plenary 2 Exhibition hall MeetingICCM General Annual Coffee break 1540-1600 WEDNESDAY 14 AUGUST WEDNESDAY Time 1630-1830 1600-1630

74 SCIENTIFIC PROGRAM SCIENTIFIC PROGRAM SCIENTIFIC 77 - - , Ulster Ulster , ,

4115 Mechanics of composites Meeting room 219 room Meeting 4115-1 4115-1 ON THE EXPERIMENTAL OF THE VALIDATION WAVE PROPAGATION FORMODELLING TWO-DIMENSIONAL TEXTILEPERIODIC COMPOSITES ThierryVictor University of Nottingham An experimental of a validation methodnumerical vibroacoustic allowing and ultrasonic propagation wave analysis in complex compositeswoven is proposed paper. in this 4115-2 ABSORP ENERGY TION MECHANISMS IN LAYER-TO-LAYER COM 3D WOVEN POSITES Geoffrey Neale University research This the investigates suitability of a novel composite3D woven an axial as architecture absorbing energy crush system for automotive applications. - , Doshisha , Ifremer

41145 Fatigue Meeting room 218 room Meeting 4114-1 4114-1 LONG-TERM AGEING SEA-WATER EFFECT ON FATIGUE GROWTHCRACK PROPERTIES OF CFRP Antoine Guen- Le Geffroy 4114-2 EFFECTS OF GLASSSUBMICRON ADDITION ONFIBER PROP MECHANICAL ERTY OF SHORT FIBER CARBON REINFORCED VINYL ESTER RESIN Nhan Thi Thanh Nguyen University improvement The of Mode I fracture toughness and fatigue life of resin and short carbon fiber composite reinforced vinyl ester matrix - , The , Imdea

4113 compositesHybrid Meeting room 217 room Meeting 4113-1 VEIL FIBER CNT INTERLEAVED FIBER/ CARBON EXPOXY LAMINATE COMPOSITE Ou Yunfu Materials Mode I interlaminar toughness fracture of fabric/ woven was epoxy laminate as much improved as interleaving 60% when fluffyas-received CNT veils, degradation while observedwas in the unidirectional system. 4113-2 OF OPTIMIZATION FIBRE RE- CARBON INFORCED POLYMER COMPOS (CFRP) ITES WITH A THIN - POLYU EMBEDDED RETHANE FILM Pappa Evanthia University of Edinburgh - - , , University

4112 methods Testing Meeting room 216 room Meeting 4112-1 ASSESSMENT OF THE APPLICABILITY OF COMPOSITE TEST MECHANICAL FOR STANDARDS 3D WO WITH USE COMPOSITESVEN PooleMatthew Physical National Laboratory 4112-2 DIGITAL COMBINING CORRE- IMAGE PASSIVE LATION, THERMOGRAPHY ACOUSTIC AND INVES TO EMISSION DAMAGE TIGATE AND INITIATION OF PROPAGATION OUT-OF-PLANE WAVINESS FIBER Michael Thor of Applied Sciences Austria Upper - , Volvo , Volvo , Bmw

4111 Automotive Meeting room 215 room Meeting Car Corporation work, this In a for efficientframework analysis of composite presented. is structures is framework The into implemented commercial software and takesready for use modes failure relevant account.into 4111-1 A NEW CONCEPT FOR THE OF AN INTEGRATION INDUCTIVE UNIT CHARGING IN ELECTRIC VEHICLES FIBER USING REINFORCED PLASTIC Mayr Tobias Group a new study this In concept for the of an integration unitinductive charging underbody the into of an electric vehicle by fiberusing reinforced described. is plastic 4111-2 FRAMEWORK FOR DURABILITY ANALY OF COMPOSITE SIS STRUCTURES IN THE AUTOMOTIVE INDUSTRY Henrik Molker - , , Airborne Oil

4110 subseaOffshoreand Meeting room 214 room Meeting 4110-1 TERM LONG FATIGUE – DEGRADATION SUPERPOSITION OF DRY WET AND PROPERTIES Andreas Echtermeyer Ntnu 4110-2 A GENERIC FRAMEWORK FOR THERMO-MECHAN OF CREEP ICAL THERMOPLASTIC MATERIALS Sandeep Kumar Namdeo & Gas methodologyA generic for thermo-mechanical developed, is creep provideswhich a and time-systematic efficient for approach model material the in an calibration unequivocal manner. - , - ,

4109 and damage Fracture Meeting room 213 room Meeting 4109-1 VOLUME DIGITAL FOR CORRELATION ANALYSIS DAMAGE FIBER IN CARBON COMPOSITES Mahoor Mehdikhani KU Leuven of digital Potential volume correlation of for investigation in in-situ damage imagessynchrotron of carbon fiber composites explored. is 4109-2 AXIAL COMPRES PROPERTIESSIVE OF RANDOMLY DISTRIBUTED DISCONTINUOUS LONG-CARBON REINFORCEDFIBER THEMOPLASTIC MA TRIX COMPOSITE Kimiyoshi Naito for Institute National ScienceMaterials (NIMS) , Deakin , National , National

4108 dimensional Three composites Meeting room 212 room Meeting 4108-1 SYNERGISTIC DELAMINATION OF TOUGHENING COMPOSITES USING NANO- MICRO- AND REINFORCE- SCALE MENTS Anil Ravindran University 4108-2 SUPPRESSING DELAMINATION IN COMPOSITE INTERSECTIONS WITH TUFTING AND Z-PINNING ScottMatt Composites Centre - , , , Deakin University

4107 modellingMultiscale Meeting room 211 room Meeting AGE PROPAGATION PROPAGATION AGE REGARDING WOVEN LAMINATES CFRP ON HOMOG- BASED THEORY ENIZATION Nonoyama Kosuke 4107-2 NUMERICAL OF DAM ANALYSIS Department of Aerospace Engineering, UniversityNagoya propagation Damage of CFRP woven simulated is laminates based onnumerically homogenizationthe theory and the damage continuum mechanics with of the consideration elasto-viscoplasticity of epoxy resin. 4107-1 FIBERSHORT COMPOSITES: COMPUTATIONAL HOMOGENIZATION VS ORENTATION AVERAGING Seyed Mohsen Valashani Mirkhalaf University of Gothenburg/ chalmers University of Technology , UIUC Tiffany Walsh Tiffany (retired) (Meeting, Boeing 211) room (retired) , School of Nancy SottosNancy , Imperial

4106 Composite structures Meeting room 210 room Meeting 4106-2 4106-2 STRENGTH TENSILE OFPREDICTION NOTCHED FROM A LAMINATES TENSION COMPACT TEST Qiang Ma Aerospace Engineering & Applied Mechanics, University Tongji 4106-1 THE PERFORMANCE OF THERMOPLASTIC THERMOSETAND COMPOSITES TO SUBJECTED AND LOW-VELOCITY HIGH-VELOCITY LOADING IMPACT LiuJun College London performanceThe of (AS4/ thermoplastic PEEK) and thermoset (T700/epoxy) laminates under drop-weight gun impactsand gas Three- evaluated. is Digitaldimensional Correlation Image (DIC) and ultrasonic C-scan techniques are employed. , Universityof Rhode Island (Plenary 2) John Hart-Smith - - , Tsinghua , Tsinghua POLYMERIZATION Arun Shukla , School

4105 Additive manufacturing Meeting room 209 room Meeting 4105-2 NANO CARBON - TUBE/POLYCAPROL ACTONE COMPOSITE FILAMENTS USED FOR 3D PRINTING Liangliang Li University Carbon nanotube/ polycaprolactone composite filaments filler various with contents were synthesized. The composite filaments electricallywere conductive and could be for 3D printing. used 4105-1 VELOCITYLOW OF ADDI IMPACT - TIVE MANUFAC TURING TI-6AL-4V PANELS SANDWICH WITH LATTICE Li Peiyao of Aeronautics, Northwestern Polytechnical University, Xi’an, China objective main The to is research of this velocity low the study impact of response with panels sandwich BCC and FCC lattice by SLM. manufactured - - -

, Ecole , Beihang

, Cornell University , UCLA , Boeing, USA , US Air Force Lab Research 4104 Liquid composites moulding and ofmachining composites Meeting room 208 room Meeting 4104-2 STUDY NUMERICAL OF MULTI-DIMEN MUL - SIONAL TI-PHASE FLOW IN THE VACUUM RESIN ASSISTED INFUSION Zhou Yubo University 4104-1 OF CONSIDERATION SCALE THE DUAL INOF PORE SIZE – VALIDA WICKING TION ON CARBON REINFORCEMENTS APPLICATION AND THE SWELLING TO REIN OF BIO-BASED FORCEMENTS Vo Hong-Nhan Des Mines capillary the During wicking in Liquid Composite Moulding, a new model is proposed, taking into account effect the of two at fibre swelling scales: elementary fibres and yarns. - Ximin He - Jerry Young , Institute , Institute Robert Shepherd , Hong Kong Michael F. Durstock Michael F.

4103 Nano-composites Meeting room 206 room Meeting CATION Lu Wenjiang 4103-2 THE ENHANCED INTERLAMINAR FRICTIONAL BEHAV IOR OF WRINKLED FORGRAPHENE APPLI DAMPING for Composites Science Innovation (incsi), School of ScienceMaterials and Engineering, Zhejiang University 4103-1 BIOINSPIRED GRAPHENE/LIQUID CRYSTALLINE POLYMER NANOCOMPOSITE FOR COATINGS TRIBOLOGICAL APPLICATIONS Xi Shen University of Science and Technology Novel graphene/ compositesLCP with heterogeneous layered show structures extremely high wear and areresistance suitable therefore tribological for many applications. , - - - - - , , Texas , Texas , HP Labs , Georgia , University (Meeting 213) of room Southhampton NSF-AFOSR Joint NSF-AFOSR on Workshop Mechanics-Based Design of Intelligent Material Systemsby Additive Multimaterial 2 PART Manufacturing Meeting room 205 room Meeting This session starts at hours1100 JET FUSION MULTI AND TECHNOLOGY VOX ITS ADVANCED POTENTIALSEL Lihua Zhao ADDITIVE- MANU AND FACTURING ARCHITECTED NEW MATERIALS: METHODS AND MATERIALS Spadaccini Christopher LivermoreLawrence Laboratory National - MANU ADDITIVELY SOLID/ FACTURED COM METAL LIQUID ACTUATORS: POSITE AND PROMISES CHALLENGES HartlDarren A&M University MAN AND DESIGN OF UFACTURING COMPLEX-GEOME- TRY COMPOSITES FUSED COMBINING FILAMENT FABRI (FFF) AND CATION FIBER AUTOMATED PLACEMENT (AFP) Felix Raspall UniversitySingapore of and Design Technology 3D PRINTING OF BIO-COMPATIBLE MEM SHAPE TOUGH ORY HYDROGEL Hu Yuhang of Technology Institute by Sponsored , Fill, Austria , , Ford, USA , Furnace Engineering,, Furnace Australia , Advanced Australia Cluster, Fibre , RMIT RMIT , DYNAMIC INSTABILITY OF ANISOTROPIC CYLINDERS IN CONFINING ENVIRONMENTS CYLINDERS OF ANISOTROPIC INSTABILITY DYNAMIC COMPOSITES MATERIALS OF – ONLY THING AS MATERIAL A COMPOSITE NO SUCH THERE IS TECHNIQUES FOR IMAGING OF LARGE ASSESSING THE PERFORMANCE COMPOSITES STRUCTURESINTEGRATING Janice Barton COMPOSITES IN POLYMER REVEALING FIBRE FUNCTIONALISATION THE MOLECULAR-SCALE OF CARBON ROLE (Meeting 219) room , Boeing, USA

, High Volume Manufacturing Catapult Centre, Manufacturing , High Volume UK , Quickstep, Australia

Day 4 Welcome & Announcements 4 Welcome Day Plenary 2 4101-2 4101-2 EFFECT OF ON SEA WATER COMPRESSIVE PROPERTIES OF FIBER CARBON ESTER VINYL COMPOSITES PenumaduDayakar University of Tennessee 4101-1 OF DEGRADATION THE EXPLOSIVE BLAST RESISTANCE OF COMPOSITES SEAWATER DUE TO ABSORPTION Adrian Mouritz David Doral David SimpsonRichard Jennifer Conley Sayata Ghose Plenary 2 PRINTING 3D APPLICABILITY IN NEXT-GENERATION – THEIR AND INVERSION VIA PHASE FILMS COMPOSITE OF POROUS TUNABLE MECHANICS FLEXIBLE STORAGE ENERGY ELECTRONICS AND KEYNOTE 1: KEYNOTE 2: KEYNOTE 3: KEYNOTE 4: University of the Degradation Explosive Blast Resistance of Composites to Due Absorption Seawater Mike Hinton Industry Forum on the Future of Composites Future on the Forum Industry Wilhelm Rupertsberger Blanchard Patrick 1 PART Manufacturing Additive by Multimaterial Systems Material of Design Intelligent on Mechanics-Based Workshop Joint NSF-AFOSR L FRONTA COMPOSITES AND USING OF THERMOSETTINGADDITIVE MANUFACTURING POLYMERS COMPOSITES COMPLIANCE VARIABLE SELF-SENSING THROUGH 4-D PRINTING BIO-MORPHOGENESIS UNVEILING Exhibition hall 4101 ONR Solid Mechanics Symposium TRENDS IN AEROSPACE COMPOSITES PLENARY LECTURE: TRENDS IN AEROSPACE Coffee break rooms concurrent to Move Plenary 2 1100-1130 0800-0805 0805-0850 0850-1030 0900-1030 1100-1320 1030-1100 1130-1140 1140-1200 THURSDAY 15 AUGUST THURSDAY Time 1200-1220

76 SCIENTIFIC PROGRAM SCIENTIFIC PROGRAM SCIENTIFIC 79 , , , Northwestern Meeting room 219 room Meeting 4115-4 4115-4 EXPERIMENTAL NUMERICAL AND INVESTIGATION ON DAMAGE RESISTANCE OF 3D BRAIDED COMPOSITES Di Zhang Polytechnical University 4115-5 EFFECT OF THROUGH- THICKNESS PENETRATIVE REINFORCEMENTS ON THE MECHANICAL OF BEHAVIORS COMPOSITE-TO- BONDED METAL JOINTS LiuLongquan Tong Jiao Shanghai University A through-thickness penetrative reinforcement technology of theimproving tolerance damage and mechanical performance of the metal-composite joints discussed. was 4115-3 4115-3 GROWTHDISBOND ASSESSMENT FOR PATCH BONDED OF PRIMARY REPAIR AIRFRAME- STRUC TURES Tanulia Veldyanto University of New South Wales , , TU , Meeting room 218 room Meeting 4114-4 4114-4 DAMAGE FATIGUE OF MECHANISMS FROM HIGH CF-PPS VERY HIGH TO CYCLES Dominic Weibel Kaiserslautern - Institute of Science Materials and Engineering VHCF properties of appliedaerospace CF- investigated are PPS ultrasonic using frequencies 10 while HCF testsHz serve as benchmark. Similar mechanisms damage can be detected. 4114-5 RESEARCH ON THE STIFFNESS OF PIPES COMPOSITE UNDER STATIC AND FATIGUE FATIGUE CYCLIC Zhen Yuqing UniversityWuhan of Technology fatigue on static Basis test and cyclic fatigue test of different type deflection,and different equation ofthe of ring the variation stiffnessis obtained. 4114-3 4114-3 CRACK FATIGUE PROPAGATION IN COMPOSITE A BY LAMINATES APPROACH NOVEL ON THE S-NBASED DIAGRAMS Antonio Raimondo Delft University of Technology , Deakin , Guangzhou Meeting room 217 room Meeting 4113-3 4113-3 INTERFACE HYBRID FIBER CARBON COMPOSITES – PERFOR- IMPROVED MANCE, REDUCED WEIGHT. Filip Stojcevski University designs inspired Nature in been recreated have composite laminates modificationsusing fiberto interface Resultsbonding. show improvements vast performanceto specifically when multiple interface types employed are simultaneously. 4113-4 FAILURE OF MECHANISM TITANIUM-BASED CARBON-FIBRE/ LAMINATES EPOXY UNDER TENSION Jing Sun University of behaviour Tensile carbon- titanium-based laminates fibre/epoxy (TI-CF FMLs) were The investigated. as mechanism failure specific the as well of absorption energy FMLs TI-CF the were analyzed and evaluated respectively. , , , National , National Meeting room 216 room Meeting 4112-3 APPLICABILITY FOR 14125 OF ISO STEEL-COMPOSITE STRUCTURES Houssin Wehbe TU Braunschweig, und Füge- für Institut Schweißtechnik of lack The testing standardised methods hybrids for the motivates of the investigation bending test.four-point challengesParticular addressed,are the e.g. asymmetric structure of anisotropy and the materials. hybrid 4112-4 NOVEL MEASUREMENT FOR SYSTEM DETERMINING TEXTILE BEHAVIOR DURING OUT- OF-PLANE IMPREGNATION Björn Willenbacher für Institut Verbundwerkstoffe GmbH An out-of-plane permeability system is measurement initially that presented enables monitoring of inhomogeneous hydrodynamic compaction of textiles impregnation. during the data this From distribution non-linear of fiber volume content along sample thickness can be derived. 4112-5 PRACTICAL APPLICATION OF TEXTILE PERMEABILITY MEASUREMENT Ana Yong Physical Laboratory Permeability is measurement beginning advance to research the from industry toward stage Asapplication. this made, is transition challengespractical in the from transition the environment research meetingto needs the of be industry must addressed. , The , , Khalifa Meeting room 215 room Meeting 4111-3 AND STRENGTH - CHARAC FAILURE OF ATERISTICS RANDOM CARBON SMC-R FIBER UNDERCOMPOSITE STRESSESBIAXIAL Pankaj Mallick University of Michigan- dearborn biaxial Quasi-static stress experiments on a carbon fiber that SMC-R show stress at tensile the decreases failure shear increasing with failure stress and the the envelope follows closely. Equation Hill 4111-4 MULTI-PHYSICS OF SIMULATION SOFT MAGNETIC COMPOSITES FOR INDUCTIVE POWER SYSTEMS TRANSFER Maedeh Amirpour University of Auckland 4111-5 TUNABLE SELF-SENSING PERFORMANCE OF ADDITIVE MANUFACTURING ENABLED PLA NANOCOMPOSITES FOR BIOMEDICAL APPLICATIONS Jabir Ubaid University - , , Meeting room 214 room Meeting 4110-3 4110-3 THEPREDICTING WETTED VIBRATION OF FLEX BEHAVIOR COMPOSITE IBLE HYDROFOILS Andrew Phillips Defence Science and Group Technology objectiveThe of this develop to is awork modellingnumerical can that approach predict wetted the of behavior vibration flexible composite hydrofoils. 4110-4 GRAPHENE/ POLYMER COMPOSITES FOR BARRIER IMPROVED PERFORMANCE Raine Thomas University of Manchester observe anWe of magnitude order reduction in carbon dioxide permeation of and shutdown sulfidehydrogen through permeation polyamide/graphene Epoxy/CF/laminates. compositesgraphene a 60% reductionshow in carbon dioxide permeation. , , Tokyo , Tokyo Meeting room 213 room Meeting 4109-3 PREDICTING SHEARNON-LINEAR DEFORMATION IN 3D FAILURE AND FIBRE-REINFORCED COMPOSITES Carolyn Oddy Chalmers University of Technology following The proposeswork a framework general for modelling the mechanical response of 3D fibre-reinforced composites. 4109-4 IN-SITU OBSERVATION OF STRAIN FIELD IN ADHESIVELY CFRPBONDED JOINTS UNDER MODE IIMODE I AND LOADING Sota Oshima University of Agriculture and Technology paperThis quantitatively evaluates microscopic failure process in adhesively bonded CFRP joints by digital the image method. The correlation comparedresults were of numerical that with analyses. - , , , Ulster Ulster , Meeting room 212 room Meeting 4108-3 OF TEXINFLUENCE ARCHITECTURETILE ON MECHANICAL PROPERTIES OF 3D CARBON WOVEN COMPOSITES Dahale Monali University 4108-4 NOVEL MANUFACTURING TECHNIQUES FOR OPTIMIZED 3D MULTIAXIAL ORTHOGONAL PREFORM Vivek Koncherry The University of Manchester presents study the This manufacturing robotic process development and mechanical properties of optimised flat,3D multiaxial cylindrical, near net preform and ultra-thick orthogonalwith binders. 4108-5 MESO-SCALE AND OPTIMISATION MANUFACTURING OF CONTINUOUS FIBRE 3D REINFORCEMENTS Mikhail Matveev The University of Nottingham , Beijing , , National , National Meeting room 211 room Meeting 4107-5 INCREASING THE THERMAL CONDUCTIVITY OF POLYMER NANOCOMPOSITES WITHFILLED CARBON NANOTUBES VIA MOLECULAR DYNAMICS SIMULATION Gao Yangyang University of Chemical Technology 4107-3 A DIRECT FE2 METHOD FOR CONCURRENT MULTILEVEL OFMODELING COMPOSITES IN A FINITESINGLE ELEMENT ANALYSIS Tan Vincent University of Singapore Direct FE2 allows analysisfor the of made structures heterogeneousfrom (e.g. materials composites) without need the for homogenized constitutive relations. outIt can be carried directly on commercial for non- FE software linear finite deformation problems, including plasticity and damage. 4107-4 OF FORMULATION REDUCED THE SIZE FORUNIT CELL TRIAXIALLY BRAIDED COMPOSITES Mingming Xu University of Nottingham Relative displacement boundary conditions beenhave for the formulated size reduced unit cell braided of triaxial composites. From implementation the in UnitCells©, it has full prediction ability and cut CPU the time dramatically.

, Inegi/ , Karlsruhe ,

Meeting room 210 room Meeting 4106-5 AN INVARIANT BASED TRANSVERSELY ISOTROPIC 4106-3 ASSESSING DELAMINATION GROWTH UNDER VARIABLE AMPLITUDE LOADS Molent Loris Defence Science and Technology growth Delamination in simple laminate specimens appears thus and systematic be predictable.should 4106-4 OF INVESTIGATION THE INFLUENCE OF MECHANICAL AND PRE-DAMAGE ON STRAIN RATE THE MECHANICAL PROPERTIES OF CFRP/METAL PROFILES HYBRID Muth Markus of Technology Institute a hand, at work the In out made of structure steel and carbon fibre reinforced plastics under is (CFRP) for itsinvestigation properties in quasi- and dynamicstatic properties. CONSTITUTIVE FORMODEL UNIDIRECTIONAL POLYMER COMPOSITES THE CONSIDERING VISCOUS MATRIX EFFECTS Fermin Otero cimne A constitutive law ply the levelat for unidirectional FRPs The presented. is model capable to is the predict accurately effectsviscous the and non-linearities in the response. material , Nottingham University,, Nottingham UK , University , Imperial , ETH Zurich , University of Colorado Boulder Meeting room 209 room Meeting 4105-3 INK A FACILE JETTING SYSTEM FOR ADDITIVE MANUFACTURING WITH ABRASIVE INK COMPOSITIONS 4D TOWARDS PRINTING Naguib Hani of Toronto of4D printing functional materials a novelusing binder jetting approach. prints approach The functionally graded composites, allowing 4D pattern-driven of activatableprinting materials. 4105-4 ADDITIVE MANUFACTURING OF BONE-INSPIRED STRUCTURAL- POWER COMPOSITES Ajit Panesar College London , Sanida National Laboratories , Sanida National , The Kurt Maute Kristina Shea , Miguel Aguilo Meeting room 208 room Meeting 4104-3 WEAR BEHAVIOR CUTTINGOF SOME IN TURNINGTOOLS - OF SILVER-IMPREG GRAPHITE NATED COMPOSITES Yan Chaoren Nanjing University of Aeronautics and Astronautics 4104-4 DAMAGE THERMAL OF EVALUATION CFRP PROCESSED WITH NANOSECOND UV LASER PULSES Tamaru Hiroharu University of Tokyo wavelength The dependence of thermal for CFRPdamage processing laser was byevaluated Raman and it spectroscopy, observedwas the that lessresin is damaged of a wavelength at 258nm. - , Meeting room 206 room Meeting 4103-3 4103-3 NANOENGINEERING OF FIBRE SURFACE FOR CARBON FIBRE-CARBON HIERARNANOTUBE - COMPOS CHICAL ITES Wojciech Szmyt Fachhochschule Nordwestschweiz, Für Institut Kunststofftechnik of coating An alumina carbon fiber provides harsh protection the in conditions of direct carbon nanotube enhanced We growth. alumina-fibre the adhesion by surface that treatment covalent promotes bonding. , - - - - - , , Texas , Texas , HP Labs , Georgia Meeting room 205 room Meeting CONTINUED MULTI JET FUSION MULTI AND TECHNOLOGY VOX ITSADVANCED POTENTIALSEL LihuaZhao ADDITIVE- MANU AND FACTURING ARCHITECTED NEW MATERIALS: METHODS AND MATERIALS Spadaccini Christopher LivermoreLawrence Laboratory National - MANU ADDITIVELY SOLID/ FACTURED COM METAL LIQUID ACTUATORS: POSITE AND PROMISES CHALLENGES HartlDarren A&M University MAN AND DESIGN OF UFACTURING COMPLEX-GEOME- TRY COMPOSITES FUSED COMBINING FILAMENT FABRI (FFF) AND CATION FIBER AUTOMATED PLACEMENT (AFP) Felix Raspall UniversitySingapore of and Design Technology 3D PRINTING OF BIO-COMPATIBLE MEM SHAPE TOUGH ORY HYDROGEL Hu Yuhang of Technology Institute by Sponsored , Bristol Composites (ACCIS), Bristol Institute , New - , University of Delaware , University of Southampton , Imperial , The University

Session continues 1515 at PERSPECTIVE DESIGN: A FORWARD-LOOKING OPTIMIZATION-BASED TOPOLOGY OPTIMIZATION FOR ACTIVE AND MULTI-FUNCTIONAL COMPOSITES MULTI-FUNCTIONAL FOR AND ACTIVE OPTIMIZATION TOPOLOGY Tsu-Wei Chou Tsu-Wei Ole Thomsen Quality and future of journal publications of journal Quality and future Michael Wisnom 3 PART Manufacturing Additive by Multimaterial Systems Material of Design Intelligent on Mechanics-Based Workshop Joint NSF-AFOSR MACHINES IN AUTONOMOUS 4D PRINTING: WITH DESIGNING EXPLORATIONS PLENARY LECTURE: OF TEXTILE PERFORMANCE AND MANUFACTURE DESIGN, COMPOSITES Andrew Long ITE SANDWICH ITE SANDWICH STRUCTURES WITH EPOXY TOUGHENED MATRICES George Irven 4101-5 RESPONSE IMPACT OF COMPOS College London 4101-4 DIC- A COMBINED EXPERIMENTAL PIV APPROACH FOR OFTHE STUDY RESPONSE IMPACT OF WATER-BACKED PANELS Maurizio Porfiri UniversityYork Tandon School of Engineering a demonstrate We combined approach fluid-structure study to associated interaction water-backed with impact, based on the of particleintegration velocimetryimage and digital image correlation. Plenary 2 sessions concurrent to Move 4101-3 UNDERSTANDING EFFECTOF ARCTIC TEMPERATURE ON POST-IMPACT FLEXURAL OF STRENGTH COMPOSITES Tan K.T. of Akron studies work This collapse flexural the modes of sandwich composites low due to and arctic temperature usingimpact damage analytical prediction and experimental validation. Plenary 2 Lunch Exhibition hall 1220-1240 1420-1505 1400-1515 1505-1515 THURSDAY 15 AUGUST THURSDAY Time 1300-1320 1320-1420 1330-1415 1240-1300

78 SCIENTIFIC PROGRAM SCIENTIFIC PROGRAM SCIENTIFIC 81 - , ACCIS - , Tel-aviv Tel-aviv , , University of

P4215 modellingMultiscale Meeting room 219 room Meeting P4215-2 FINITE STRAIN PARAMETRIC HFGMC OF THEPREDICTION MICROMECHANI OF BEHAVIOR CAL COMPOSITE Breiman Uri University Extension of the HFGMCparametric to finite- the incorporate micromechanics strain of composites is Macroscale presented. and microscale ofresponse UDs is successfully compared orthogonal the with HFGMC FEA. and the P4215-3 DEVELOPMENT OF MULTISCALE DAMAGE PROPAGATION METHOD ANALYSIS FOR WOVEN A USING LAMINATES HOMOGENIZATION THEORY Gai Kubo Tsukuba we study, this In develop an efficient analysismultiscale method for damage of woven propagation a using laminates homogenization theory. P4215-1 FORACCOUNTING SHEARED TEXTILE UNITCOMPOSITE PROPERTIES CELL FE SCALE IN MACRO SIMULATIONS Meng-yi Song University of Bristol Homogenised mechanical properties extractedare from textilesheared composite unit cell models for use in macro-scale component analysis. Macro-scale mechanical models the with run then are the from deformation included, stage forming for performance predictions. - , , Deakin , Chalmers

P4214 Fibers Meeting room 218 room Meeting P4214-2 TRANSVERSE MODULUS YOUNG’S MEASUREMENT FIBRE OF CARBON FORCE ATOMIC BY AND MICROSCOPE NANOINDENTATION Duan Shanghong Chalmers Universisty of Sweden Technology, P4214-3 SPECIMEN PREPARATION FOR TRANSVERSE MODULUS MEASUREMENT OF FIBRESCARBON FOCUSED USING ION BEAM LiuFang University of Technology P4214-1 HIGH LOW-COST, POL- STRENGTH YACRYLONITRILE PRECURSOR FIBRE Khan Huma University, Waurn Ponds, Australia system research This atically investigates of wet-spinning the of blends textile the and carbon fibre grade polymers. The PAN stability of different the dope solutions and their spinnability was checked by rheological measurements.

, Sabancı , Ningbo , Zhejiang P4213 Interfaces and interphases Meeting room 217 room Meeting P4213-1 TUNABLE MICROWAVE DIELECTRIC IN RESPONSE CARBON NANOCOMPOSITES VIA VERTICAL INTERPHASE Faxiang Qin University P4213-2 TAILORING INTERFACIAL INTERACTIONS IN REINFORCEDFIBER POLYMERIC COMPOSITES BY THE ELECTROSPRAY OFDEPOSITION WATERBORNE CARBON NANOTUBES Tansan Murat University aims study This the enhance to mechanical performance of fiber reinforced polymeric composites by depositionelectrospray of waterborne single-walled carbon dispersion nanotube dryonto carbon woven fabric. P4213-3 MOLECULAR SIMULATIONS OF INTERPHASE FORMATION OFPROCESS FIBER CARBON REINFORCED POLYMER COMPOSITES Yingdan Zhu of Material Institute technology and Engineering (NIMTE), Chinese Academy of Science reactionThe of cross- mechanism linking process and model of interphase carbon fiber reinforced epoxy composites developedwas and analyzed by molecular dynamics simulation.

, Singapore , Tokyo , Tokyo , The

P4212 structures Sandwich and materials Meeting room 216 room Meeting P4212-1 FRACTURE AND BEHAVIOR SHEET FACE BUCKLING OF ANALYSIS CFRP/HONEYCOMB PANELS SANDWICH TO SUBJECTED LOAD BENDING Oiwa Mae University of Agriculture and Technology clarified study the This local behavior buckling of sheet face the of a CFRP/Nomex honeycomb sandwich panel subjected to bending load four-point finiteusing element method. P4212-2 DESIGN EXPLORATION OF MULTI-LAYER SANDWICH STRUCTURES TRANSVERSE TO LOADING Anbazhagan Subramani University of and Design Technology P4212-3 DECONSOLIDATION OF BEHAVIOR FIBER CARBON REINFORCED THERMOPLASTICS AS CORE IN SANDWICH STRUCTURE Bing Xiao University of Tokyo - , , Carbon , Harbin

P4211 Resin and polymers Meeting room 215 room Meeting P4211-1 ANTIPLASTICSA TION OF ARYL ETHER EPOXIES Larry Reyes Nexus, for Institute Materials,Frontier Deakin University simultaneousThe ofimprovement and modulus, strength was strain-to-failure achieved for multi-aryl epoxies by varying the patterns substitution their backbonewithin without significant in Tg. decrease P4211-2 THE PREPARATION, PROCESSING HEALINGAND OF DIELS-ALDER THEIR AND EPOXIES FIBRE-REINFORCED POLYMER COMPOSITES Callum Branfoot University of Bristol 828Epon (DGEBA) modifiedwas into adaptable covalent networks (CANs) Diels-Alder using These chemistry. then there were CANs thermomechanically and characterised tested as matrices for functional FRP composites. P4211-3 THE ONE-POT SYNTHESIS, CHARACTERIZATION AND POLYMERIZATION OF HYPERBRANCHED BENZOXAZINE DERIVEDRESINS FROM A2 + B3 MONOMERS Cai Wanan Engineering University , , , Japan

P4210 methods Testing Meeting room 214 room Meeting P4210-1 EFFECTS OF GEOMETY AND STACKING SEQUENCE ON APPARENT RATIO POISSON’S OF QUASI- ISOTROPIC CFRPS LAMINATE UNDER THE COMPRESSION TESTS Eiichi Hara Aerospace Explolation Agency P4210-2 AXIAL COMPRESSION TESTING OF FIBERSCARBON Shipeng Zhu Aerospace Research of Materials Institute and Processing Technology, the study, this In axial compression of carbon strength fiber multifilament has been on determined a series PAN-based carbon fibers using bundle compression to test similar compressionthe measurement of unidirectional composites.laminated allows test This response for rapid and utilizes smaller amounts of material screeningfor initial testing. P4210-3 FIBER SINGLE PULL-OUT TEST FOR THE MATERIAL OF SELECTION RESIN A HYBRID COMPOSITE Holger Buettemeyer Bremen Faserinstitut e .V. deals study This fibre pull-outwith test. It gives general for recommendations embedding fibres the liquid resin. the into , University , Shimizu , type hydrogen Ⅳ P4209 Computational and finite element methods Meeting room 213 room Meeting Corporation paper introducesThis simulation a numerical for optimizing the mixture of fiber- the cement- reinforce composites.based Short fibers are individuallyarranged specimen.in the The model capabilities assessedare through bending analyses. P4209-1 DESIGN MATERIAL FOR SIMULATION REINFORCEDFIBER CEMENT-BASED COMPOSITES MESO-SCALE USING ANLYSIS Hiroki Ogura P4209-2 STRESS– DYNAMIC STRAIN RELATION OF ALUMINUM USING POWDERS MULTI-PARTICLE FINITE ELEMENT METHOD Kefeng Peng of Science and of China Technology on theBased multi-particle finite element methods,the dynamic stress–strain of granular relationship was metal materials determined. P4209-3 OF 70MPA DESIGN COMPOSITE HYDROGEN VESSEL STORAGE Cheng Shuo Hefei University of Technology modeling Accurate of vessel andstorage optimize structure the design by 3D on the scanner,based progressive damage theory predict burst cylinderspressure , , , Beihang

P4208 Nano-composites Meeting room 212 room Meeting P4208-1 OF RESOLE USE SEPIOLITE- PHOSPHATE NANOCOMPOSITE FOR BUILDING FACADES SoufeianiLeila University of Melbourne Combustibility of materials cladding system façade in the problem. a serious is Therefore, investigation of new nanocomposite material to be existing the replaced cladding’s combustible purpose the is material study. of this P4208-2 NUMERICAL INVESTIGATION ON MECHANICAL PROPERTIES OF POLYMER COMPOSITES REINFORCED WITH MXENE NANOSHEETS Daiva Zeleniakiene UniversityKaunas of Technology addressed is study This identifyto a suitable methodology based on finite element homogenization for predictionapproach of mechanical properties of polymer composite reinforced MXenewith 2D nanoparticles. P4208-3 POLYIMIDE AEROGELS CROSS-LINKED WITH AMINATED NANOWIRES: AG MECHANICALLY ANDSTRONG TOUGH Zhang Tianyi University , Korea , Kyoto , University

P4207 Joints Meeting room 211 room Meeting University analysesNumerical conducted to were fracture the investigate mode in the behavior toughnessII fracture test. Cohesive zone was modeling (CZM) the evaluate used to of adhesivesfailure and adherends. P4207-3 ONA STUDY OF THE CHANGE SHEARADHESIVE OF STRENGTH STEEL/ CARBON FIBER CARBON REINFORCED PLASTIC COMPOSITE BY SURFACE OF TREATMENT STEEL CARBON Seung Song Hak University the study, this In changes of the adhesive shear according to strength surfacethe roughness and oxidechange film presence were and the measured of fracture the cause analyzed through was surface fractured the observation. P4207-1 P4207-1 NUMERICAL OFMODELING ADHESIVELY BONDED JOINTSCFRP CONSIDERING NON-LINEAR OF DEFORMATION LAYERS ADHESIVE Mimura Shunta P4207-2 THE EFFECTS OF ENVIRONMENTAL CONDITIONS ON OF THE STRENGTH LAPDOUBLE JOINTS Aakash Paul of Bristol were Tests conducted Room at Dry, Temperature Dry Temperature Hot Temperature and Hot conditions. Wet changing The modes failure were identified, and material tests characterisation conducted to were joint the understand performance. , ,

P4206 and damage Fracture Meeting room 210 room Meeting P4206-3 DEVELOPMENT OF PROGRESSIVE ANALYSIS FAILURE METHOD FOR COMPOSITE LAMINATES CONTAINING WITHOPENINGS IMAGE DIGITAL CORRELATION Yoon Donghyun P4206-1 FRACTURE CHARACTERISTICS OF PARTICULATE REINFORCED COMPOSITES USING IMAGE DIGITAL CORRLELATION Sangdeok Kim Chungnam National University wedge study, this In testssplitting were performed evaluate to of behavior fracture particulate reinforced composite materials. digitalAlso, image method was correlation analyze to used the field. strain P4206-2 DAMAGE PROGRESSION OF NOTCHED UNNOTCHED AND COMPOSITE UNDER LAMINATES PICTURE-FRAME SHEAR LOADING Daniel Rapking Rx-FEM The was formulation applied topreliminarily two distinct material systems for a picture testing shear frame Both configuration. material systems and un- notched had configurations.notched Chungnam National University A progressive failure analysis model was developed crack- using accordingband-model existing researches.to evaluated and it was withcomparing resultsexperimental contour including strain DIC.obtained from results numerical The a good demonstrated the with correlation results.experimental , , University , Khalifa

P4205 Recycling and sustainability and energy renewable Meeting room 209 room Meeting P4205-3 OF UPCYCLING AEROSPACE CARBON SCRAP: IMPACT OF MATERIAL PROPERTIES Sanjeev Rao University P4205-1 OF INFLUENCE TYPESNOVEL OF OLEFIN-MALEIC- ANHYDRIDE BASED COPOLYMER ADDITIVES IN AND OF PA BLENDS PET RECYCLED Bianka Nagy of Pannonia Effects of olefin-maleic- copolymeranhydride based additives have been investigated blends. in PET/PA Compatibilizer having molecular lower and sameweight of half-ester and ratio unreacted anhydride most the groups was advantageous. P4205-2 DEVELOPMENT OF HIGH PERFORMANCE ALIGNED DISCONTINUOUS FIBRE COMPOSITES: FIBRE SURFACE MODIFICATION PozegicThomas University of Bristol Performance High The Discontinuous technologyFibre effective an is and high sustainable performance Aligned Discontinuous ReforcedFibre Composite (ADFRC) process,manufacturing potential the with for high production throughput. this In fibrepresentation, surfaces modified are throughput. increase to , , , Universityof

P4204 Process modelling Meeting room 208 room Meeting P4204-3 MACHINE-DRIVEN EXPERIMENTATION FOR SOLVING CHALLENGING CONSOLIDATION PROBLEMS Anatoly Koptelov Advanced Composites Collaboration for and ScienceInnovation (ACCIS), University of Bristol A new consolidation for framework sensor characterisation the of resin flow in composite precursors developed.was existing Unlike characterisation approaches, the proposed consolidation not limited is sensor typeby material the and predefined loading schedule test. for the P4204-1 MODELING OF STRATEGY IR LAMPS WITH INTEGRATED REFLECTOR IN THE USED MANUFACTURING OFPROCESS THERMOPLASTIC COMPOSITE TAPES Olivier De Almeida Clement AderInstitut P4204-2 1D SQUEEZE FLOW ANALYSIS OF CHOPPED FIBER LONG THERMOPLASTIC COMPOSITE Ali Waqas Twente objectiveThe of to is our work fibre the investigate separation matrix compressionduring moulding and for that, 1D squeeze flow experiments are performed in a flat geometry. , , Yonsei , Yonsei , Swinburne

P4203 Self-healing and dimensional three composites Meeting room 206 room Meeting Changwon National National Changwon University we study, this In apply 2D carbon the fiber beam for the optimizestructure, of the parameters the the beam through evaluationexperimental and analysis, and then try find optimum to the of beam the strength the by manufacturing 3D beam. University of Technology P4203-3 PI- ON CFRP STUDY BEAM PARAMETRIC STRENGTH AND ANALYSIS Park Geon Tae P4203-2 P4203-2 SELF-HEALING PROPERTIES OF CARBON-BLACK IMPREGNATED THERMOPLASTIC POLYURETHANE VIA PROCESSED DEPOSITION FUSED MODELLING Tamaddoni Fareed Jahromi P4203-1 MICROCAPSULE- BASED SELF- HEALING PROTECTIVE USING COATING OIL LINSEED HEALING AGENT Dong-min Kim University it was study, this In be developedto for a microcapsule-type self-healing protective linseed using coating a soft into oil turning film a healing agent as to for application cementitious materials linseedusing oil. , Clemson NSF-AFOSR Joint NSF-AFOSR on Workshop Mechanics-Based Design of Intelligent MaterialSystems by Additive Multimaterial 3 PART Manufacturing Meeting room 205 room Meeting Session continued 1400 from FUNCTIONALIZING BISTABLE COMPOSITE LAMINATE STRUCTURES Myers Oliver University EFFICIENT MULTISCALE OPTIMAL DESIGN FABRICATION AND OF CONTINUOUS REINFORCEDFIBER COMPOSITES Gowri Narasimha Boddeti, Singapore University of and Design Technology by Sponsored , , Ihi ,

P4201 Computational and finite element methods P4201-3 MICROMECHANICS OFMODELING TENSILE/SHEAR AND BEHAVIOR CRACK DENSITY OF COMPOSITE MATERIALS Daichi Haruyama Corporation the considered We the method evaluate to betweenrelationship and crack matrix and crack transverse stiffness degradation matrix of brittle composites. P4201-2 P4201-2 FINITE ELEMENT AND ANALYSIS EXPERIMENTAL TESTING OF NON- FABRIC CRIMP TENSION COMPACT SPECIMENS – INFLUENCE OF COHESIVE PROPERTIES. Dimitris Gouskos Imperial College London P4201-1 POTENTIAL OF APPLICATION MESH WOVEN WIRE TOWER AS PACKING LIMITER- BED COMPUTATIONAL APPROACH Ebrahiminejad Vahid University of Southern Queensland potential The bulk ofapplication Wire cross (WBC) truss-like periodic cellular metal packing tower future as support FEA evaluated. and CFD results were combined case for real optimise scenarios to bestthe porosity ratios. Plenary 2 1515-1520 1515-1550 THURSDAY 15 AUGUST THURSDAY Time 1525-1530 1520-1525

SCIENTIFIC PROGRAM 80 SCIENTIFIC PROGRAM SCIENTIFIC 83 ------, Institut , Institut , Tsukuba , Tsukuba , Meeting room 219 room Meeting P4215-5 OVERALL ELASTOPLASTIC PROPERTY OF PARTICULATE WITHCOMPOSITE STRAIN GRADIENT MATRIX Ma Hansong Laboratory of Nonlinear Mechanics (lnm), of Mechanics,Institute Chinese Academy of Sciences P4215-6 OF IDENTIFICATION THE QUASI-STATIC OF A BEHAVIOR COMPOSITE WOVEN THE TO SENSITIVE ENVIRONMENTAL CONDITIONS USING HO NUMERICAL MOGENIZATION RozyckiPatrick de Recherche en Génie Civil et Mécanique - Ecole de Centrale Nantes A double scale numer ical homogenezition obtain the to used is curve for astress-strain compos thermoplastic influenced is which ite and by temperature the humidity relative the of doing experinstead iments. P4215-4 OF ANALYSIS MICRO/MESO/ TEMPERA MACRO TURE-DEPENDENT ELASTOVISCOPLAS TIC PROPERTIES OF COMPOS WOVEN ITES Tetsuka Junpei University Elastoviscoplastic analysis of plain-woven fiberglass reinforced com (GFRP) plastic posites in consideration of temperature-de pendence of matrix carried is materials out based on the triple-scale homogeni method. zation - , Beihang , La Trobe , La Trobe SIC FIBER SIC , The Xinjiang Meeting room 218 room Meeting P4214-5 PROPERTIES AND STRUCTURAL PERFORMANCE OF KD-Ⅱ WITH DIFFERENT IN TEMPERATURE ARGON AND AIR ATMOSPHERE Chenxi Yang University high temperature The exposure for KD-Ⅱ siliconcontinuous carbide fibers was out 800°C,carried at 1000°C, 1200°C, 1400°C and 1500°C for 1 h in air atmosphere and argon prop the investigate to erties and structures evolution of fibers the tests, tensile using XRD and SEM analysis P4214-6 OIL-WATER USING SEPARATION MEMBRANES JANUS Baji Avinash University P4214-4 FACTORS THEGOVERNING STRENGTH TENSILE FIBRE OF BASALT Dan Xing of Institute Technical Physics and Chemistry, Chinese Academy of Sciences of seven strength The commercial basalt studied fibres was and compared, and factors affectingthe strength tensile the of these fibres were investigated. - - - - - , Faser , Institute , Institute , Beijing , Tongji , Tongji Meeting room 217 room Meeting P4213-7 P4213-7 INSPIRED MUSSEL MOD SURFACE AND IFICATION FUNCTIONALIZA TION METHOD WITH EFFICIENT HIGHLY ENVIRONMEN AND FRIENDLY TAL Wang Wencai University of Chemical Technology P4213-4 CHARACTERISATION OF BOND STRENGTH IN OVERMOULDED HIGH- PERFORMANCE THERMOPLASTIC COMPOSITES Robert Gaitzsch e.V. Bremen institut bond strength The of overmoulded fibre PAEK-carbon composites experi is mentally characterised a rib-pull-offusing test. Manufacturing varied are parameters effectsand the on are bond strength discussed. P4213-5 MODIFICATION OF CARBON FIBRE SURFACES SUFEX BY CLICK CHEMISTRY James Randall Materials for Frontier employmentThe of SuFEx ‘click’ were chemistries explored on carbon fibres first for the time. a 130% Remarkably, the to improvement IFSS in epoxy resin obtained, no with was fibre to degradation properties.tensile P4213-6 DIRECTIONAL USING LAMINATES NANOTUBE CARBON INTERFACES Shen Lulu University Self-sensing capability of carbon nanotube network as played on sensor in situ in delamination fiberglass reinforced composite laminates investigated. was , Beijing , The , , Harbin Meeting room 216 room Meeting P4212-7 P4212-7 MANUFACTURING COMPARISON AND OF SPRINGBACKED FIBER CARBON REINFORCED THERMOPLASTIC SANDWICH STRUCTURES Zhang Yunqian University of Tokyo focused study This novelon the manufacturing progress of CFRTP structures sandwich and improved energy abilityabsorption of the to structures sandwich extenta great low with density. P4212-4 MECHANICAL PROPERTIES ENERGY AND ABSORPTION CAPABILITY OF HYBRID HONEYCOMB SUPERSTRUCTURE Mengchuan Xu of Technology Institute paper introducesThis designthe concept of hierarchical the in the structures structures.AuxHex honeycombHybrid with superstructures ofsub-structures and arrows triangles proposed. were P4212-5 NUMERICAL SIMULATION OF IMPACT FORPERFORMANCE FILLED FOAM PMI CORRUGATED SANDWICH BOARD STRUCTURE Peiyan Yang Engineering University P4212-6 THE ANALYTICAL NUMERICAL AND CHARACTERIZATION REGARDING INDENTATION OF COMPOSITE HONEYCOMB SANDWICH STRUCTURES Xiaoyu Zhang Northwestern Polytechnical University paper focusesThis analyticalthe and methodnumerical ofon indentation structure sandwich shear considering effect and nonlinear collapse of core material. , , , Melamin

, The University Meeting room 215 room Meeting Deakin University resinsBisoxazoline due to emerging are transition high glass and temperatures fireimproved inherent performance compared traditional with epoxy resins. this In thermal the study, properties the and effect the bisoxzolineof CALIDUR™in the is composite structure investigated. P4211-7 POLYANILINE/ PHENOL- DIVINYLBENZENE RESIN FOR CFRP COMPOSITE WITH ENHANCED AND ELECTRICAL MECHANICAL PROPERTIES Zhou Yu of Tokyo study present The focuses on phenolic- modified Polyaniline/ Divinylbenzene enhancedresin with electrical conductivity and mechanical givesproperty, which resin systemthis a in future promising carbon fiber reinforced application. plastic P4211-4 NEW THERMOSET ON BASED MATRIX BISOXAZOLINES Salumeh Issazadeh P4211-5 MELAMINE- MELTBLOWN A HIGH- NONWOVEN PERFORMANCE MATERIAL FORCOMBINING THE FIRST TIME THERMOSET MELAMINE WITH EXCELLENT AND THERMAL ACOUSTIC PROPERTIES. Simona Lavric D.d. Kocevje P4211-6 LIQUID PROCESSABLE, STABLE, THERMALLY HYDROPHOBIC PHENOLIC- TRIAZINE RESINS FOR ADVANCED COMPOSITE APPLICATIONS Aristeidis Tsiamis University of Bristol (ACCIS) aim of projectThe the combine to ais commercial phenolic- (PT)triazine oligomer a liquid cyanate with ester monomer to produce liquid processable, stable,thermally PThydrophobic for advancedresins composite applications. , , , Meijo , University Meeting room 214 room Meeting University Considering deformation large ofbehaviors circular subjectedring to compressive force, an methodinnovative is developed measure to modulus of Young’s in a flexibleeach layer materials multi-layered plate). (wire,thin P4210-7 TEST A NOVEL METHOD TO BI-AXIAL INDUCE IN STRESS STATES CARBON THIN PLY COMPOSITES UNDER COMBINED LONGITUDINAL COMPRESSION TRANSVERSEAND TENSION Rev Tamas of Bristol objectiveThe of this develop to study an method test innovative ply thin carbon/using epoxy composites for a more allows that determination accurate of compressive for such strength materials. P4210-4 RESIN TREATMENT FOR RELIABLE TRANSVERSE SHEAR STRENGTH ASSESSMENT IN AEROSPACE STRUCTURES Chuaqui Tomas University of Bath is A resin treatment applied on short beam coupons produce to lessfar conservative predictions of transverse the of strength shear aerospace large components, by edgesuppressing free effects. P4210-5 INNOVATIVE AN CIRCULAR RING METHOD FOR MEASURING MODULUS YOUNG’S OF THIN FLEXIBLE MULTI-LAYERED MATERIALS (COMPRESSIVE METHOD) Atsumi Ohtsuki P4210-6 CHARACTERIZATION STATISTICAL AND OF ANALYSIS FIBER SINGLE OF STRENGTH VARIOUS FIBERS AT PROCESSING STAGES Ashok Rajpurohit Textiles Chomarat Industries addresses work This challenges in single fibre automatic It characterization. question: the ifanswers textile processes such or NCF spreading as affectsmanufacturing (and strength the parameters) Weibull of fibers during processing what and to extent? , Harbin , Xi’an , Harbin Meeting room 213 room Meeting P4209-4 A MICROMECHANICAL IN CYCLIC MODEL PLASTICITY FOR REINFORCEDFIBER COMPOSITES WAVY Danhui Yang UniversityJiaotong A micromechanical model based on parametric the finite-volume direct averaging micromechanics theory and the Abdel-Karim-Ohno cyclic constitutive build to model was cyclic the simulate of periodicbehavior composites wavy with microstructure. P4209-5 MULTISCALE ANALYSIS FAILURE OF 3D BRAIDED COMPOSITE STRUCTURE BY FEM AND COUPLING FFT METHOD Guodong Fang of Technology Institute P4209-6 INDENTATION OF RESPONSE TOPOLOGICAL LATTICE Xiao-fei Guo of Technology Institute propose a novel We periodic topological mechanical metamaterial, topological lattice, whose opposite surfaces have significantly different hardness.indentation , , Beijing Meeting room 212 room Meeting P4208-4 INTERFACIAL PROPERTIES OF MXENE/GRAPHENE/ MATRIX POLYMER NANOCOMPOSITES Kristina Žukienė UniversityKaunas of Technology study aim ofThe this the determine to is interfacial adhesion and compatibility MXene-polymerat interface andmatrix MXene/ overall the graphene/polymer nanocomposite performance. P4208-5 FATIGUE ENHANCED PROPERTIES OF OXIDE/ GRAPHENE BLACK/ CARBON RUBBER NATURE COMPOSITES Shipeng Wen University of Chemical Technology , , Haribin Meeting room 211 room Meeting P4207-4 P4207-4 HYBRID IN DAMAGE JOINTED GLARE STRUCTURES UNDER THE QUASI- STATIC Peifei Xu of Technology Institue P4207-5 MECHANICAL PROPERTIES OF LAP SINGLE CFRP JOINTADHESIVE Yanagisawa Kotono Metropolitan Tokyo University of strength The metal-CFRP adhesive evaluated was joint The quantitatively. betweenrelationship and failure strength mode of joints the was characterized. also , Xi’an , Beihang Meeting room 210 room Meeting P4206-4 MICRO-CRACK OFSTUDY MULTICRYSTALLINE SOLARSILICON BASED PANEL ON IN-SITU EXPERIMENT Zhang Yangbo University,Jiaotong Xi’an, China paper,an this In effective experimental tensile in-situ methodexperiment is a backboard with the study explored to behavior micro-crack of polycrystalline the silicon photovoltaic the including wafers, initiation micro-crack and propagation. P4206-5 INTERLAMINAR PROPERTIES OF CONTINUOUS REINFORCEDFIBER THERMOPLASTIC COMPOSITES WITH DIFFERENT RESIN FRACTION Zhang Tao University influenceThe of on theresin fraction propertiesinterlaminar glassof continuous fiber reinforced poly(phenylene sulfide) modified(PPS) with carbonmulti-walled (MWNTs) nanotubes and silicon carbide studied. were whiskers ,

, Kyushu , Kyushu , Meeting room 209 room Meeting P4205-6 SINGLE REAL-TIME MOLECULAR STUDY OF A PRETREATED CELLULOSE MODE HYDROLYSIS INDIVIDUAL AND ENZYME MOVEMENT Zhang Yanan Nanjing University of Technology P4205-4 IN NOVELTY RECYCLING OF WASTE ELASTOMERS IN BLENDS HDPE/PP EXPERIMENTAL BY COMPATIBILIZERS Lilla Simon-Stőger University of Pannonia, Faculty of Engineering, DepartmentInstitutional of MOL Hydrocarbon and Coal Processing has Rubbery waste been jointly recycled filleras of HDPE/PP by incorporation matrix of experimental compatibilizers for achieving property specific end-product selectingthrough with additive structure molecular suitable copolymer. weight P4205-5 EFFECT ON OF CFRP VORTEX-INDUCED OF VIBRATION A BRIMMED- SHROUD DIFFUSER FOR A WIND TURBINE Kim Taeyoung University discusses study This effectthe of CFRP brimmed- for the used onshroud diffuser vortex-inducedthe a using vibration coupling analysis of 3D analysismodal and 2D analysis.aeroelastic , , Beijing , Northwestern Meeting room 208 room Meeting P4204-6 NUMERICAL OF SIMULATION RUBBER OF FLOW COMPOUNDS IN FILLED PARTIALLY INTERNAL MIXER Haibo Yang University of Chemical Technology(buct) P4204-4 THEMODELING TEMPERATURE GRADIENT EFFECTON THE CURE-INDUCED OF DISTORTION L-SHAPED CFRP LAMINATES Li Yujun Polytechnical University P4204-5 A CHARACTERIZATION RELATING STUDY CROSS-SECTIONAL DISTRIBUTION OF FIBRE VOLUME FRACTION AND PERMEABILITY Filip Salling Rasmussen University ofTechnical Denmark , Harbin , Changwon Meeting room 206 room Meeting P4203-5 EFFECT OF TUBESVASCULAR ONDESIGN AND MECHANICAL SELF-HEALING PROPERTIES OF COMPOSITESCFRP Song Jungil University National P4203-4 THE OPTIMIZATION OF PROCESS PARAMETERS OF THREE- DIMENSIONAL NEEDLED COMPOSITES ON ANN BASED GAAND Qi Yunchao Institute of Technology Institute model for A surrogate optimizing process of three parameters needleddimensional of C/C-SiCpreforms composites was established based on back propagation network(BP) neural combing improved with genetic algorithm. NSF-AFOSR Joint Joint NSF-AFOSR on Workshop Mechanics-Based ofDesign Intelligent Material Systems by Multimaterial Additive Manufacturing PART 3 Session continued 1400 from by Sponsored Meeting room 205 room Meeting , Unist , Bristol , Bristol , School of Materials ScienceMaterials and Engineering, Beihang University, Beijing, China Plasma sprayed mullite/Lu2Si2O7- were coatings Lu2SiO5 vapor Water fabricated. behavior corrosion mechanism and failure investigated. were P4201-6 VAPOR WATER CORROSION BEHAVIOR FAILURE AND OF MECHANISM PLASMA SPRAYED MULLITE/LU2SI2O7- COATINGS LU2SIO5 Xunxun Hu P4201-5 MECHANICAL BEHAVIOR OF TEXTILE COMPOSITES A TWO-STEPUSING HOMOGENIZATION TECHNIQUE Chaeyoung Hong two-stepThe homogenization fiber/ method the at level andmatrix textilethe level It is presented. is this demonstrated capable of is approach efficiently predicting effectivethe properties of textile composites. P4201-4 APPLICATION OF A VARIABLE- KINEMATICS CONTINUUM ELEMENT SHELL THE ADAPTIVE TO NONLINEAR OF ANALYSIS COMPLEX SHELL STRUCTURES Hii Aewis K.W. Composites Institute (accis) A variable-kinematics shellcontinuum element, whose through-thickness kinematics are adaptively refined/ reduced `on-the-fly’ developed.is The model applied is to analysis fracture the of composites, with elementadaptive higher- using splitting cohesiveorder zone model. Plenary 2 1530-1535 THURSDAY 15 AUGUST THURSDAY Time 1540-1545 1545-1550 1535-1540

SCIENTIFIC PROGRAM 82 SCIENTIFIC PROGRAM SCIENTIFIC 85 , , Bristol , Bristol , Nanjing

4315 Aerospace Meeting room 219 room Meeting University of New At TheSouth Wales DefenceAustralian Force Academy adapters Payload structural the are provideelements that mechanical interface between spacecraft launch and a rocket paper, this vehicle. In new designs of the composite adapters proposedare and analysed. 4315-2 OF ADESIGN COMPOSITE MORPHING FISHBAC DEVICE FOR LIFT SPANWISE CONTROL Andres Rivero Composites Institute (ACCIS) - University of Bristol paper introducesThis of FishBAC use the the devicemorphing -a composite camber structure morphing for aerodynamicused for optimisation- aerodynamic spanwise The load control performed is study a fluid-structure using (FSI) modelinteraction developed around Plate Mindlin-Reissner Theory and (structures) correcteda viscous modellifting-line (aerodynamics). 4315-3 ANDDESIGN FABRICATION OF W-SHAPED DEPLOYALBE BOOM COMPOSITE ShiJiaqi University of Aeronautics and Astronautics 4315-1 ANDDESIGN OF THE ANALYSIS SPACECRAFT COMPOSITE ADAPTER PAYLOAD WITH LOCAL SUPPORTS Morozov Evgeny , , Harbin , U.S.

4314 Joints Meeting room 218 room Meeting 4314-2 4314-2 THERMAL-FLOATING ROLLER PEEL OF BEHAVIOUR COMPOSITE-TI JOINTSADHESIVE FOR REPAIR IsapalapatiSridhar Technological Nanyang University 4314-3 HIGH TEMPERATURE STRENGTH TENSILE OF C/ ANALYSIS COMPOSITE SIC AND SUPERALLOY JOINT BOLTED STRUCTURE Shuyuan Zhao of Technology Institute work, this In a progressive damage model for 2D woven C/SiC composite was predictestablished to high temperature performancetensile of behavior and failure single-lap, single-bolt 2D C/SiC composite joint.and superalloy of failure variations The imposed with strength and bolt temperature discussed were preload bolted studied for the joint. 4314-1 4314-1 OF VALIDATION LASER BOND (LBI) INSPECTION TECHNOLOGY Storage Kara Air Force Research Laboratory abilityBecause the inspectto bonded joints considered is a high priority within compositesthe Air the community, ResearchForce Laboratory funded has laser validate to work bond inspection (LBI). , , National , National , University of

4313 Smart composite structures Meeting room 217 room Meeting 4313-3 GRAPHENE- CARBON BLACK- RUBBER SILICONE COMPOSITE WITH LOW FILMS TEMPERATURE- COEFFICIENTS OF FOR RESISTANCE LARGE STRAIN SENSORS Balaji Mohan Velram University of Auckland 4313-1 PERFORMANCE OF RARE EARTH ORGANIC COMPLEXES LIGHTBASED SHAPE ACTIVATED MEMORY POLYMER COMPOSITES Madhubhashitha Herath Southern Queensland of Incorporation selectively triggered fillers photothermal fibreand glass reinforcements memory shape into polymer matrix demonstrated has to potential the develop light large-scale stimulus smart engineering applications. 4313-2 HIGH PERFORMANCE FIBER CARBON REINFORCED SHAPE MEMORY EPOXY COMPOSITES Liu Yayun Center for Nanoscience CAS and Technology, , , , Njust 4312 compositesHybrid Meeting room 216 room Meeting 4312-3 ACHIEVING FAILURE GRADUAL IN HYBRID COMPOSITE IN LAMINATES BENDING Meisam Jalalvand University of Strathclyde composite hybrid Two designed,beams are and analysedtested their failure study to process. Unlike composites,standard these hybrid composites a show very successful gradual a significant and failure dissipationenergy before final failure. 4312-1 EXPERIMENTAL NUMERICAL AND OF INVESTIGATION BEHAVIOR TENSILE OF CARALL WITH FABRICATED DIFFERENT FIBER ORIENTATION Gupta Rishi Kumar of Indian Institute Patna Technology behaviors tensile The of carbon fiber laminates aluminum in three fabricated different configurations using studied were experiment, finite element simulation strength and maximum observed in Al/0º/ Al/0º/Al configuration fiberwith pull out and delamination failure a major as mechanism. 4312-2 AND TENSILE THERMAL PROPERTIES OF TI/ LAMINATES CFRP ONBASED RESIN POLYIMIDE Hu Yubing , , Feng , Rmit

4312 Civil engineering matrix and ceramic composites Meeting room 215 room Meeting 4311-3 4311-3 BASE ADAPTIVE AN FOR CLT ISOLATOR STRUCTURES USING REINFORCEDFIBER COMPOSITES Chong LiaoWei Chia University 4311-1 HEAT VERTICAL OFTRANSFER ALUMINUM COMPOSITE CLADDINGS NguyenKate 4311-2 OF APPLICATIONS FRP PULTRUDED TUBES IN CIVIL INFRASTRUCTURE Aravinthan Thiru University of Southern Queensland reinforcedFibre (FRP) have Polymers increased gained popularity in civil infrastructure in recentapplications years. A review of field applications FRP pultruded where beensections have effectivelyused in is civil infrastructure presented. University , , , Monash , Monash

4310 intolerance Damage matrix and ceramic composites Meeting room 214 room Meeting University of Maine of resistance Damage compositea 3D woven compared with was of a 2D baseline that composite using impact,drop-weight absorptionenergy analysis, depth dent measurements, C-scan, andultrasonic Micro-CT imaging. 4310-3 AND IMPACT EDGE COMPRESSION AFTER IMPACT EDGE IN SIMULATIONS LAMINATES CFRP Albertino Arteiro University of Porto - Faculty of Engineering A composite damage model validated is levels higher at of test pyramid,the capturing accurately edgethe impact and compression after impact of response different composite openinglaminates, new perspectives for its on material use qualification through virtual testing. 4310-1 TOOLS SIMPLE FOR ASSESSING DELAMINATION GROWTH UNDER VARIABLE AMPLITUDE LOADS Rhys Jones University 4310-2 DAMAGE RESISTANCE OF THREE- DIMENSIONALLY CARBON WOVEN COMPOSITESFIBER Roberto Lopez-Anido , , MINES ,

4309 and damage Fracture Meeting room 213 room Meeting 4309-3 PRACTICAL INTERLAMINAR FRACTURE-BASED METHODSLIFE FOR AIRFRAMEBONDED STRUCTURE Carl Rousseau, Lockheed Martin Corporation. A simplified fracture method was and demonstrated further development issues identified. The ECTstatic test was explored; ENF-based onset andfatigue growth tests were and demonstrated; recommendations made. 4309-1 EFFECT OF THROUGH- THICKNESS COMPRESSIVE STRESS AND POROSITY ON THE STRENGTH TENSILE OF CARBON-FIBRE REINFORCED COMPOSITES Jan Rojek - PSLParistech UniversityResearch testing setup A custom designedis and the influence of porosity on investigated is strength tensile the of cross-ply CFRP specimens in the presence of a through- thickness compressive load. 4309-2 NUMERICAL OF INVESTIGATION REINFORCEDCNT INCOMPOSITE CRASH Rouhi Mohammad RISE SICOMP AB in absorption Energy in composite crash strongly is materials dependent on the fibre architecture layup, and type of resin, thermoplastic e.g. vs. thermoset. Thus, modelling of the of behaviour crash composites highly is influenced by the chosen composite system, and material constitutive models some extent to have be to tailored to systemthe under consideration. , , ,

4308 Fibers Meeting room 212 room Meeting 4308-3 OF THE EVALUATION EFFECT OF TENSION DURING CARBON FIBRE PROCESSING Claudia Creighton Carbon Nexus, Deakin University 4308-1 NANO-MAGNETITE DECORATED FIBRE CARBON FOR ENHANCED SHEAR INTERFACIAL STRENGTH Sobhan Fakhrhoseini Carbon Nexus/deakin University 4308-2 SIMULTANEOUSLY INCREASING THE HYDROPHOBICITY INTERFACIAL AND OFADHESION FIBRES: ACARBON PATHWAY SIMPLE PASSIVE INSTALL TO FUNCTIONALITY COMPOSITESINTO ArnoldChantelle Deakin University findings ofThe dispel study this commonthe misconception of fibreincreased wettability amounting in increase an to composite strength and provides a method ofrapid surfaceinstalling functionality that offacilitates adaptation carbon fibres for new applications. , , Harbin , National , National

4307 structures Sandwich and materials Meeting room 211 room Meeting Khalifa University 4307-3 THE ENERGY- ABSORBING CHARACTERISTICS OF COMPOSITE- REINFORCED HONEYCOMBS CantwellWesley 4307-1 RESIN SIMULATING FORINFUSION MANUFACTURING SANDWICH- STRUCTURED COMPOSITES KaoYi-Kai University Hua Tsing 4307-2 VIBRATION ATTENUATION OFPERFORMANCE COMPOSITE HYBRID LATTICE PANELS SANDWICH WITH COMBINED HIGH DAMPING MATERIALS Yang Jin-Shui Engineering University , , LSE , Nanyang , Nanyang

4306 Composite structures Meeting room 210 room Meeting 4306-3 TECHNOLOGICAL IMPLEMENTATION OF A TOROIDAL COMPOSITE PRESSUR VESSEL FOR HYDROGEN STORAGE Norbert Schramm GmbH composite toroidal The vesselpressure with manufactured windingnew ring technology a large has potential saving mass compared 30%) to (up cylindricalto pressure vessels for hydrogen 700 bar. at storage 4306-1 ANALYSIS LOAD WIND OF SMALL TURBINE BLADES WITH FIBER-METAL SKIN LAMINATE Sai Wei Technological University 20kW the Calculated turbine wind small wind loading at blade speeds 7.5m/s, of 6m/s, The and 10m/s. 8.5m/s, airfoilstress in the was numerically studied in colorand displayed codes the show to stress concentration software The area. is study in the used MATLAB. 4306-2 DESIGNING FOLDABLE COMPOSITE STRUCTURES ON THE MICROMETRE SCALE Arthur Schlothauer ETH Zürich developmentThe of foldable ultra-thin composites for small scale applications (nano-satellites or heart-stents) investigated is to regard with maximizing stiffness maintaining whilst packagability. , , , 4305 Additive manufacturing Meeting room 209 room Meeting 4305-3 EFFECTIVE TENSILE OF STRENGTH ADDITIVELY MANUFACTURED DISCONTINUOUS FIBER- CARBON REINFORCED VIA POLYMER COMPUTED TOMOGRAPHY Striemann Patrick University of Applied Science Ravensburg- Weingarten ofA combination destructive and non- destructive testing used tomethods is process-compensate induced defects by additive manufacturing in an effectiveresulting strength tensile and a local material performance. 4305-1 FIFDM – ADVANCED 3D PRINTING WITH CONTINUOUS FIBER REINFORCEMENT Jens Schlimbach 4305-2 OF EVALUATION BUNDLEA FIBER A TWISTING AT CURVED SECTION OF 3D PRINTED FIBER CARBON COMPOSITES Shiratori Hirohide of Institute Tokyo Technology has study present The revealed twisting the of amechanism carboncontinuous fiber bundle in a process a of printing curved section and itsevaluated effect mechanicalon the properties. Institut Für Für Institut Verbundwerkstoffe Gmbh FRPC an are ideal lightweight material construction theyas combine low density very with high mechanical performance. is there However, of a lack generally processesautomated productionfor the of geometrically complex components with load-specific and economical fiberthus reinforcement.

, , University , Auckland

4304 Process modelling ofand machining composites Meeting room 208 room Meeting 4304-3 STUDY NUMERICAL OF THE 3D-FLOW CHARACTERISTICS DURING COMPRESSION OF SMC MOULDING AlnerssonGustaf AbGestamp Hardtech model A numerical for compression moulding of Sheet Moulding Compound is based the in which presented, modelled is as charge a fluid a specified with viscosity. 4304-1 SIMULATING COMPRESSION- RESIN INDUCED FROMTRANSFER A NON- SATURATED A DRY INTO WOVEN STRUCTUREFIBER Allen Tom University 4304-2 EXPERIMENTAL AND CALIBRATION OF VALIDATION MATRIX POLYMER COMPOSITES IN SUPPORT OF PROCESS MODELING Gibson Thao of Dayton Research Institute paper discussesThis experimental andthe effortscharacterization support to required developmentthe of a finite element- based computational of polymericsimulation thermoset polyimide composite processing. , School of , The , Institute , Institute

4303 Nano-composites Meeting room 206 room Meeting 4303-3 IMPROVED MECHANICAL BARRIERAND PROPERTIES OF GRAPHENE/ FIBRE- CARBON HYBRID EPOXY COMPOSITES Yao Xudan University of Manchester Graphene/carbon hybrid fibre/epoxy composites were through fabricated followed coating spray by resin infusion. distribution Uniform achieved withwas propertiesbarrier improved. 4303-2 3D GRAPHENE/ POLYMER NANOCOMPOSITES FOR HIGHLY AND SENSITIVE STRECHABLE SENSORS Shuying Wu Engineering, Macquarie University work present The highly demonstrates sensitive strain based on 3Dsensors networkgraphene including graphene aerogel and vertical Effectsgraphene. theof of 3D microstructure on sensing graphene performance of its nanocompositesPDMS systematicallywere investigated. 4303-1 BASEDGRAPHENE NANOCOMPOSITES FOR TRIBOLOGICAL APPLICATION Wang Han of Research, Metal Chinese Academy of Science work, this In graphene used as were additiveslubricating for improving tribological behavior of graphene-based nanocomposites. NSF-AFOSR Joint NSF-AFOSR on Workshop Mechanics-Based Design of Intelligent Material Systems by Additive Multimaterial 4 PART Manufacturing NSF-AFOSR Joint Joint NSF-AFOSR on Workshop Mechanics-Based ofDesign Intelligent Material Systems by Multimaterial Additive Manufacturing DISCUSSION PANEL by Sponsored Meeting room 205 room Meeting , , ,

Exhibition hall 4301 ONR Solid Mechanics Symposium Coffee break 4301-3 DYNAMIC MODE-II INITIATION CRACK PROPAGATION AND OF BEHAVIOR FIBER/ CARBON UNDER EPOXY ELEVATED MOISTURE CONTENT Rodrigo Chavez University of California San Diego effectThe of moisture dynamicon the mode-II stress intensity offactor carbon fiber/ epoxy composites Notched studied. was carbon epoxy fiber/ specimens high with contents were moisture subject dynamic to experiments fracture samples . The were loaded under mode-II conditions and samplescompared to no significantwith content. moisture Technical University ofTechnical Denmark work aim of The this consists in developing a novel test rig, which by the inspired is Bending Shear Torsion designed(STB) rig for unidirectional composites. 4301-2 4301-2 DEVELOPMENT OF A MODE I/ II/III TEST RIG FOR COMPOSITE AND LAMINATES FACE/ SANDWICH CORE FRACTURE CHARACTERIZATION Pietro Sabbadin 4301-1 FRACTURE MECHANICS FORSOLUTIONS INTERFACE CRACKS AND IN BI-MATERIAL BEAMS SANDWICH Roberta Massabo University of Genova Plenary 2 1620-1640 1620-1820 1550-1620 THURSDAY 15 AUGUST THURSDAY Time 1640-1700 1700-1720

SCIENTIFIC PROGRAM 84 SCIENTIFIC PROGRAM SCIENTIFIC 87 , Japan , Meeting room 219 room Meeting 4315-5 OFMODELING EFFECTVOID ON MATRIX-DOMINATED OF CFRP STRENGTH LAMINATES Shigeki Aratama HeavyKawasaki Industries, Ltd. and locations Void were dimensions investigated statistically CT images. X-ray using proposedA model was effectfor the of voids reductionon the of matrix-dominated of CFRPstrength laminates. 4315-4 DETAILED EVALUATION OF VISIBLE IN DEFORMATION LAMINATES CFRP OUT- TO SUBJECTED OF-PLANE IMPACT LOADING Takeda Shin-ichi Aerospace Exploration Agency authorsThe visible investigated and deformation of damages internal thermoset laminated Out-of- CFRP to owing impactplane loading. , , , University Meeting room 218 room Meeting 4314-5 4314-5 JOINING OF RESISTANT AGEING STRUCTURES OUT OF LIGHT METALS CARBON AND COMPOSITES BY ULTRASONICS Balle Frank of Department Freiburg, Systems of Sustainable Engineering 4314-6 INCREASING THE OF STRENGTH MECHANICALLY JOINED CONNECTIONS AND OF METAL FIBER-REINFORCED PLASTICS USING A STRUCTURED JOINING AUXILIARY ELEMENT Marcel Droß Universität Technische Institute Braunschweig, and of Tools Machine Production Technology plasticity low The to in comparison metals represents a limiting for factor plastics fiber-reinforced in mechanical joining systems. Therefore, the a at aims study present auxiliarypin-structured joining element as a new technology support for increasing load-bearing the capacity of mechanical joints between metal and fiber reinforced plastics. 4314-4 4314-4 DISCRETE DAMAGE OF MODELLING COUNTERSUNK FASTENED LAMINATED COMPOSITES IN BEARING Alex Harman Defence Science and Group Technology , , Centre , Seoul Meeting room 217 room Meeting 4313-6 THREE- DIMENSIONAL CONSTITUTIVE OF SHAPE MODEL MEMORY POLYMER COMPOSITES CONSIDERING RATE-DEPENDENT BEHAVIOUR KimJinsu UniversityNational 4313-4 COMPOSITE ORIGAMI FOR ARTIFICIAL FLUIDIC MUSCLES Michael Dicker University of Bristol Realising high- performance fluidic by combiningactuators designsnew origami compositewith materials. 4313-5 4D PRINTED PROGRAMMABLE STRUCTURES BASE SHAPE ON ACTIVE MEMORY POLYMER COMPOSITES Qinghua Guan for Composite Materials and Structures, Harbin of Technology Institute three study, this In programming methods of 4D compositesprinted based and structures on external loads, and pre-strain internal viscoelasticity were investigated presented here. ------, , East China , East , Beijing Meeting room 216 room Meeting 4312-6 OF PREPARATION SIO2/ HOLLOW POSS/FLUORINATED - POLY(2,5-THIENYLB ENZOBISOXAZOLE) NANOCOMPOS WITHITE FILMS DIELEC- ULTRA-LOW TRIC CONSTANT Zhe Zhang University of Science and Technology A novel method to 6FP fabricate BO-POSS-HMS nanocomposite films dielectric ultra-low with constant, excellent mechanical properties and high-temperature resistance. 4312-4 ENVIRONMEN EFFECTS TAL ON NOTCHED OFCOMPRESSION HIERARCHICAL NANOENGINEERED COM AEROSPACE POSITES STUDIED MICROTO X-RAY BY MOGRAPHY Reed Kopp Massachusetts Institute of Technology Open-hole compression of CFRP aligned- with CNT interlaminar was reinforcement conducted across hygrothermal various micro- conditions. X-ray computed tomography employedthen for hot/ dry condition reveal to non-destructively the complex 3D damage progression. 4312-5 HETEROSTRUC- TURED {001} TIO2/G-C3N4 GREATLY HYBRIDS H2 ENHANCED FROMPRODUCTION UNDER WATER LIGHT IRRA UV-VIS DIATION Zhang Hui University of Chemical Technology Nanosheet array-like hy heterostructured in {001}TiO2 with brids growth on g-C3N4situ remarka shows layers bly improved hydrogen (26.2evolution rate mmol•g-1•h-1) under irradation light UV-vis upon high separation efficiency of photocre electron-hole. ated , , , Shanghai , Shanghai Meeting room 215 room Meeting 4311-6 4311-6 DYNAMIC MECHANICAL IN-SITU ANALYSIS MATRIX OF CERAMIC COMPOSITES AT 1300°C IN OXIDIZING ATMOSPHERE Christian Kudisonga The University of Queensland 4311-4 4311-4 TEXTILE REINFORCED CONCRETE COMPOSITES FOR ADVANCED CONSTRUCTION APPLICATIONS Priyan Mendis University of Melbourne 4311-5 IN-SITU X-RAY COMPUTED TOMOGRAPHY CHARACTERISATION OF TENSILE DAMAGE EVOLUTION IN TEXTILE MATRIX CERAMIC COMPOSITES Daxu Zhang University Tong Jiao damage Tensile evolution of plain matrix ceramic weave composites was by in-situ the studied CT X-ray nanofocus and theirexperiment progressive damage were mechanisms established. , , Beihang , Inner Meeting room 214 room Meeting 4310-6 DESERT- OF USE SANDS TO SYNTHESIZE MGSIO3-SIC COMPOSITE CERAMICS Zhiming Shi Mongolia University of Technology work present The synthesize to aims MgSiO3-SiCp the composite ceramics desert- natural using evaluate sand and to their microstructure and properties. 4310-4 MAXIMISING THE FRACTURE OF RESISTANCE GLASS FIBRE COMPOSITES BY CONTROLLED LARGE FIBRE SCALE BRIDGING Stergios Goutianos University ofTechnical Denmark work, present the In increase aim to we resistance fracture the of unidirectional composites by large scale fibre bridging. the that shown It is fracture steady-state canresistance be several increased times by modifying the fibre sizing and matrix material. 4310-5 DETECTION ON CURING OFPROCESS LARGE THICKNESS USING COMPOSITE BRAGG FIBER GRATING Zhang Guowei University the investigate To and strain temperature history throughout process curing the of thickness three-large Kevlar/ hundred-ply epoxy composite fiber the laminate, (FBG) grating Bragg adjacently were embedded in the composite specimen monitor situ in to and temperature the evolution at strain points5 monitoring thicknessalong the direction.

, , , KU Leuven Meeting room 213 room Meeting 4309-6 FIBRE THE CRITICAL BREAK CLUSTER FOR LONGITUDINAL OF FAILURE TENSILE UNIDIRECTIONAL COMPOSITES: MISCONCEPTIONS NEWAND INSIGHTS Swolfs Yentl commonThe misconception that critical cluster the the from originates to prior cluster largest debunked, and is failure fibre-hybridisation is significantly to shown clusters. large stabilise 4309-4 STRAINS MAPPING FIBREAND FRACTURE IN FIBRE CARBON COMPOSITES IN SITUUSING VOLUME DIGITAL CORRELATION Erich Schoberl University of Southampton paper presentsThis a novel application of Digital Volume and (DVC) Correlation Synchrotron in situ ComputedRadiation (SRCT) Tomography loading uniaxial to in Carbon Fibre Reinforced Polymers is DVC (CFRPs). a relatively novel for quantifyingtool full-field volumetric anddisplacements fields.implicit It strain novel, that shown is mechanistically consistent be may measurements fibre to in relation made events.failure 4309-5 ESTABLISHING SCENARIO DAMAGE OF RANDOMLY ORIENTED STRAND (ROS) THERMOSET COMPOSITES MULTI- USING INSTRUMENTATION MICRO-CTAND SouffoisLoic Unniversityof of Technology Compiègne scenario A damage oriented of randomly thermoset strand composites is established under loading. tensile purpose, this In multi insrumentation including digital image acoustic correlation, emission, microscopy is and tomography used. , Deakin , Mines Meeting room 212 room Meeting 4308-4 EFFICIENTAN HIGH-THROUGHPUT GRAFTING PROCEDURE FOR ENHANCING FIBRE- CARBON TO-MATRIX INTERACTIONS IN COMPOSITES Daniel Eyckens University talk describesThis the chemical modification of surface the of carbon fibres by diazonium salts. covalent The of of theseattachment salts surface the to through initiated was and means different outcomesthe of each discussed. is 4308-5 OF ADAPTATION WEIBULL ANALYSIS REPRESENTTO STRENGTH OF BEHAVIOUR BRITTLE FIBRES IslamFaisal ParisTech , Center for , LOMC Meeting room 211 room Meeting 4307-4 AND FABRICATION COMPRESSIVE OF BEHAVIORS FIBER CARBON REINFORCED COMPOSITE SANDWICH STRUCTURES WITH CURVED-CREASE FOLDCORE Du Yuntong Composite Materials and Structures, Harbin of Technology Institute A composite sandwich foldcore based structure on curved-crease designed is origami The and fabricated. curved-crease foldcore better a much have capacityantibuckling foldcore. chevron than 4307-5 FLAXUSING FIBRES SHIVESAND IN SANDWICH STRUCTURES FOR TRANSPORT APPLICATIONS Safa Essid articleThis presents an experimentally of investigation bending quasi-static of anbehavior flaxinnovative based and structure sandwich a reference material, typically used for truck and floors.walls , , Indian , UNSW tute of Technology of Technology tute i Meeting room 210 room Meeting 4306-6 BUCKLING OF UD BEHAVIOUR CARBON/EPOXY SUBJECTED PANELS DIRECTTO LIGHTNING STRIKE Thomsen Ole Thybo University of Southampton, School of Engineering 4306-4 ENHANCED INTERFACIAL PROPERTY OF FIBRE CARBON COMPOSITES ONBASED VERTICAL GRAPHENE Zhao Sha interfacialThe shear of carbon fibrestrength was and epoxy matrix improved dramatically verticalwith graphene on carbon fibre grown surface by plasma enhanced chemical depositionvapor low method relative at temperature. 4306-5 EFFECT OF LIGHTNING STRIKE ON THE BUCKLING OF BEHAVIOUR COMPOSITE – A MATERIALS FINITE ELEMENT STUDY T M Dhanya Inst India Bombay, , , Xi’an , IHI IHI , Meeting room 209 room Meeting 4305-6 ADDITIVE MANUFACTURING OF ADVANCED REINFORCEDFIBER COMPOSITES AND APPLICATIONS Xiaoyong Tian University,Jiaotong China Additive manufacturing for composite material been has structures to investigated componentsfabricate integrated with performance of structure, material, and functions, thus overcome the to bottleneck problems fieldsin the of additive and manufacturing composites. 4305-4 PATH LOAD FOR VISUALIZATION TRAJECTORYFIBER OPTIMIZATION OF ADDITIVE MANUFACTURING COMPOSITES Suzuki Takuya Corporation A methodology of fiber trajectory optimization proposedis for Additive Manufacturing of composites. The and stiffnessstrength simultaneously were improved by the proposed method. 4305-5 OF HIGHDESIGN TEMPERATURE RESISTANT THERMOPLASTIC COMPOSITES FOR FDM 3D PRINTING Daniel Therriault Polytechnique Montréal presents work the This development of carbon high- fiber-reinforced resistant temperature thermoplastics processabilityfeaturing in melt mixing, printability for fused deposition modeling (FDM), and high mechanical properties meetto aerospace standards. , , Centre , The Meeting room 208 room Meeting 4304-6 PREDICTING LIFE FATIGUE OF COMPOSITE MATERIALS Ferdous Wahid Materials for Future (CFM), University of Southern Queensland 4304-4 MODELING COMPLEXITIES IN THE PROCESS SIMULATION OF POLYMERIC COMPOSITE MATERIALS Robert Brockman University of Dayton Institute Research Composite process modeling presents unique challenges due evolution continuous to of key material properties. paper This discusses issues with conventional adapting test methods to process modeling, sensitivityand the of data predictions to and measurement reduction methods. 4304-5 FINITE ELEMENT FORMING SIMULATION OF COMPLEX COMPOSITE PANELS SANDWICH Shuai Chen University of Nottingham , , Deakin Meeting room 206 room Meeting 4303-5 UNDERSTANDING DISPERSION CNT IN POLYMER PRECURSOR AND SOLUTIONS PROPERTIES OF COMPOSITES FROM SCALE THE ATOMIC Hendrik Heinz University of Colorado Boulder 4303-4 HIGH GAS BARRIER PROPERTIES OF POLYMER/MOS2 NANOSHEET NANOCOMPOSITES Jin Zhang University Hydroxyl-functionalized MoS2 nanosheets obvious shown has modification effect polymer on a PVA matrix, including helium gas ultralow high permeability, break at elongation and toughness and thermal high in-plane conductivity.

NSF-AFOSR Joint Joint NSF-AFOSR on Workshop Mechanics-Based ofDesign Intelligent Material Systems by Multimaterial Additive Manufacturing DISCUSSION PANEL by Sponsored Meeting room 205 room Meeting CONTINUED , , Queens 4301-5 COMPARISON OF IN-PLANE COMPRESSIVE CHARACTERISTICS OF HEXAGONAL AUXETICAND HONEYCOMBS WITH FIBRE REINFORCEMENTS Zafer Kazancı University Belfast 4301-4 COMPUTATIONAL OFMODELING LOW-VELOCITY RESPONSE IMPACT CARBON OF WOVEN LAMINATES IN ARCTIC CONDITIONS Prabhakar Pavana University of Wisconsin- madison Plenary 2 ICCM Conference Banquet Melbourne Room,Melbourne MCEC 1720-1740 THURSDAY 15 AUGUST THURSDAY Time 1845-2230 1800-1820 1740-1800

SCIENTIFIC PROGRAM 86 SCIENTIFIC PROGRAM SCIENTIFIC 89 , DLR - , Singapore , Hunan University, Hunan , East China UniversityChina East ,

5115 and structures Sandwich materials 5115-1 ON THE LOW- STUDY VELOCITY IMPACTING AND RESPONSES PROPERTIES OF RESIDUAL SANDWICHES COMPOSITE Xintao Huo paper revealedThis the ofimpacting mechanism structures. foam sandwich and analyticalNumerical developedmodels were to support design the of structural crashworthiness. Besides, the residual properties also were considered 5115-2 OF A LAYERED UTILIZATION NANOCOMPOSITE BY CONSTRUCTED NANOSHEETS LITAWO6 PORPHYRIN COBALT AND TO AS ELECTRO-CATALYST REDUCTION OXYGEN JinpengLi of Science and Technology Layered nanocomposite was CoTMPyP/LiTaWO6 by exfoliation/constructed self-assembling method, and electrocatalyticthe activity of nanocomposite oxygen to tested. reduction reaction was 5115-3 SANDWICH COMPOSITE A OF OPTIMIZATION PANEL STIFFENED STRUCTURE M. Meddaikar Yasser German Aerospace Center for Optimization strategy compositessandwich based on parameters, applied lamination a stiffenedto panel problem. 5215-1 ADHESION INTERFACIAL BETWEEN CARBON FIBRE THERMOPLASTIC INCOMPOSITES FOAM AND STRUCTURESSANDWICH Quan Ngoc Tran Le of Manufacturing Institute A-STAR Technology, several study, this In of skin- the investigations interfacecore of sandwich conducted, are structures including physico-chemical based on surfaceinteractions and mechanicalenergies interlocking influenced by foam surface morphology. 5215 and structures Sandwich materials Meeting room 219 room Meeting , Rmit University , Tu Dortmund , Tu , Isae-supaero

5114 Joints 5214 Joints Meeting room 218 room Meeting 5114-1 INTERFACE INTERLOCKING IN METAL-CFRP DESIGN JOINTS A MONTE- USING SIMULATION CARLO APPROACH Günther Fabian University joint single lap experimental In the test and FEM simulations qualitative and quantitative positioning of mesoscale pin in interlocking CFRP structures joints developed are by a Monte-Carlo approach. 5114-2 JOINTSMICROPINNED UNDER LAP SHEAR CONDITIONS LOADING Simon Inverarity a new present approach We micropinned jointsto which involves interference fitting, and its for effecta is characterised composite-to-metal under joint loading. shear lap 5214-1 MODEL ZONE COHESIVE ON MODE IDENTIFICATION ASSEMBLY: I BONDED SENSITIVITY AND ROBUSTNESS ANALYSIS JaillonAgathe , inspire , University , JSOL JSOL , , The University

5113 Process modelling 5213 Process modelling Meeting room 217 room Meeting 5113-1 VIRTUAL AND HYBRID EXPERIMENTAL THERMOFORMING OF GFRP ALUMINUM AND Michael Grubenmann IVP thermoforming A hybrid process of fibre- glass and reinforced thermoplastic process considering aluminum parameters, geometry tool experiments is and validation experimentally and virtually investigated. 5113-2 AND EVALUATION ON THE SIMULATION PROCESSMOLDING CARBON OF CHOPPED REINFORCED TAPE FIBER THERMOPLASTICS Tiansheng Han of Tokyo evaluate to aims research This compressionthe molding outcome of a specific short fiber CFRTP ROS named as UT-CTT utilizing analysis the thickness and ratio of charge of free-edge samples and process the a with simulate new modeling technology and in LS-DYNA®, implemented mechanical to eventually leads property prediction on based pre-setthe molding conditions. 5213-1 OF THE MODELLING METHODHIPERDIF FOR MANUFACTURING COMPOSITES RECYCLED SPH USING Huntley Samantha of Bristol enables HiPerDiF reclaimed remanufacturing carbon fibres comercially- into productsvaluable by ensuring a high-level of fibre alignment. fluidThe dynamic alignment process modelled is SPH using modeland the validated. is 5113-3 ANALYSIS STRENGTH THE RESULT USING OF COMPRESSION SIMULATION MOLDING CARBON FOR LONG REINFORCEDFIBER THERMOPLASTICS Hayashi Shinya Corporation New compression molding techniques for long simulation fiber CFRP a beam-in- using solid couplingadaptive function and a component strength deformedanalysis the using presented. beams are

, University of , Jan Dlugosz , Seoul National

, Beihang University

5112 Composite materials 5212 Interfaces & interphases Meeting room 216 room Meeting 5112-1 FORMABILITY SIMULATION OF STEEL-POLYMER COMPOSITES SANDWICH Sungjin Han University andSandwich structures materials 5112-2 TURBINETIDAL BLADE COMPOSITES USING FIBRE REINFORCED BASALT EPOXY POWDER Conchur Bradaigh Edinburgh energyRenewable 5212-1 GRAFTING CARBON NANOTUBES ON SURFACE FIBER CARBON THE ENHANCING AND PROPERTIES INTERFACIAL OF COMPOSITES Shu Xiong Interfaces and interphases 5112-3 MATERIALS NEW HYBRID ON CARBON BASED NANOTUBES METAL AND ALLOYS Damian Kulawik University Hybrid composites , , KU , University of , Xi’an Jiaotong

5111 Biocomposites 5211 Biocomposites Meeting room 215 room Meeting 5111-1 EFFECT OF DIFFERENT ON TREATMENTS SURFACE FIBERS CURAUA Linconl Teixeira Brasília 5111-2 BAMBOO FIBRE COMPOSITES - MOISTURE AND DURABLERESISTANT Aart Vuure Willem Van Leuven Bamboo high fibres show in composites for use potential of combination gooddue to mechanical properties, high availability, abundant capabilityCarbon capture and they their keep factthe that mechanical properties high at humidity. 5211-1 FRACTURE TOUGHENING OF PERITUBULAR DENTINE POROUS IN BIOLOGICAL MICROSTRUCTURE Rong Wang University of PTD role The microstructure properties fracture on the of investigated is dentine human by analysis of its tip shielding crack effect and on microcracks macrocracks. 5111-3 COMPOUNDING NATURAL FIBERS WITH HIGH TEMPERATURE- PROCESS THERMOPLASTICS WITH SHEAR SOLID-STATE FLAX/ PULVERIZATION: 6 POLYAMIDE Katsuyuki Wakabayashi Bucknell University A chilled twin extrusion screw process called Solid-State effectivelyShear Pulverization fibers compounds natural polymerswith are that incompatibleconventionally because of their high processing temperature. , , Central , University of Bath

5110 Rail 5210 tolerance Damage Meeting room 214 room Meeting 5110-1 MATERIALS COMPOSITE SECTOR FOR THE RAILWAY Roberto De Villoria Guzman FIDAMC 5110-2 OF ENDPOST INFLUENCE ON SUB- MATERIALS RAILHEADSURFACE OF DAMAGE MATERIAL RAIL JOINTS INSULATED WHEEL/RAIL DUE TO LOADINGS CONTACT Mandal Nirmal Queensland University 5210-1 FOR MODEL A PLATE TOLERANCE DAMAGE DESIGN AND PREDICTION LOADING FOR MULTI-AXIAL Mark Nielsen A new semi-analytical method for predicting the delamination which at strain initiate will propagation sublaminate following for design Adaptation buckling. included, is optimisation benefitshowing of non- surface plies.standard

, Bristol , Bristol , NLR - , Isae - Supaero

, Auckland University Segula Sad 5109-1 ELEMENT NEW INTERFACE WITH NON COINCIDENT SIMULATE NODES TO IN DISCRETE DAMAGE LAMINATE COMPOSITE Antoine Trellu 5109-2 OF ANALYSIS COMPARATIVE TECHNIQUESMODELLING ON THICK FOR IMPACT COMPOSITE FABRIC STRUCTURES Hoorn Niels Van Netherlands Aerospace Centre A comprehensive due of damage characterisation impactto events fabric on thick remains composite structures task.an elusive and challenging methods varying with Three degrees of computational complexity developed are and predict a simulate to impact problem. representative 5109-3 NONLOCAL AND LOCAL CONTINUUM DAMAGE OF IMPACT SIMULATION AFTER COMPRESSION AND TESTS ON CFRP IMPACT LAMINATES Reza Vaziri 5209-1 DETERMINING THE TRUE STRAIN OF FAILURE TENSILE FIBRE COMPOSITESCARBON AFFECTING IT FACTORS AND Michael Wisnom Composites (ACCIS) Institute specimenNovel tests that show volume and ply thickness have effect greater tensilea much on of carbon-epoxy strain failure stress components.other than 5109 and damage Fracture 5109 and damage Fracture Meeting room 213 room Meeting , Delft Delft , (Plenary 2) , University of , Harbin Engineering , The University of Tokyo

Brian CoxBrian , United States Office of Naval Research, Office States , United USANaval of 5108-1 SPHERICAL TRUNCATED SHELL COMPOSITE FOR TRANSMITTING ELECTROMAGNETIC WAVE BEARINGAND CAPACITY LOAD UNDER WIND Lili Tong University thickness of paper, this In which radome a sandwich consisits of two dense dielectric by skins a less dense relative a lower having core the than dielectric constant by determined are skin for highest equations Maxwell coefficientstransmission and stiffness. 5108-2 TESTING AND ANALYSIS OF A THERMOPLASTIC STIFFENEDCOMPOSITE UNDER PANEL COMPRESSION Dooren Kevin Van University of Technology analysisThe and test results compositeof a thermoplastic stiffened panel under compression be will presented. has separation Skin-stringer been modelled by VCCT and by experimental bewill validated testing. 5108-3 OF MOLDING EVALUATION EFFECTSPROCESSES ON INTERNAL GEOMETRY OF ORIENTED RANDOMLY STRANDS YI Wan geometry internal The property, key the considered is which combines inner that the factor mechanical with structure properties, for evaluated is both strands oriented randomly quantitatively under and visually molding processes.different 5208-1 STRENGTH AND BUCKLING OF VARIABLE ANALYSIS STIFFNESS PANELS FABRIC BY MANUFACTURED STEERING TECHNOLOGY Zhaofei Xiao Glasgow 5108 Composite structures 5208 Composite structures Meeting room 212 room Meeting Yapa Rajapakse Yapa , Clement Ader (Meeting 213) room , Boeing Australia , Japan , Concordia University , University of Glasgow

Michael Edwards 5105-1 VULNERABILITY OF STRUCTURECOMPOSITE FUSELAGE UNDER INTERNAL BLAST EFFECTS: MITE APPROACH CollombetFrancis Institute 5105-2 OF SHOCKWAVE INFLUENCE OF ON LIGHTNING DAMAGE LAMINATE CFRP Hirano Yoshiyasu Aerospace Exploration Agency 5105-3 PROCEDURESDESIGN LAMINATE FOR IMPROVED IN BENDING PERFORMANCE EXTENSIONAND Lee Jason articleThis discusses improved performance relating laminate properties both in-plane to (e.g. first and out-of- ply failure) propertiesplane initial (e.g. double angle-plybuckling) using ±Ψ and ±Φ ply (with laminates stiffness are which orientations), laminate standard to matched configurations. 5205-1 COIL SPRINGS COMPOSITE 4D PRINTING BY MADE METHOD Suong Hoa of compositeCharacteristics coil by method made the ofsprings this In presented. are 4D printing changes method, structure the the to simple shape initial from curing final complex after shape and cooling. 5105 Aerospace Advanced manufacturing and Advanced manufacturing automation 5205 Meeting room 209 room Meeting , USQ , Norwegian , Institute of Aircraft , Institute , University of Bristol

5103-2 ON IMPACT BALLISTIC COMPOSITE-COVERED THE AND CERAMIC EFFECT ON PROJECTILE FRAGMENTATION B.Bernt Johnsen Defence Establishment Research (FFI) A composite cover on alumina ballistic the can improve performance. highest effect The a cover with back on the was and not on the of alumina, the face. strike 5103-1 COMPACTION MODELLING IN OUT-OF- VARIABLITY PREPREG AUTOCLAVE LAMINATE Daria Bontch-Osmolovskaia paper proposesThis an methodexperimental for imaging a flowthe air through of trapped stack. laminate The prepreg OOA quantify to goal is volume the between trapped the of air, manufacturing plies the during process the cause will which porosityundesirable in the part.cured 5103-3 MODELLING NUMERICAL COMPOSITES OF UHMWPE LOADING UNDER IMPACT Behjat Ansari A finite element model is developed predict to energy interfaces the at absorption underof UHMWPE laminates varying of impact. rates 5103 Defence 5203-1 VOID PHASE DUAL INPREDICTION YARN MICROSCOPIC MODELS Silvio Faccioto Design - University of Stuttgart 5203 modellingMultiscale Meeting room 206 room Meeting , Tohoku University (Meeting 219) room , Tohoku

- MULTI-SCALE MODELING OF FIBER-REINFORCED PLASTIC COMPOSITES: FROM ATOMISTIC MODELING TO STRUCTURAL TO DESIGN MODELING PLASTIC OF FIBER-REINFORCED MODELING COMPOSITES: FROM ATOMISTIC MULTI-SCALE Tomonaga Okabe Tomonaga (Meeting 212) room COMPOSITES FORRESIN INFUSION AEROSPACE MANUFACTURING RELATED DEFECTS –WHERE AND WHY THEY WHY AND OCCUR, DEFECTS DO THEY Simon AND Bickerton –WHERE MATTER? RELATED MANUFACTURING LAMINATES FOR MULTI-SCALE 3D PRINTING SYSTEM NATURE’S AMELOGENESIS: , Deakin University , Nihon University

, Northwestern

KEYNOTE 4: Move to concurrent sessions concurrent to Move

KEYNOTE 3: KEYNOTE 2: MENTAL MENTAL MATERIALS Aoyagi Takao been on studying have We effective defibration of bacterial cellulose (BC) and recently found polycaprolactone-grafted that very was usefulBC suspension a thermo-responsive prepare to drug control to membrane permeation. 5101-2 NETWORKSEPOXY DERIVED AMINES FROM NOVEL Varley Russell 5101-1 - CELLU BACTERIAL LOSE-POLYCAPROLACTONE COMPOSITES AS ENVIRON KEYNOTE 1: PLENARY LECTURE: IN COMPOSITES FOR STRUCTURES MARINE CHALLENGES Plenary 2 sessions concurrent to Move 5101 materials matrix Polymer 5201-1 INVESTIGATION NUMERICAL METHODSON THE LOADING EFFECT SIZE FORAND RESPONSE COMPRESSION OF BRAIDED COMPOSITES Peng Liu Polytechnical University effectsThe of sample size and loading methods on compression braided ofresponse triaxially the composite numerically are meso- the using investigated scale finite method. element Exhibition hall 5201 Dynamic properties and fracture Coffee break Plenary 2 Day 5 Welcome & Announcements 5 Welcome Day 0930-0940 0940-1000 0850-0900 0900-1040 0900-0930 1000-1020 1100-1230 1020-1040 1040-1110 1110-1130 FRIDAY 16 AUGUST FRIDAY Time 0800-0805 0805-0850

SCIENTIFIC PROGRAM 88 SCIENTIFIC PROGRAM SCIENTIFIC 91 , Onera , The , School of , Kanazawa , Seoul National 5215-3 ON A BEAM ON ELASTIC ANALYSIS FOUNDATION FORMODEL SANDWICH TEST SPECIMEN SCB Takaryu Kazuya of Technology Institute be on applying noted to Points an analysis model named “beam foundation on Vlasov model” SCB sandwich test to specimen discussed. are 5215-4 EXPERIMENTSBUCKLING OF THE ANALYSIS AND SANDWICH SOFT-CORE BEAMS Dongjian Zhang Aeronautics, Northwestern Polytechnical University 5315 analysis and Structural optimisation 5315-1 A NEW ANALYTICAL THE PREDICT TO MODEL STIFFNESS OF FILAMENT COMPONENTSWOUND Michael Heitzmann University of Queensland 5315-2 ON THE OF PARAMETERIZATION LAMINATES ORTHOTROPIC OPTIMIZE COMPOSITETO STRUCTURES Irisarri François-Xavier with deals presentation This optimization ofthe orthotropic lamination using laminates parameters. An additional defines variable orientation the axes of of material the Link with made symmetry. is parameters. polar 5215-2 EXPERIMENTAL FORMABILITY STUDY OF STEEL-POLYMER COMPOSITES SANDWICH Jewook Yang University Meeting room 219 room Meeting , , , Nippon , KINDAI, , Department of 5314 Aerospace Institute of Technology Institute methodJoining between sheet and CFRTPaluminum Fiber(Carbon Reinforced sheet without Thermo-Plastic) rivets by induction using discussed, was heating were and joining strength investigated. 5314-1 METHODOLOGY A NOVEL QUANTIFY TO SHAPE COMPLEXITY OF AEROSPACE COMPOSITE PARTS Chowdhury Tanvir Mohammad The University of Nottingham paper introduces a newThis quantify to metric Shape the Complexity of composites partsaerospace CAD using early from design information stages. 5314-2 SIMULATION NUMERICAL SHELL OF FOLDABLE EXTENDIBLE TUBE OF UNIDIRECTIONAL COMPOSITE Doto Yuki Aeronautics and Astronautics, University Tokyo, of Tokyo, Japan About a new deployable and of made shells structure a film, FEM and experiments conducted investigate to were its extending and behavior deployability. 5214-4 DIRECT MECHANICAL JOINING BETWEEN CFRTP SHEET METAL AND HIGH FREQUENCYUSING INDUCTION HEATING Kaname Fujisaku Meeting room 218 room Meeting 5214-2 INDUCTION WELDING OF WOVEN- BEHAVIOR LAMINATES CF/PPS HIGH FREQUENCYUSING CONTINUOUS INDUCTION HEATING Kazuki Kurima University clarified study behavior the This of induction of welding woven- the using CF/PPS laminates high frequency of supply power 2.0MHz.around 5214-3 FIBER/PEEK CARBON RIVETS FOR FASTENING COMPOSITES STRUCTURES Laberge LebelLouis Polytechnique Montreal molded-in rivetsC/PEEK were CFRP and Steel joints by Joule The and pressure. heating higher is strength shear tested typicalthan grade aerospace rivets.aluminum , Department , Michigan , School of , Ulsan National 5313 Process modelling Meeting room 217 room Meeting 5313-1 FINITE ELEMENT OF LAYUP MODELING WITH HEAT PROCESS TRANSFER AND OF CFRTP DEFORMATION Nishikawa Masaaki of Mechanical Engineering and Science analyzed study present The the and viscoelastic transfer heat of materials the deformation processing thermal the during coupled using of CFRTP, based on finite simulations element method. 5313-2 OF MODELING MULTISCALE THERMOSET COMPOSITE PROCESS-INDUCED STRESSES RESIDUAL Maiaru Marianna University Technological A novel Integrated multi-scale Computational Material (ICME)Engineering approach predict evolutionto the of curing residual stress during of thermoset composites is presented. Aeronautics, Northwestern Polytechnical University, Xi’an, China 5213-2 RESIN OF THE SIMULATION IN A TRI-AXIALLY TRANSFER BRAIDED PREFORM USING EFFECTIVE PERMEABILTY Hye-gyu Kim of Science andInstitute Technology for the simulations Numerical molding processresin transfer performedare observe to the resin tri-axial flow the through the including preform, braided effect.temperature 5213-3 EFFECT OF CURING CYCLE OF ON THE STRENGTH WING COMPOSITE UAV STRUCTURES Zhendong Liu , Deakin Meeting room 216 room Meeting 5212-2 BASED PHOSPHORUS MIMETIC ACID A-AMINO FLAMEFOR ENHANCED PROPERTIES RETARDANT RESIN EPOXY IN AN Melissa Stanfield University projectThis employs surface emulsion electroinitiated polymerisation (SEEP) process modifyto carbon surfaces; on generating focusing interfacesmultilayer induce to novel physical and chemical properties carbon in fibre reinforced composites. This process scalable, rapid, is be any appliedand able to to conductive surface. , IIT DELHI , University of , School of Materials Meeting room 215 room Meeting 5211-4 BIOINSPIRED ACHITECTURES TOWARD DAMAGE IMPROVING ON CFRP RESISTANCE LAMINATES AmorimLuís Minho velocity low Under impact, the CFRPbioinspired laminates more shown proposed have onset and damage to tolerance damages,less larger to prone a standard compared to when one. aeronautic 5211-2 OF BIOCOMPATIBILITY B-CA3(PO4)2/MG-ZN COMPOSITES PREPARED METALLURGY POWDER BY Yu Kun Science and Engineering, SouthCentral University 5211-3 TUNING THE MECHANICAL THERMO-AND RESPONSES MECHANICAL NANOCOMPOSITE OF BIO OF PLASTICIZEDFILMS WITH ACID POLYLACTIC NANOTUBES HALLOYSITE Swati Sharma acid (PLA),Poly-lactic a polyester natural derived from resources been had modified in its improve to ductility work this To help the ofwith plasticizer. decrease for the compensate halloysite strength, in tensile (HNT)nanotubes been have in plasticized PLA.incorporated , Imperial , Nanyang , Nanyang , Institut für , Institut , ArianeGroup , China Academy, China of 5310 Repair Meeting room 214 room Meeting 5310-1 STRENGTH TENSILE OF BOLTED PREDICTION ON COMPOSITE REPAIR LAMINATE Xiang Li Engineering Physics 5310-2 ANALYSIS AND DESIGN WITH REPAIRS OF SCARF CIRCULAR ROUNDED AND REPAIR RECTANGULAR CUTOUTS IdapalapatiSridhar University Technological 5210-4 THE DAMAGE ENHANCING OF SRPP/CFPP TOLERANCE COMPOSITES VIA A HYBRID DESIGN BIO-INSPIRED Mencattelli Lorenzo College London successfully designedWe micro-engineered SRPP/ tailoring via CFPP structures meet to patterns laser-cut tolerance damage different different at requirements same the within locations engineering creating structure, solutions of significant impact. industrial 5210-2 VELOCITYLOW IMPACT ON LAMINATE MODELLING COMPOSITE: AN APPLICATION INDUSTRIAL PeresPatrick validation Industrial methodology of velocity low impactcomputation on based resultsexperimental CFRP with sizes for different of sample. 5210-3 IMPACT LOW-VELOCITY A WITH SIMULATION FOCUS ON THICK SPECIAL COMPOSITES Sachse Ronny - UniversitätFlugzeugbau Stuttgart the paper investigates This influence thickness of laminate and initiation on damage velocity low during propagation impact. An enhanced cohesive modelzone and impact are for validation simulations presented. , Kyushu University, Kyushu , Kaust (king, Kaust , Industrial , Industrial 5209-4 EXPERIMENTAL OF INVESTIGATION MICRO/MACROSCALE MECHANISM DAMAGE IN THERMOPLASTIC COMPOSITES QUASI- UNDER IMPACT AND STATIC Arief Yudhanto Abdullah University of Science and Technology) 5209-2 THICKNESS EFFECTOF PLY DAMAGE ON IMPACT CFRP PLY MODE OF THIN LAMINATES Kohei Yamada Center of Fukui Technology Prefecture impact tests and study, this In CAI tests varying impact the conducted using were energies which laminates quasi-isotropic ply(0.02, different thicknesshad mm). 0.24 0.12, 5209-3 MODELING A SIMPLE PREDICTING TO APPROACH PROGRESS DAMAGE IN UNIDIRECTIONALLY STRAND CHOPPED ARRAYED LAMINATES Shigeki Yashiro Meeting room 213 room Meeting , University of , Beihang University , Center for Composite , Northwestern , Tohoku University , Tohoku 5308-1 PROPERTIES TENSILE OF NANOCELLULOSE REINFORCED SILKWORM FIBERS COMPOSITE SILK Chen Wu 5308-2 HIGH-PERFORMANCE CELLULOSE FIBRESNANOCOMPOSITE AS COMPOSITE SUSTAINABLE REINFORCEMENT Chenchen Zhu Bristol 5208-4 COPPRESSIVE AND DESIGN PROPERTIES OF LONG- LASS-FIBER REINFORCED THERMOPLASTIC LATTICE OCTAHEDRAL STRUCTURE Zhao Yueqing compressive paper, this In properties of diverse octahedral assembled by structures lattice cross-shaped partsnonplanar by mechanical interlocking method investigated. were 5208-2 MECHANICAL OFPERFORMANCE PYRAMIDAL HIERARCHICAL AND MATERIALS LATTICE IT’S THREE DIMENSIONAL MAPS MECHANISM FAILURE Jian Xiong and Structures,Materials Harbin of Technology Institute 5208-3 EFFECT OF ABSORBENT ON FILLING FOAM OF BEHAVIORS MECHANICAL 3D PRINTED HONEYCOMBS Yan Leilei Polytechnical University 5308 Fibers Meeting room 212 room Meeting - - , Fidamc , Pacific , University of , Institut für , Institut , Institute of Aircraft , Institute

MATIC LAY-UP AND IN-SITU AND LAY-UP MATIC THE TO CONSOLIDATION DEVELOPMENT OF A REIN COVER SKIN FORCED WING PROJECT – OUTCOME María Isabel Martín 5305-1 FIBER AUTOMATED PLACEMENT AND PRESSING VARIOTHERMAL OF THERMOPLASTIC TOWPREGS Peter Mitschang GmbH Verbundwerkstoffe 5305-2 ONENHANCEMENTS PREFORMING AUTOMATED FOR COMPOSITE STRUCTURES HelberFlorian Design 5205-4 OF AUTO APPLICATION 5205-2 VIRTUAL MATERIAL OF 3D CHARACTERISATION COMPOSITES CartwrightBruce Engineering Systems International Pty Ltd 5205-3 MULTIPLE-FRONT FOR POLYMERIZATION RAPID COMPOSITE MANUFACTURING Polette Centellas Illinois At Urbana-champaign polymerization offersFrontal significant time savings cure compositeover conventional Applying a manufacturing. initiates local trigger heat polymerization; therefore, using furthermultiple triggers reduce times large- and enable cure scale manufacturing. 5305 and Advanced manufacturing automation Meeting room 209 room Meeting , , Chair of, Chair Plastics , Autodesk Australia , Autodesk Australia , Harbin Engineering

5303-2 OF MODELLING BEHAVIOUR MECHANICAL OF MXENE/POLYMER NANOCOMPOSITES Gediminas Monastyreckis UniversityKaunas of Technology aimed to was study This mechanical the investigate properties of MXene/polymer nanocomposites. finite The element modelling of a single MXene flake and MXene/polymer performednanocomposite was conditions.under tension 5303-1 THE DOUBLE TO A SOLUTION J-INTEGRALCRACK’S IN THE PLAIN PLATE LiHuan University 5203-3 THERMO- ANISOTROPIC VISCOELASTIC RESIDUAL STRESS FOR MODEL OF SIMULATION WARPAGE PARTS MOLDED INJECTION Zhiliang Fan Pty Ltd 5203-2 OF INFLUENCE ORIENTATION FIBER RECONSTRUCTION ON MECHANICAL PROPERTIES OF SHORT REINFORCEDFIBER THERMOPLASTICS Kevin Breuer Technology reconstructed is Fiber orientation as well as harmonics by spherical by method of entropy. maximum representative Subsequently, volume elements generated are influence the investigate to effectiveon the composite properties. 5303 Mechanics of composites Meeting room 206 room Meeting , Institut , Institut

, Onera , Wuhan University, Wuhan , Johns Hopkins, Johns

Clément Ader - IMT Mines Albi Microscopy and DSC techniques model to used PEKKare crystallizationisothermal kinetics a coupledwith kinetic equation. induced by Transcrystallinity andcarbon fibres investigated is by of means a pixelsimulated method. coloring 5301-2 ISOTHERMAL CRYSTALLIZATION OF PEKK MODELING COMPOSITES: KINETIC AND PREDICTIONS MORPHOLOGY Olivier De Almeida 5301-1 EFFECT OF NOVEL INTUMESCENT FLAME ON THERMAL RETARDANT FLAME AND STABILITY PROPERTIES RETARDANCY OF CONTINUOUS GLASS FIBRE REINFORCED POLYPROPLENE COMPOSITES Hongda Chen of Technology Lunch Exhibition hall 5301 materials matrix Polymer 5201-3 EXPERIMENTAL OF CHARACTERIZATION SENSITIVITY STRAIN-RATE PROPERTIES OF ON FAILURE COMPOSITE CARBON/EPOXY CoussaFabien 5201-2 EFFECTOF MICROSTRUCTURE AND ON THE STRAIN-RATE TRANSVERSE COMPRESSIVE OF UHMWPE STRENGTH COMPOSITES Parker Jason University Plenary 2 1210-1230 1230-1330 1330-1510 1330-1350 1350-1410 1150-1210 FRIDAY 16 AUGUST FRIDAY Time 1130-1150

SCIENTIFIC PROGRAM 90 SCIENTIFIC PROGRAM SCIENTIFIC 93 , Herr , Imperial College , Changwon 5315-5 HIERARCHICAL AEROGEL CARBON MODIFIED CARBON COMPOSITES FORFIBER STRUCTURAL POWER APPLICATIONS Anthony David London Multifunctional structures containing carbon aerogels positivelycontribute to electro-chemical double layer capacitive performance but mechanicalreduce overall properties; addition the of nano-scale (carbon reinforcers proposed are to nanomaterials) address these concerns. 5315-3 EVALUATION MECHANICAL HYBRID ON SUS410-CFRP LONG LOAD OF HEAVY PIN CHAIN ROLLER PITCH Chang Uk Kim UniversityNational analysis structural study, this In of - load long pitch a heavy out carried and was chain roller pin was metal/composites the and evaluated manufactured CFRP. using 5315-4 STRUCTURALPREDICTION MOLDED OF INJECTION REINFORCED FIBER LONG PLASTICS ON BASED FIBER INDUCED PROCESS MICROSTRUCTURE WillemsFabian Meeting room 219 room Meeting - , Rmit , FIDAMC , Kaist Meeting room 218 room Meeting 5314-3 OF THE INTERPLAY DEGRADATION COMPOSITE FOR LONG MECHANISMS LIFETIME AIRCRAFT OPERATION Katherine Grigoriou 5314-4 AND RADIATION SPACE HYPERVELOCITY IMPACT EARTH OF LOW SHIELDING STRUCTURES ORBIT SPACE ULTRA-HIGH- USING MOLECULAR-WEIGHT POLYETHYLENE Jihun Cha 5314-5 INNOVATIVE SHERLOC: AND MANUFACTURING STRUCTURAL HEALTH OF THERMO MONITORING PLASTIC STRUCTURES Tortosa Jacinto , University , Chalmers University of , Composites Research Meeting room 217 room Meeting 5313-3 INDEX FOR COMPATIBILITY DEFECT FREE FORMING CURVATURE WITH DOUBLE Andrew Rhead of Bath A compatibility index that identifies stacking sequences defect minimise which experimentally is formation of various forming via validated stacking sequences a onto complex an industrial using tool former. double diaphragm 5313-4 AND MODELING EXPERIMENTAL OF THE VARTM VALIDATION PROCESS Da Wu Technology propose a novel model to We predict thickness the variation fiber preforms of thin-walled process. VARTM the during high model The shows computational efficiency and good accuracy justified by an experiment.infusion 5313-5 FINITE ELEMENT OF BI- MODELLING WITH AXIAL FABRIC BENDING CONSIDERING STIFFNESS FOR COMPOSITES PREFORMING Fei Yu Group, University of Nottingham A macro-scale finite element developedmodel was by effects the incorporating of bending stiffness,fabric in assess to order its significance predictionon the of defect during onset and propagation forming. Meeting room 216 room Meeting Meeting room 215 room Meeting , Defence , University of , Defence Science Meeting room 214 room Meeting 5310-3 FOR APPROACH A NOVEL REPAIR BONDED HYBRID OF PRIMARY METALLIC STRUCTURES Chang Paul and Technology 5310-4 PATCH WET-LAYUP OF COMPOSITE REPAIR STRUCTURES Andrew Charles Group Science and Technology 5310-5 KISSING OF COMPARISON DE- DISBOND BOND AND FECTS LAMINATES IN CFRP AFTERCOMPRESSION BY TESTING IMPACT Robert Pierce Ningbo China Nottingham Defects been have in CFRP samplesmanufactured a simple newusing method, and their effect on compression and CAI performance been has investigated. Meeting room 213 room Meeting - , KU Leuven , Sapienza University , Basque Country, Basque 5308-3 PROPERTIES OF TENSILE FIBRES CARBON SINGLE AUTOMATED TESTED WITH EQUIPMENT Mesquita Francisco An extensive of amount single carbon properties fibre tensile automated using gathered were equipment. fibre diameter, The and stiffness strength tensile analysed.Some fibreswere unexpectedshowed results, newproviding insights on single fibre testing. 5308-4 OF NEW SYNTHESIS PEPTIDES IN BASED NON AND NATURAL AMINOACIDS NATURAL À LAPOSSESSING CARTE POLARITIES FOR SURFACE OF NATURAL MODIFICATION FIBERS Iván Rivilla University work, this In a present we modifynew to route basalt fibers synthesis on the based andof peptides, natural ring-opening through unnatural, polymerization process. 5308-5 OF FUNCTIONALIZATION HYDRO FIBERS BY BASALT GROWTHTHERMAL OF ZINC NANOSTRUCTURESOXIDE LilliMatteo of Rome Chemical, and morphological mechanical analysis of basalt zinc with fibres decorated a through oxide nanostructures process different at hydrothermal growth times. Meeting room 212 room Meeting , National , National , Gifu University , Chalmers University 5305-3 LASER-ASSISTED THERMOPLASTIC TAPE PLACEMENT: EFFECTS OF AND HISTORY THERMAL ON PLACEMENT SPEED OF STRENGTH PEEL WEDGE CF/PA6 ZinneckerVictoria University of Australia effect the paper investigates This tapeof different placement three speeds six and process different peel wedge on the temperatures of unidirectional CF/ strength in manufactured laminates PA6 tape placement a laser-assisted process. 5305-4 DEVELOPMENT OF BEND- FORMING TECHNOLOGIES ON CFRTP TUBE Banno Tatsuya both experiment research, this In has approach and numerical been investigate to challenged mechanism. bend-forming the was simulation Bend-forming predictchallenged to defects, limits and reliability of forming. 5305-5 HIGH PERFORMANCE/ COMPOSITE HIGH RATE TRAPPED WITH PROCESSING RUBBER Blinzler Brina of Technology processing, rubber an Trapped achieving to alternative autoclave compositehigh pressures during processing, requires an accurate material thermomechanical model for implementation. Meeting room 209 room Meeting , National University, National , Harbin Institute of , Harbin Institute , National University, National of 5303-3 A NEWTONIAN-MECHANICS- MECHANISM BASED FOLDINGCONTROL PROTEIN Lin Yang Technology 5303-5 EXPLICIT DAMAGE OF MODELLING COMPOSITES UNDER COMPRESSIVE LOADING Jie Zhi Singapore presents work a high-fidelityThis discrete-smeared integrated for modelling approach crack compositenotched laminates under compressive loads. loads predictedThe failure well compare and patterns and experimental data with observations literature. in the 5303-4 CONSISTENCY MECHANISM OF COMPOSITE ANALYSIS IN ACCELERATED RUBBER TEST DEGRADATION Wang Yashun of Defense Technology test methodA likelihood ratio consistency mechanism for the analysis of composite rubber products in an accelerated developed is test degradation to validity the ofensure test data. Meeting room 206 room Meeting - , , Shizuoka , Dalian University of Technology a significant Particle size has influence friction on the Oversizedmechanisms. particles of resistance wear the improve but without causing materials, excessive wear. disc 5301-3 EFFECTOF CERAMIC ON SIZE PARTICLE RESIN OF PERFORMANCE COMPOSITE MATRIX FRICTION MATERIAL Xuesong Fu The University of Auckland behaviour complex The fatigue of composites the requires identification of service the life under cyclic loads, which mechanical involves intricate study Therefore, this testing. identify to sought a relationship between five-cycle load/ unload and full cycle fatigue performance. 5301-5 RELATION ACOUSTIC LOAD/ BETWEEN 5-CYCLE FULL-CYCLE AND UNLOAD OF COMPOSITES FATIGUE WITHOUTWITH AND RESIN CHANNEL FLOW Kariappa Karumbaiah Maletira POLYMERS WITH HYDROXYL WITH HYDROXYL POLYMERS - GROUPS VIA THE BENZOXAB INTERACTION OROLE-DIOL Kotsuchibashi Yohei 5301-4 OF CO FUNCTIONALIZATION of Science andInstitute Technology A facile functionalization method of poly(ethylene-co- vinyl alcohol) (EVOH) nanofiber demonstrated meshes was benzoxaborole-diol the via betweeninteraction EVOH and benzoxaborole-based copolymers. Plenary 2 1430-1450 1450-1510 FRIDAY 16 AUGUST FRIDAY Time 1410-1430

SCIENTIFIC PROGRAM 92 The ICC, Belfast Northern Ireland Dates: 1st – 6th August 2021

Visit our stand to win free registration and accommodation at ICCM 23 Belfast www.iccm23.org 95

POSTER PROGRAM POSTER PROGRAM 96 97

MONDAY 12 AUGUST POSTER SESSION MONDAY 12 AUGUST POSTER SESSION Poster title Presenter name Poster no Poster title Presenter name Poster no Additive manufacturing Ceramic matrix composites DEVELOPMENT OF COMPOUND MELT EXTRUDED NANOCOMPOSITE FDM FILAMENT BY CONTINUOUS SYRINGE PUMPING OF DISPERSED Joshua Brooks P001 BEHAVIOR OF GFRP BARS SUBJECTED TO DYNAMIC LOADING Farid Abed P050 NANOFILLERS DURING EXTRUSION RESIDUAL BEARING CAPACITY OF RC MEMBER AFTER EXPOSURE TO HIGH TEMPERATURE Lili Bai P051 OPTIMIZATION OF PROCESS PARAMETERS FOR FUSED FILAMENT FABRICATION USING TOOL PATH REVERSING Vishal Hayagrivan P002 IMPROVEMENT OF PENETRATION RESISTANCE OF AMINE CURED EPOXY RESIN FOR CONCRETE LINING BY ION EXCHANGE ZEOLITE Tetsuya Sakai P052

FLEXURAL FATIGUE STRENGTH OF 3D-PRINTED CONTINUOUS CARBON FIBER REINFORCED THERMOPLASTIC LAMINATES Morihumi Inaba P003 UNDER SULFURIC ACID POSTER PROGRAM 3D PRINTING OF CONTINUOUS SIZED CARBON FIBER REINFORCED PA6 COMPOSITES Tengfei Liu P004 Composite Materials: Route to Impact INTERLAYER BONDING BEHAVIORS OF 3D PRINTED CONTINUOUS CARBON FIBER REINFORCED PEEK COMPOSITES Meng Luo P005 UNDERSTANDING RESIDUAL STRESS IN RAPIDLY CURED CARBON FIBRE REINFORCED COMPOSITE Saman Ghadi P053 DEVELOPMENT OF A TEST BENCH FOR FUSED FILAMENT FABRICATION Alexander Matschinski P006 EVALUATION OF THERMOELECTRIC PROPERTIES OF GRAPHENE-ENABLED REINFORCED POLYMER COMPOSITES: A PROFICIENT MOVE Azadeh Mirabedini P054 TOWARDS ADVANCED STRUCTURAL APPLICATIONS IMPROVING THE STIFFNESS OF HIGH RESOLUTION DLP STEREOLITHOGRAPHIC MATERIAL Chow-shing Shin P007 A STUDY ON HEAT TRANSFER EFFECT OF HEAT SINK FOR DIFFERENT COMPOSITE MATERIALS Meehye Oh P055 EFFECT OF LASER RE-MELTING PROCESS ON THE MICROSTRUCTURE AND MECHANICAL PROPERTIES OF ADDITIVELY MANUFACTURED Jianshen Wang P008 METAL MATRIX COMPOSITES Composites structures INSTRUMENTED IMPACT BEHAVIOR OF PANELS PRODUCED BY ADDITIVE MANUFACTURING Thomas Whitney P009 THERMO-MECHANICAL BEHAVIOUR OF MICROWAVE-CURED CARBON NANOTUBES-BASED POLYMER COMPOSITES Gaurav Arora P056 Advanced manufacturing and automation STIFFENED COMPOSITE PARTS BY RESIN INFUSION PROCESS FOR AIRCRAFT APPLICATION Oyoung Choi P057 EFFECTS OF CURE CYCLE PRESSURE PROFILE AND HEATING RATE ON PROPERTIES OF OUT-OF-AUTOCLAVE RAPIDLY CURED CARBON Sima Kashi P010 TTT CURE DIAGRAM FOR AN AMBIENT TEMPERATURE CURING EPOXY-AMINE THERMOSET Wannakuwattewaduge P058 FIBRE COMPOSITES Minolie Shanelle Fernando HIGLY AUTOMATED MANUFACTURING PROCESS OF LARGE AIRPLANE CFRP STRCTURES Marcin Malecha P011 DETERMINATION OF MODE II INTERLAMINAR FRACTURE TOUGHNESS ENHANCEMENT OF UNIDIRECTIONAL CARBON FIBER-REINFORCED Nongyue Gao P059 MATRIX COMPOSITES WITH GRAPHENE AND MULTI-WALLED CARBON NANOTUBES CONTINUOUS TAPE LAYUP MOLDING BEHAVIOR OF CFRTP USING NEAR-INFRARED HEATING AND INDUCTION HEATING Naoki Nakata P012 A TRISTABLE CROSS-SHAPED UNSYMMETRIC FIBER-REINFORCED CROSS-PLY LAMINATES: EXPERIMENTAL AND SIMULATION METHODS Yang Li P060 IMPREGNATION PROCESS IN OPEN MOLDING METHOD USING MULTI-FILAMENT WINDING Kazuma Otake P013 THE ENERGY-ABSORBING CHARACTERISTICS OF COMPOSITE TUBE-REINFORCED ALUMINUM FOAMS UNDER COMPRESSION Zheng Liu P061 Aerospace A NUMERICAL MODEL FOR COUPLING HYGRO-MECHANICAL PHENOMENA IN COMPOSITE MATERIALS Mamadou Abdoul P062 MODE I FRACTURE TOUGHNESS OF 3D COMPOSITES REINFORCED WITH METAL OR CARBON Z-BINDERS Sadaf Abbasi P014 MBACKE WARPAGE BEHAVIOUR OF DISCONTINUOUS CF/PEEK THIN PLATES Natassia Batista P015 STUDY ON THE PROPERTY OF LIGHTWEIGHT BUILDING STRUCTURE Comfort Mensah P063 EXPERIMENTAL STUDY ON INTER-YARN FRICTION CHARACTERISTICS OF STF-KEVLAR FABRICS WITH DIFFERENT MASS CONCENTRATIONS Wei Chen P016 NONLINEAR FINITE ELEMENT ANALYSIS OF COMPOSITE BOLTED LAP-JOINTS : EXPERIMENTAL VS . NUMERICAL TESTS Benoit Montagne P064 CF/MODIFIED-PEEK COMPOSITES FOR AIRCRAFT Takahiro Hayashi P017 EXPERIMENTAL VALIDATION OF A COMPOSITE BEAM SUB-STRUCTURAL TEST SPECIMEN Alex Quinlan P065 EFFECTS OF PROCESS CONDITIONS ON AEROSPACE GRADE EPOXY/CARBON FIBRE COMPOSITE PROPERTIES Matt Jennings P018 NOVEL FILLER MATERIALS FOR SKIN-STIFFENER STRUCTURES Zsombor Sápi P066 OBTENTION OF A CARBON-CARBON COMPOSITE MATERIAL FOR ITS USE IN EXPANDING NOZZLES FOR AEROSPACE VEHICLES Liliana Maricarmen Lopez P019 MICRO-MECHANICAL FAILURE ANALYSIS OF A UNI-DIRECTIONAL COMPOSITE PLY – COHSEIVE ELEMENTS & A DUCTILE FRACTURE Akash Sharma P067 QUANTIFYING AND MINIMISING THE EFFECTS OF THE ROOT CONDITION OF DRUM DEPLOYED COMPOSITE TUBULAR BOOMS FOR Jason Shore P020 APPROACH SPACECRAFT EFFECT OF LAYING METHOD ON MECHANICAL PROPERTIES OF CONTINUOUS GLASS FIBER REINFORCED POLYPROPYLENE SANDWICH Yiliang Sun P068 MINIMIZATION OF THE OUT-OF-PLANE THERMAL DEFORMATION OF CFRP REFLECTORS BY STACKING SEQUENCE OPTIMIZATION Shun Tanaka P021 PANELS VIBRATION FREQUENCY DESIGN AND STUDY OF COMPOSITE FUSELAGE STRUCTURE Kaijian Wang P022 KINKING MECHANICS IN COMPOSITES UNDER COMBINED LOADING Sachin Vankar P069 DESIGN AND ANALYSIS OF FILAMENT-WOUND COMPOSITE PRESSURE VESSELS BASED ON MESH WINDING THEORY Hui Xu P023 EFFECT OF INTERFACE LAYER AND DISLOCATION ON TANDEM HONEYCOMB MECHANICAL PROPERTY Hangjian Weng P070 A COMPUTATIONALLY EFFICIENT APPROACH FOR ANALYSING THE ONSET OF FAILURE IN AEROSPACE COMPOSITE STRUCTURES Shibo Yan P024 INVESTIGATION INTO 3D PRINTING OF CFRP USING COVERING COMPOSITE YARN Takato Yoshizawa P071 Automated fibre placement QUASI STATIC COMPRESSIVE RESPONSE OF CFRP HONEYCOMB CORE WITH FOAM FILLERS Hao Zhou P072 SCALED BOUNDARY FINITE ELEMENT BASED METHOD FOR CRACK INITIATION AND PROPAGATION IN FIBER REINFORCED COMPOSITE Nikhil Garg P025 Computational and finite element methods STRUCTURES. POTENTIAL APPLICATION OF WIRE WOVEN MESH AS PACKING TOWER BED LIMITER-COMPUTATIONAL APPROACH Vahid Ebrahiminejad P073 INTRA-LAMINAR AND INTER-LAMINAR PROGRESSIVE FAILURE ANALYSIS OF AFP COMPOSITE ON A TOW LEVEL Xie Li P026 FINITE ELEMENT ANALYSIS AND EXPERIMENTAL TESTING OF NON-CRIMP FABRIC COMPACT TENSION SPECIMENS – INFLUENCE OF Dimitris Gouskos P074 PEFORMANCE MONITOR AND PREDICTION OF A BIAXIALLY LOADED THIN COMPOSITE TUBE Md Shamsuddoha P027 COHESIVE PROPERTIES. TOOLPATH STRATEGY & GENERATION FOR ROBOTIC FIBRE PLACEMENT ON CURVED SURFACES Nahaad Vaheed P028 MICROMECHANICS MODELING OF TENSILE/SHEAR BEHAVIOR AND CRACK DENSITY OF COMPOSITE MATERIALS Daichi Haruyama P075 SIMULATION AND TEST VERIFICATION OF PREPREG PEEL FOR PLACEMENT PROCESS Xianzhao Xia P029 APPLICATION OF A VARIABLE-KINEMATICS CONTINUUM SHELL ELEMENT TO THE ADAPTIVE NONLINEAR ANALYSIS OF COMPLEX SHELL Aewis K.W. Hii P076 STRUCTURES Automotive MECHANICAL BEHAVIOR OF TEXTILE COMPOSITES USING A TWO-STEP HOMOGENIZATION TECHNIQUE Chaeyoung Hong P077 SIMULATION AND EXPERIMENTS FOR MECHANICAL PROPERTIES DOMINATING THE PRESS MOLDING USING CFRTP PREFORMS Yuji Abo P030 BUCKLING ANALYSIS OF MULTILAYERED BEAMS WITH SOFT AND RIGID INTERFACES An Le P078 CHARACTERIZATION OF UNDAMAGED AND DAMAGED CARBON FIBER COMPOSITES IN ELECTROMAGNETIC FIELDS FOR INDUCTIVE Tobias Mayr P031 CHARGING OF ELECTRIC VEHICLES CARBON FIBRE PROSTHETIC FOOT: DESIGN AND MANUFACTURING PROCESS Chao Liu P079 DEVELOPMENT OF BENDING PROCESS FOR THERMOPLASTIC COMPOSITE PIPE DURING PULTRUSION MOLDING PROCESS Asami Nakai P032 MATERIAL DESIGN SIMULATION FOR FIBER REINFORCED CEMENT-BASED COMPOSITES USING MESO-SCALE ANLYSIS Hiroki Ogura P080 PRESS AND INJECTION HYBRID MOLDING OF GF/PP HAT-SHAPED MEMBER AND EVALUATION OF ITS BENDING PROPERTY Kazuto Tanaka P033 DYNAMIC STRESS–STRAIN RELATION OF ALUMINUM POWDERS USING MULTI-PARTICLE FINITE ELEMENT METHOD Kefeng Peng P081 DESIGN AND ANALYSIS OF COMPOSITE CARBON FIBER REINFORCED ANTI-COLLISION BEAM BASED ON ANSYS ACP Chuanxiang Zheng P034 DESIGN OF 70MPA COMPOSITE HYDROGEN STORAGE VESSEL Cheng Shuo P082 Bio-composites TOWARDS UNDERSTANDING AND MODELING IRREVERSIBLE BEHAVIOR OF WOVEN FABRICS UNDER LOADING-UNLOADING BENDING Reza Sourki P083 REGIMES FACTORIAL STUDY OF MATERIAL AND PROCESS PARAMETERS ON FIRE AND MECHANICAL PROPERTIES OF WOOL AND WHEAT GLUTEN Nam Kyeun Kim P035 COMPOSITES SIZE-EFFECT DETERMINATION OF THE MODE I INTRALAMINAR FRACTURE TOUGHNESS USING COMPUTATIONAL MICROMECHANICS Luis Varandas P084 BAMBOO BASED BIO-COMPOSITES UNDER DAMAGED AND UNDAMAGED FRACTURE Wen Liu P036 A MICROMECHANICAL MODEL IN CYCLIC PLASTICITY FOR FIBER REINFORCED WAVY COMPOSITES Danhui Yang P085 ADVANCED QUALIFICATION OF COMBOO - A BAMBOO BASED CORE MATERIAL Andreas Loth P037 CHARACTERIZATION AND THERMAL EFFECT ON MECHANICAL PROPERTIES OF BIOMATERIAL-REINFORCED-POLYPROPYLENE Anh Dung Ngo P038 MULTILEVEL RESISTIVE SWITCHING IN NANO SILVER INCORPORATED CHITOSAN THIN FILMS Sreedevi Vallabhapurapu P039 Bio-inspired composites DESIGN AND CONSTRUCTION OF BIO-INSPIRED SMART MATERIALS WITH REVERSIBLE ADHESION Ying Chu P040 PREPARATION AND ELECTRICAL CHARACTERIZATIONS OF MAN-MADE NACRE-LIKE COMPOSITES Yingbang Yao P041 BONE TISSUE SCAFFOLD BASED ON SHAPE MEMORY POLYMER Wei Zhao P042 Biomedical DIC ANALYSIS OF SHRINKAGE BEHAVIORS OF DENTAL COMPOSITES DURING DENTAL RESTORATION Nak-sam Choi P043 IN VITRO STUDY OF A NOVEL BIOFUNCTIONALIZATION FOR 3D PDMS SCAFFOLD VIA SURFACE MODIFICATION Baek Ji Hun P044 CARBON DOT/POLYPYRROLE NANOPARTICLE COMPLEXES AS MULTIFUNCTIONAL THERANOSTIC AGENTS Tae Eun Kim P045 CARBON QUANTUM DOTS USING POLYPHENOL COMPOUNDS:SKIN ANTI-AGING SeokWon Park P046 Ceramic matrix composites OXIDATION AND INDENTATION RESISTANCE OF CARBON-CARBON COMPOSITE BY SILICON CARBIDE COATING Kee Sung Lee P047 HIGH-TEMPERATURE THERMAL AND MECHANICAL PROPERTIES OF AEROGEL/FIBROUS ZIRCONIA CERAMIC COMPOSITES Jingjing Sun P048 SIC/SIC COMPOSITES FABRICATED BY ELECTROPHORETIC DEPOSITION COMBINED WITH POLYMER INFILTRATION AND PYROLYSIS Honglei Wang P049 PROCESS POSTER PROGRAM POSTER 99 P071 P091 P081 P061 P074 P077 P097 P087 P072 P073 P075 P067 P076 P078 P079 P057 P092 P070 P093 P095 P099 P094 P096 P082 P098 P062 P085 P089 P083 P086 P088 P084 P090 P069 P063 P059 P055 P064 P080 P068 P065 P066 P054 P056 P058 P060 Poster no Poster Feng Huang Seung Goo Lee Theminimulla Sithila Yadav Ramdayal Yadav Ramdayal Pooneh H.M Attar H.M Pooneh Yuyan Yu Yuyan Challagulla Krishna Marzena Pawlik Marzena Striewe Jan Unnikrishnan Vishnu Hisaki Matsuda Hisaki Ran Li Feng Li Félix Lessard Isa Emami Tabrizi Emami Isa Farzaneh Hassani Sneha Bhushan Cheryala Bhushan Sneha Natee Srisawat AhmedSohail Alex Osei Bonsu Cao Wenxin Nae-man Park Nae-man Hee Park Yoon Bich Nam Jung Bich Nam Nagammanavar Uday Paglicawan Marissa Sabu John Farzin Javanshour Rupam Gogoi Rupam He Hailing Laurent BizetLaurent Yangbo Zhang Yangbo Tao Zhang Tao Donghyun Yoon Donghyun Hongjun Yu Ma Yifan Ma Daniel Rapking Min’ge Duan Min’ge Fikry Mohammad M.j. Sangdeok Kim Min-Seok ChoiMin-Seok Dominik Banat Briand Tanguy Giuseppe Catalanotti Presenter name Presenter Keith Ballard PROGRESS IN STRUCTURAL TAILORED POLYMER INSERTS; TRENDS AND STRATEGIES TOWARDS FUNCTIONAL POLYMERIC INTER-PLY INTER-PLY FUNCTIONAL POLYMERIC TOWARDS INSERTS; TRENDS AND STRATEGIES POLYMER PROGRESS IN STRUCTURAL TAILORED REINFORCEMENTS CARBON FIBRE FROM VICTORIAN LIGNITE MULTIFUNCTIONAL STRUCTURAL COMPOSITES ENERGY STORAGE MULTIFUNCTIONAL PROCESSING HIGH BY SHEAR RATE COMPOSITE MATERIALS OF THE PVDF/PAR PREPARATION composites Hybrid FIBER REINFORCED HYBRID EPOXY COMPOSITESBASALT COMPRESSION PROPERTIES OF MULTIFUNCTIONAL CFRP LAMINATES WITH EMBEDDED LITHIUM-ION POLYMER BATTERIES WITH EMBEDDED CFRP LITHIUM-ION LAMINATES POLYMER COMPRESSION PROPERTIES OF MULTIFUNCTIONAL TEMPERATURE SENSOR BASED ON PHASE TRANSITION FORTEMPERATURE ALARM SYSTEM Power and Structural Computation Sensing, Actuation, for Composites on Multifunctional Forum Interdisciplinary PIEZOELECTRIC COMPOSITESELECTROMECHANICAL RESPONSE OF MULTIFUNCTIONAL HOW THE SPRAYING OF GRAPHENE CHANGES MECHANICAL NANOPLATELETS PROPERTIESHOW THE OF CARBON FIBRE SPRAYING REINFORCED POLYMER? CFRP-STEEL HYBRIDS WITH IMPROVED AGEING RESISTANCE THROUGH OF BASIC MECHANISMS HYBRIDS ZINC WITH IMPROVED OXIDECFRP-STEEL NANORODS - INVESTIGATION AGEING RESISTANCE NANOCOMPOSITES GRAPHENE-MOF. USING POLYMER HYRID MULTIFUNCTIONAL EFFECT OF ARAMID ON CARBON/ARAMID FIBER FIBER CLOTH REINFORCED THERMOPLASTICS GAMMA-RAY SHIELDING PROPERTY OF TUNGSTEN/BASALT FIBER REINFORCED EPOXY MATRIX COMPOSITES FABRICATED BY TWO BY SHIELDING COMPOSITES FIBER PROPERTY REINFORCED FABRICATED EPOXYGAMMA-RAY MATRIX OF TUNGSTEN/BASALT TUNGSTEN HYBRID WAYS HYBRID NANOCOMPOSITE OF ZIF-67 AND COBALT-NICKEL LAYERED DOUBLE HYDROXIDE AS ELECTROCATALYST FOR HIGHLY EFFICIENT FOR HIGHLY DOUBLE HYDROXIDE AS ELECTROCATALYST LAYERED HYBRID NANOCOMPOSITE OF ZIF-67 AND COBALT-NICKEL EVOLUTION REACTIONOXYGEN IMPACT OF CELLULOSE FILAMENTS CELLULOSE OF ON INTERLAMINARIMPACT PROPERTIES, FLAMMABILITY OF BEHAVIOUR AND THERMAL DEGRADATION COMPOSITES MATRIX POLYMER PROPERTIES AND FAILURE PREDICTION OF INTERPLY HYBRID COMPOSITES OF GLASS PREDICTION OF INTERPLY AND SELFREINFORCEDPROPERTIES AND FAILURE POLYPROPYLENE INVESTIGATION OF DAMAGE ACCUMULATION IN GLASS/CARBON ACCUMULATION OF DAMAGE FIBER HYBRIDINVESTIGATION COMPOSITES THROUGH EMISSION METHOD ACOUSTIC EFFECT OF FIBER RESPONSE DISTRIBUTION OF HYBRID ON COMBINED COMPOSITES COMPRESSION-TORSIONAL ROBUST AND CONDUCTIVEROBUST HYDROGEL BASED ON CARBON NANOTUBE/ARAMID NANOFIBER FOR STRUCTURAL STORAGE ENERGY TUBE MADE FROM POLYLACTIC ACID YARN AND SILK YARN BY FILAMENT BY WINDING AND TECHNIQUE SILK YARN ACID YARN TUBE MADE FROM POLYLACTIC composites Hybrid ON THE COMPRESSION RESPONSE OF HYBRID 3D ORTHOGONAL WOVEN COMPOSITES OF HYBRID SANDWICH AND COMPOSITES BEHAVIOR CAI IMPACT OF LOW-VELOCITY INVESTIGATION ONE-STEP EXTRACTION OF CELLULOSE NANOCRYSTALS ONLY USING HIGH-PRESSURE HOMOGENIZER HIGH-PRESSURE USING ONLY EXTRACTIONONE-STEP NANOCRYSTALS OF CELLULOSE RESEARCH ON COMBUSTION BEHAVIOR OF HYBRIDRESEARCH COMPOSITE FIRE BEHAVIOR BY ON COMBUSTION DYNAMICSSIMULATOR EVALUATION OF TENSILE PROPERTIES AND WATER ABSORPTION FIBER OF ABACA THERMOPLASTIC FIBER TO COMPOSITE RELATIVE OF TENSILE PROPERTIES AND WATER EVALUATION AND ADDITIVES TYPELENGTH, OF MATRIX THE FABRICATION OF POLYLACTIC ACID (PLA) / CELLULOSE NANOFIBER (CNF) ACID (PLA) / CELLULOSE NANOCOMPOSITES OF POLYLACTIC WITH PLASTICIZER AS DISPERSING THE FABRICATION AGENT OF THE FUTURE COMPOSITES FROM BAMBOO-A MATERIAL FIBRE PANEL GREEN AND NATURAL WASTE-DERIVED NANOCELLULOSE-CHITIN HYBRID MATERIALS WITH TUNABLE PROPERTIES PHYSICAL HYBRID MATERIALS NANOCELLULOSE-CHITIN WASTE-DERIVED THERMAL AND MECHANICAL BEHAVIOUR OF FLAX YARNS MODIFIED WITHTHERMAL GRAPHENE OF FLAX AND MECHANICAL OXIDE BEHAVIOUR YARNS NATURAL FIBRE BASED HYBRID POLYPROPYLENE COMPOSITES: AN INSIGHT FIBRE THERMAL INTO BASED HYBRID PROPERTIES POLYPROPYLENE NATURAL AND JUTE ON STRENGTHENING FIBER REINFORCED AND TOUGHENINGTHE EFFECT OF POLYLACTIDE OF CORE-SHELL NANOPARTICLES COMPOSITE POLYLACTIDE Green & natural fibe composites & natural Green AND MECHANICAL CHARACTERISTICSELABORATION OF FLAX-PCL COMPOSITES AND SANDWICHES MICRO-CRACK STUDY OF MULTICRYSTALLINE SILICON SOLAR PANEL BASED ON IN-SITU SILICON SOLAR EXPERIMENT PANEL MICRO-CRACK STUDY OF MULTICRYSTALLINE INTERLAMINAR PROPERTIES OF CONTINUOUS FIBER REINFORCED THERMOPLASTIC COMPOSITES WITH DIFFERENT RESIN FRACTION EVOLUTION OF FRACTURE OF A CRACK IN PARAMETERS A MICROPOLAR ELASTICSOLID DEVELOPMENT OF PROGRESSIVE FAILURE ANALYSIS METHOD FOR COMPOSITE LAMINATES CONTAINING OPENINGS WITH DIGITAL IMAGE METHOD OPENINGS WITH FOR DIGITAL COMPOSITE CONTAINING LAMINATES ANALYSIS DEVELOPMENT OF PROGRESSIVE FAILURE CORRELATION DUCTILE-BRITTLE FRACTURE IN-SITU OF TIB2/AL COMPOSITE SIMULATION DAMAGE PROGRESSION OF NOTCHED AND UNNOTCHED COMPOSITE UNDER AND PROGRESSION UNNOTCHED PICTURE-FRAMEDAMAGE OF NOTCHED LAMINATES SHEAR LOADING FRACTURE MECHANISM AND PREDICTION STRENGTH OF IN-SITU TIB2/AL COMPOSITE IMAGE CORRLELATION REINFORCEDFRACTURE COMPOSITES DIGITAL USING CHARACTERISTICS PARTICULATE OF DIC DEFORMATION MEASUREMENT IN CRACKED CFRP CROSS-PLY LAMINATES MEASUREMENT IN CRACKEDDIC DEFORMATION CFRP CROSS-PLY EFFECT DEGRADED OF CARBON NANOTUBE CONTENTS NANOCOMPOSITE ON FRACTURE VIA FILMS THE PROPERTIES OF THERMALLY ESSENTIAL WORK OF FRACTURE TEST COMPARATIVE DAMAGE ANALYSIS OF VARIOUS OPEN CROSS-SECTION OPEN GLARE COMPOSITE OF VARIOUS COLUMNS ANALYSIS DAMAGE COMPARATIVE SIZE EFFECT AND INTRALAMINAR FRACTURE TOUGHNESS OF FIBRE REINFORCED COMPOSITES EFFECT OF PLY THICKNESS ON TRANSVERSE CRACKING AND TEMPERATURE PROCESS IN COMPOSITEEFFECT OF PLY LAMINATES TUESDAY 13 AUGUST POSTER SESSION TUESDAY title Poster and damage Fracture A PRELIMINARY ASSESSMENT OF A NEW XFEM FRAMEWORK FOR PREDICTING COMPLEX FRACTURE P011 P017 P051 P041 P031 P021 P013 P012 P018 P019 P014 P015 P016 P010 P001 P037 P047 P027 P052 P032 P024 P053 P042 P025 P039 P023 P033 P035 P038 P007 P022 P036 P029 P026 P034 P049 P028 P043 P045 P050 P046 P048 P030 P044 P020 P040 P002 P003 P009 P005 P006 P004 P008 Poster no Poster Avinash Baji Avinash Chenxi Yang Dan Xing Hyun Ju Oh Ju Hyun HyunSeok Jung HyunSeok Khan Huma Liu Fang Shanghong Duan Shanghong Shipeng Wen Eduard Relea Eduard Ran Liu Aakash Moncy Marc Möller Marc Sebastian Backe Sebastian Li Yanqi Lei Zu Lei Sailong Xu Tao Wen Tao Koranat Pattarakunnan Koranat Junki Nakano Junki Keisuke Nagayoshi Keisuke Xiaoyu Guan Lee Won Jae Yu Fu Xiaojun Yan Sanghyun Yoo Sanghyun Dai Fuhong Jian Yu Jian Wataru SUGIMOTO Wataru Ming LiMing Taeseong Choi Taeseong ChoudhurySantanu Junhong Chen Junhong OKOSHI MASAYUKI OKOSHI King Jye Wong Jinqiao Jiang Jinqiao Takeharu Isaki Takeharu Pablo Chávez Gómez Chávez Pablo Peng Li Peng Puneet Garg Puneet Jeongho ChoiJeongho Fan Yang Fan Greg Beziuk Long Nguyen Meredith Mahoney Meredith Yuequan Wang Yuequan Liling He Florian Schimmer Florian Satoshi Tomita Satoshi Pu Jie Hui Jin Um Jin Hui Yeh Fang-Yao Jim Kingston Jim Presenter name Presenter SIC FIBER WITH DIFFERENT TEMPERATURE IN SIC FIBER AIR AND WITH ARGON DIFFERENT ATMOSPHERE TEMPERATURE OIL-WATER SEPARATION USING JANUS MEMBRANES JANUS USING SEPARATION OIL-WATER PROPERTIES AND STRUCTURAL PERFORMANCE OF KD-Ⅱ FACTORS GOVERNING THE TENSILE STRENGTH OF BASALT FIBRE GOVERNING THE OF BASALT TENSILE STRENGTH FACTORS MANUFACTURE OF THE PLLA/BATIO3 FIBER FOR PIEZOELECTRIC FIBROUS SENSORS OF THE PLLA/BATIO3 MANUFACTURE A STUDY OF GF/PA6 FIBER REINFORCED COMPOSITES MATERIALS USING PULTRUSION AND DIRECT EXTRUSION METHOD FIBER PULTRUSION REINFORCED USING COMPOSITESA STUDY OF GF/PA6 MATERIALS PRECURSOR FIBRE HIGH POLYACRYLONITRILE STRENGTH LOW-COST, FOR MEASUREMENT TRANSVERSE OF CARBON MODULUS FIBRES ION BEAM FOCUSED USING SPECIMEN PREPARATION Fibers FORCE MICROSCOPE AND MEASUREMENT NANOINDENTATION TRANSVERSE YOUNG’S OF CARBON MODULUS FIBRE ATOMIC BY ENHANCED FATIGUE PROPERTIES OF GRAPHENE RUBBER OXIDE/CARBON COMPOSITES BLACK/NATURE ENHANCED FATIGUE CONTROLLED STRAIN RESONANCE FREQUENCY FATIGUE TEST BENCH FOR CFRP CONTROLLED STRAIN RESONANCE FREQUENCY FATIGUE FATIGUE LIFE ANALYSIS FOR WIND TURBINE GEAR SHAFT LIFE ANALYSIS WITH OXIDE INCLUSION FATIGUE CRUCIFORM TESTING SPECIMEN IN COMPOSITES DESIGNS FOR PLANAR BIAXIAL FATIGUE INVESTIGATION ON HOMOTHETIC FAILURE ENVELOPES IN THE LAYER-BASED FATIGUE ANALYSIS OF CFRP ANALYSIS FATIGUE IN THE LAYER-BASED ENVELOPES ON HOMOTHETIC FAILURE INVESTIGATION Fatigue COMPOSITES OF MULTIFUNCTIONAL LIFE ESTIMATION FOR FATIGUE APPROACH SHORT-TIME LAMINATE OF HYBRID BI-STABLE BEHAVIOR A CREEP MODEL FOR THE FATIGUE DESIGN AND PRODUCTION OF FILAMENT ROTORS WOUND SLEEVES FOR HIGH FLYWHEEL SPEED SULFIDE COMPOSITE WITH A LARGE SPECIFIC SURFACE AREA FOR HIGH-PERFORMANCE ALL-SOLID-STATE PSEUDOCAPACITORS COMPOSITESULFIDE AREA WITH A LARGE FOR HIGH-PERFORMANCE ALL-SOLID-STATE SPECIFIC SURFACE VIBRATIONAL ENERGY HARVESTING OF MULTIFUNCTIONAL COMPOSITE BLADE ENERGY HARVESTING FOR OF MULTIFUNCTIONAL OFFSHORE WINDVIBRATIONAL TURBINE A REVIEW OF MULTIFUNCTIONAL COMPOSITEA REVIEW STRUCTURES WITH OF MULTIFUNCTIONAL EMBEDDED LITHIUM-ION BATTERIES DEVELOPMENT OF SIC NANO-PARTICLE/MG2SI THERMOELECTRIC COMPOSITESDEVELOPMENT OF SIC NANO-PARTICLE/MG2SI THE EFFECT OF VIBRATION ON MECHANICAL,THE EFFECT OF VIBRATION AND ELECTRICAL PROPERTIES OF MAGNESIUM SILICIDE BASED THERMOELECTRIC MODULES MULTIFUNCTIONAL COMPOSITES FOR HARVESTING ENERGY MULTIFUNCTIONAL FOR HIGH-PERFORMANCE SUPERCAPACITORS NANOSHEET IRON SULFIDE ARRAYS COBALT ORGANIC FRAMEWORK DERIVED ULTRA-THIN CARBON FIBERS ORGANIC MODIFIED FRAMWORK WITH METAL NANOSHEETS: AS ELECTRODE FOR USE POTENTIAL STRUCTURAL BATTERIES NUMERICAL SIMULATION OF HAIL IMPACT CHARACTERISTICS OF GLASS OF HAILNUMERICAL IMPACT SIMULATION FIBER LAMINATES IMPROVING THE DYNAMIC MATERIAL CHARACTERISATION OF CARBON/EPOXY COMPOSITES AT INTERMEDIATE STRAIN RATES INTERMEDIATE OF CARBON/EPOXY COMPOSITES AT CHARACTERISATION IMPROVING THE MATERIAL DYNAMIC and storage harvesting Energy PIEZOELECTRIC FOR COMPOSITE ENERGY HARVESTING LAMINATE BI-STABLE RESEARCH BASED ON THE ON PERIDYNAMICS TENSILE OF GFRP DYNAMIC LAMINATES MODE II INTERLAMINAR OF ZANCHOR FRACTURE REINFORCED IMPACT BEHAVIOR COMPOSITE UNDER LOW-VELOCITY LAMINATES LOADING NATURAL FREQUENCY OF BI-STABLE COMPOSITE PLATES IN THERMAL COMPOSITE ENVIRONMENTS PLATES FREQUENCY OF BI-STABLE NATURAL RATE DEPENDENT TENSILE RESPONSE OF A PLAIN TEXTILE WEAVE RATE COMPOSITE ON SHEAR OF COMPOSITES STRENGTH PLUGGING STRAIN RATES EFFECT OF INTERMEDIATE Dynamic properties & fracture OF THE TUNGSTEN GLASS FIBER BEHAVIORS REINFORCED METALLIC BULK ON THE DEFORMATION DYNAMIC EFFECT OF TEMPERATURE COMPOSITE COMBUSTION OF CARBON FIBERCOMBUSTION REINFORCED PLASTICS AN EXTENDED THICKNESS-DEPENDENT MOISTURE ABSORPTION MODEL FOR UNIDIRECTIONAL CARBON/EPOXY COMPOSITES AN ATOMISTIC STUDY OF CREEP DEFORMATION IN FIBER/MATRIX INTERFACE IN FIBER/MATRIX STUDY OF CREEP DEFORMATION AN ATOMISTIC STATISTICAL LIFE PREDICTION OF UNIDIRECTIONAL CF/PP TAPE UNDER CREEP LIFE PREDICTION TENSION LOAD OF UNIDIRECTIONAL CF/PP TAPE STATISTICAL Durability, creep and aggressive environment creep and aggressive Durability, FUEL EFFECT ON THE EVOLUTION TENSILE OF CARBON STRENGTH FIBERS UNDER DIRECT FLAME ATTACK DESIGN OF FIBER PREFORMS FOR WORLD’S LARGEST FIBERGLASS COMPANY SUPERHYDROPHOBIC COATINGS FOR ENHANCED FIBRE COMPOSITE COATINGS MATERIALS SUPERHYDROPHOBIC MECHANICAL PRINTING 3D BY PROPERTY TECHNIQUE CUBIC MODEL CREATED OF A CORE-FILLED ANALYTICAL AND EXPERIMENTAL STUDY ON HIGH-TEMPERATURE HIGH-VELOCITY IMPACT LIMIT FOR C/C COMPOSITE HIGH-VELOCITY IMPACT AND EXPERIMENTAL STUDY ON HIGH-TEMPERATURE ANALYTICAL Design and manufacture for multifunctionality for and manufacture Design MATERIALS ELECTRONIC CIRCUITS EMBEDDED COMPOSITE INTO AEROSPACE THE DEFORMATION AND FAILURE RESPONSE OF ULTRA-HIGH MOLECULAR WEIGHT POLYETHYLENE COMPOSITE TO LOCALIZED BLAST COMPOSITE LOCALIZED MOLECULAR TO WEIGHT POLYETHYLENE RESPONSE OF ULTRA-HIGH AND FAILURE THE DEFORMATION LOADING COMPUTATIONAL MULTISCALE MODELLING OF CERAMIC MATERIALS FOR DEFENCE NEEDS OF CERAMIC MODELLING MATERIALS MULTISCALE COMPUTATIONAL INFLUENCE OF DENTINFLUENCE DEFECTS ON THECOMPRESSIVE OF COMPOSITE STRENGTH LAMINATES Defence AND WOOD PERFORMANCE MADE OF THIN STEEL PLATES OF SANDWICHEXPERIMENTAL STUDY TARGET ON ANTI-PENETRATION BULLET AGAINST 7.62MM COMPARATIVE STUDY ON THE DAMAGE TOLERANCE OF THERMOSET STUDY TOLERANCE ON THE DAMAGE AND THERMOPLASTIC GLASSCOMPARATIVE FIBER-REINFORCED COMPOSITES Computational and finite element methods element and finite Computational NUMERICAL MODELING FOR MECHANICAL PROPERTIES OF NAMD(TM) CFRP tolerance Damage DETECTION OF CARBON FIBRE FOR COMPOSITE VIBRATION DELAMINATION PLATE MULTI-MODE Composites structures Composites TEMPERATURE THE OF PET INFLUENCE CRYSTALLINITY IN CARBON FIBER REINFORCED VARIOUS PET COMPOSITE AT COMPOSITE TYPESTUDY ON TRUSS STRUCTURE SEGMENTAL FOR TEMPORARY RESCUE BRIDGE Composite Materials: Route to Impact to Route Materials: Composite – THREE FOAMS DIMENSIONAL COMPOSITE NETWORKSAN INTRODUCTION SYNTACTIC TO Poster title Poster TUESDAY 13 AUGUST POSTER SESSION TUESDAY

POSTER PROGRAM 98 WEDNESDAY 14 AUGUST POSTER SESSION WEDNESDAY 14 AUGUST POSTER SESSION Poster title Presenter name Poster no Poster title Presenter name Poster no 100 Computational and finite element methods ACCOUNTING FOR SHEARED TEXTILE COMPOSITE UNIT CELL PROPERTIES IN MACRO SCALE FE SIMULATIONS Meng-yi Song P052 101 A SEMI-ANALYTICAL FINITE ELEMENT METHOD FOR THE ANALYSIS OF FUNCTIONALLY GRADED CIRCULAR PLATES Chih-Ping Wu P001 ANALYSIS OF MICRO/MESO/MACRO TEMPERATURE-DEPENDENT ELASTOVISCOPLASTIC PROPERTIES OF WOVEN COMPOSITES Junpei Tetsuka P053 POSTER PROGRAM POSTER Interfaces and interphases ON THE EXPERIMENTAL VALIDATION OF THE WAVE PROPAGATION MODELLING FOR TWO-DIMENSIONAL PERIODIC TEXTILE COMPOSITES Victor Thierry P054 CHARACTERISATION OF BOND STRENGTH IN OVERMOULDED HIGH-PERFORMANCE THERMOPLASTIC COMPOSITES Robert Gaitzsch P002 MODELLING AN IMPROVED NOL RING TEST USING A REDUCED VOLUME METHOD FOR THE CHARACTERISATION OF COMPOSITE Martinus Putra Widjaja P055 CYLINDERS THERMORHEOLOGICAL CHARACTERIZATION OF INTERFACIAL BONDING ENHANCEMENT OF Doojin Lee P003 BASALT FIBER REINFORCED EPOXY COMPOSITES Nano-composites TUNABLE MICROWAVE DIELECTRIC RESPONSE IN CARBON NANOCOMPOSITES VIA VERTICAL INTERPHASE Faxiang Qin P004 HIGH-EMISSIVITY NANO-COMPOSITE FILM FOR EUV PELLICLE APPLICATIONS IN SEMICONDUCTOR FABRICATION PROCESS Jinho Ahn P056 MODIFICATION OF CARBON FIBRE SURFACES BY SUFEX CLICK CHEMISTRY James Randall P005 EVALUATING THE MICRON LEVEL PHASE DISTRIBUTION IN COMPOSITE STRUCTURES AND ITS EFFECT ON MECHANICAL BEHAVIOR USING Ankita Bisht P057 2D MODULUS MAPPING DIRECTIONAL LAMINATES USING CARBON NANOTUBE INTERFACES Lulu Shen P006

CONDUCTIVE NANOPARTICLE ENHANCEMENTS FOR STRUCTURAL DIELECTRIC CAPACITORS KY Chan P058 POSTER PROGRAM TAILORING INTERFACIAL INTERACTIONS IN FIBER REINFORCED POLYMERIC COMPOSITES BY THE ELECTROSPRAY DEPOSITION OF Murat Tansan P007 WATERBORNE CARBON NANOTUBES NANO-ENABLED MANUFACTURING OF AEROSPACE-GRADE THERMOPLASTIC COMPOSITES Frederick Daso P059 INVESTIGATING WATER AGEING EFFECTS ON THE INTERFACIAL INTEGRITY OF CARBON FIBRE POLYMER COMPOSITES Filip Vuković P008 MULTIFUNCTIONAL COMPOSITES WITH MODIFIED CARBON FIBERS FOR LIGHTNING STRIKE PROTECTION Anchalee Duongthipthewa P060 MUSSEL INSPIRED SURFACE MODIFICATION AND FUNCTIONALIZATION METHOD WITH HIGHLY EFFICIENT AND ENVIRONMENTAL Wencai Wang P009 PHOSPHATE FUNCTIONALIZED GRAPHENE OXIDE AS ADSORBENT FOR THE REMOVAL OF PB(II) FROM AQUEOUS SOLUTION Daniel Gang P061 FRIENDLY LOW PERCOLATION THRESHOLD OF POLYPROPYLENE SPECIALLY DESIGNED GRAPHENE NANOCOMPOSITES Karolina Gaska P062 GRAFTING CARBON NANOTUBES ON CARBON FIBER SURFACE AND ENHANCING THE INTERFACIAL PROPERTIES OF COMPOSITES Shu Xiong P010 FABRICATION AND HYDROPHILIC CHARACTERIZATION OF NANOPARTICLES-FILLED POLYMER COMPOSITES Yuki Hanzawa P063 MOLECULAR SIMULATIONS OF INTERPHASE FORMATION PROCESS OF CARBON FIBER REINFORCED POLYMER COMPOSITES Yingdan Zhu P011 EFFECT OF CARBON NANOTUBES CONTENT ON THE FRACTURE BEHAVIOR OF PP/EPDM/MWCNT BLEND-NANOCOMPOSITES UNDER Mehrdad Khodabandelou P064 Joints DYNAMIC AND QUASI-STATIC LOADING INVESTIGATION OF GEOMETRICAL AND COMPOSITE MATERIAL PARAMETERS FOR TENSION-ABSORBING BOLTED JOINTS Jazib Hassan P012 COBALT COPPER ALLOYS ENCAPSULATED BY MOS2/N-DOPED GRAPHENE NANO-HETEROSTRUCTURES FOR ORR APPLICATION Nam Hoon Kim P065 AUXILIARY JOINING ELEMENT WITH INTEGRATED PIN STRUCTURES FOR MECHANICAL JOINING OF FIBER-REINFORCED PLASTIC/METAL Per Heyser P013 COBALT PHOSPHIDES COATED COPPER OXIDE NANOROD ARRAYS FOR ENHANCED OVERALL WATER SPLITTING Joong Hee Lee P066 COMBINATIONS ELECTROMAGNETIC PROPERTIES OF KH560/RGO@FE3O4/TIO2/PARAFFIN WAX COMPOSITE IN 0.5-18 GHZ FREQUENCY Yuexuan Li P067 MECHANICAL ANALYSIS FOR WELDING TECHNOLOGY OF THERMOSET FRP Masato Honma P014 ANALYSES OF MECHANICAL REINFORCEMENT FOR CELLULOSE NANOFIBERS/CLAY NANOCOMPOSITES USING X-RAY DIFFRACTION Shunichi Mori P068 A STUDY ON THE FATIGUE CHARACTERISTICS OF SINGLE LAP JOINT BETWEEN CARBON FIBER REINFORCED PLASTIC/CARBON STEEL Byunghyun Kang P015 EFFECT OF GRAPHENE NANOPARTICLES AND THEIR FUNCTIONALISATION ON VITRIMER MATRIX Quentin-Arthur Poutrel P069 TENSILE PROPERTIES OF STITCHED 3D-WOVEN-COMPOSITES/TITANIUM SINGLE-LAP JOINT Yi-rong Lu P016 PREPARATION OF FLUOROALKYL END-CAPPED OLIGOMER/MAGNETITE NANOCOMPOSITES – APPLICATION TO WATER/OIL SEPARATION Hideo Sawada P070 AXIAL TENSILE ADHESIVELY BONDED PERFORMANCE OF CFRP WOUND COMPOSITE TUBES UNDER ROOM-TEMPERATURE AND LOW- Haibo Luo P017 USE OF RESOLE SEPIOLITE-PHOSPHATE NANOCOMPOSITE FOR BUILDING FACADES Leila Soufeiani P071 TEMPERATURE CIRCULATION GRAPHENE OXIDE/POLYMER-BASED NANOCOMPOSITE HYDROGEL FOR BIOMEDICAL APPLICATIONS WITH ANTIMICROBIAL PROPERTY Lee Won Chang P072 EVALUATION METHOD OF JOINING STRENGTH OF CFRTP MANUFCTUED BY HYBRID INJECTION MOLDING PROCESS Fumiya Matsumoto P018 NUMERICAL INVESTIGATION ON MECHANICAL PROPERTIES OF POLYMER COMPOSITES REINFORCED WITH MXENE NANOSHEETS Daiva Zeleniakiene P073 NUMERICAL MODELING OF ADHESIVELY BONDED CFRP JOINTS CONSIDERING NON-LINEAR DEFORMATION OF ADHESIVE LAYERS Shunta Mimura P019 POLYIMIDE AEROGELS CROSS-LINKED WITH AMINATED AG NANOWIRES: MECHANICALLY STRONG AND TOUGH Tianyi Zhang P074 THE EFFECTS OF ENVIRONMENTAL CONDITIONS ON THE STRENGTH OF DOUBLE LAP JOINTS Aakash Paul P020 IMPROVING INTERLAMINAR SHEAR STRENGTH OF FIBER REINFORCED EPOXY COMPOSITES LAMINATES BY CARBON NANO-FILLERS Helezi Zhou P075 A STUDY ON THE CHANGE OF ADHESIVE SHEAR STRENGTH OF CARBON STEEL/CARBON FIBER REINFORCED PLASTIC COMPOSITE BY Seung Hak Song P021 SURFACE TREATMENT OF CARBON STEEL INTERFACIAL PROPERTIES OF MXENE/GRAPHENE/POLYMER MATRIX NANOCOMPOSITES Kristina Žukienė P076 DAMAGE IN HYBRID JOINTED GLARE STRUCTURES UNDER THE QUASI-STATIC Peifei Xu P022 Non-destructive evaluation MECHANICAL PROPERTIES OF CFRP SINGLE LAP ADHESIVE JOINT Kotono Yanagisawa P023 THERMOELASTIC ASSESSMENT OF COMPOSITE DELAMINATION BUCKLING Cedric Antolis P077 SILICA DEPOSITION TREATMENT FOR IMPROVING ADHESION PROPERTIES OF ADHESIVE BONDING OR COATING OF AIRCRAFTS Tetsuo Yasuoka P024 AUTOMATED IMAGE ANALYSIS OF ULTRAFAST SYNCHROTRON CT SCANS TO EXPERIMENTALLY CHARACTERISE THE FIBRE BREAK Christian Breite P078 DEVELOPMENT DURING IN-SITU TENSILE TESTS Liquid composites moulding SIMULTANEOUS MULTI-FREQUENCY DIELECTRIC ANALYSIS OF THE POLYMERIZATION PROCESS OF ANIONIC POLYAMIDE 6 Maximilian Eberhardt P079 A TWO PHASES COUPLING FREE AND POROUS FLOW METHOD AT MULTI-SCALES OF LCM PROCESS Arthur Cantarel P025 EARLY PREDICTION OF CRACK DEVELOPMENT USING DIGITAL IMAGE CORRELATION David Jesson P080 NUMERICAL SIMULATION OF RESIN FLOW THROUGH 3D FIBROUS REINFORCEMENT AT MULTISCALE Chaozhong Chen P026 FABRICATION AND CHARACTERIZATION OF DISCONTINUITIES IN AIRCRAFT COMPOSITES AS REFERENCE FLAWS FOR GUIDED WAVE Michael Koerdt P081 PERMEABILITY EVALUATION IN VACUUM-ASSISTED RESIN TRANSFER MOLDING OF CARBON FIBER REINFORCED PLASTICS Fumiya Isono P027 BASED ULTRASONIC TESTING LINKAGE ANALYSIS OF PERMEABILITY AND MECHANICAL EXPERIMENTS FOR CFRP Seonghun Kwak P028 DAMAGE DETECTION IN HONEYCOMB SANDWICH PANELS BY ACTIVE THERMOGRAPHY Sefa Kemal Mandal P082 EFFECT OF WETTABILITY ON IMPREGNATION PROCESS OF VISCOUS FLUID TO WOVEN FIBER BUNDLES Atsuki Mizuno P029 MEASUREMENT OF MOISTURE DIFFUSION COEFFICIENT OF WOOD USING TERAHERTZ WAVE Gyung-hwan Oh P083 A PARAMETRIC FLOW VISUALISATION STUDY OF THE WET COMPRESSION MOULDING PROCESS Balaji Muthuvel P030 INVESTIGATION OF DELAMINATED COMPOSITES BY DIC AND AE METHODS Hliva Viktor P084 EFFECT OF FLAME RETARDANT FILTRATION ON THE FIRE PERFORMANCE OF CARBON FIBRE REINFORCED EPOXY COMPOSITES MADE BY Ákos Pomázi P031 COMPOSITE PROPERTY DETECTION USING “WEAK” FORMULATION BASED LOCAL SPECIFIC STIFFNESS IDENTIFICATION Chao Zhang P085 RESIN TRANSFER MOULDING Polymer matrix materials EVALUATION OF MECHANICAL PROPERTIES FOR CFRTP USING IN SITU-POLYMERIZING THERMOPLASTIC URETHANE RESIN Tsuyoshi Sugita P032 EFFECT OF GRAPHENE AND MWCNTS AND ITS DOSAGE ON MODE I INTERLAMINER FRACTURE TOUGHNESS OF CFRP Shuanghui Cao P086 Machining of composites TAILORED POLYMER NETWORKS BY SEQUENTIAL THIOL-ENE PHOTOPOLYMERIZATION Sergio Cespedes P087 EPI-FLUORESCENT MICROSCOPY OF EDGE TRIMMED CARBON FIBRE REINFORCED POLYMER: AN ALTERNATIVE TO CT-SCANNING Sam Ashworth P033 STRUCTURAL COMPOSITE BATTERIES FOR AUTOMOTIVE APPLICATIONS Jaehoon Choi P088 STUDY ON THE PROCESS AND PROPERTIES OF CARBON NANOTUBE FILM CURING CARBON FIBER COMPOSITES Zhiwei Liu P034 PREPARATION AND CHARACTERIZATION OF MODIFIED POLYVINYL ALCOHOL/SODIUM ALGINATE HYDROGEL Jianle Gong P089 MACHINED SURFACE TOPOGRAPHY ANALYSIS IN ULTRASONIC VIBRATION ASSISTED END GRINDING OF SICP/AL COMPOSITES Wei Zheng P035 THE EFFECTS OF MOISTURE AND TEMPERATURE ON THE FLEXURAL PROPERTIES OF CARBON FIBER PAPER REINFORCED Xiangdong He P090 Meta-composite THERMOPLASTICS/POLYAMIDE 6 INDENTATION RESPONSE OF TOPOLOGICAL LATTICE Xiao-fei Guo P036 PREPARATION AND CHARACTERIZATION OF POLY(1,4 BUTYLENE CARBONATE-CO-TEREPHTHALATE)/ORGANICALLY MODIFIED MGAL Ming-Chen Hsu P091 Metal matrix composites LAYERED DOUBLE HYDROXIDE NANOCOMPOSITES THE MAGNETIC AND ELECTROMAGNETIC PROPERTIES OF FECONISIXAL0.4 HIGH ENTROPY ALLOY POWDERS Yuping Duan P037 PREPARATION AND CHARACTERIZATION OF ALUMINUM OXIDE/ALUMINUM NITIDE AS FILLER OF THERMALLY CONDUCTIVE MATERIALS Gyungsoo Jeon P092 ENHANCING THE MECHANICAL PROPERTIES OF TIB2 REINFORCED MAGNESIUM COMPOSITES USING STIR CASTING METHOD Anbuchezhiyan P038 THE INFLUENCE OF DIFFERENT POWDER IMPREGNATION PROCESSES ON THE PROPERTIES OF L-SHAPED WOVEN FABRIC REINFORCED Hansong Liu P093 Gnanasambandam PEEK COMPOSITES BY HOT STAMP FORMING OPTIMIZING THE MICROSTRUCTURE AND MECHANICAL BEHAVIORS OF IN-SITU TIC-Γ′/NI COMPOSITES BY SUBSEQUENT THERMAL Wenqiang Hu P039 EXPERIMENTAL EVALUATION ON FIBER ROTATION OF THERMOPLASTIC COMPOSITE LAMINATE UNDER TENSILE LOADING Taoye Lu P094 TREATMENT DEFORMATION MECHANISM INVESTIGATION FOR EPOXY BY IN-SITU MECH-ELETRIC COUPLING MEASUREMENT Yinggang Miao P095 WEAR AND MECHANICAL CHARACTERISTICS OF AL-SI/TIB2 COMPOSITES Jimmy Karloopia P040 COMPARISON OF SHORT CARBON AND POLY(P-PHENYLENE-2,6-BENZOBISOXAZOLE) FIBERS ON THE PROPERTIES OF POLYESTER Adam Pearson P096 EFFECT OF TA ADDITION ON MICROSTRUCTURES AND ROOM TEMPERATURE FRACTURE TOUGHNESS OF THE NB-16SI-20TI-5AL Wenyuan Long P041 THERMOPLASTIC ELASTOMERS ULTRAHIGH TEMPERATURE ALLOY PREPARATION AND MECHANICAL PROPERTIES OF METAL FLAKE PARTICLES/RESIN COMPOSITE Yutaro Sako P097 SIMULATION OF THERMAL CONDUCTIVITY FOR TITANIUM BORIDE PARTICLE DISPERSED ALUMINUM COMPOSITES Gen Sasaki P042 LINEAR AND NONLINEAR ELASTIC PROPERTIES OF POLYSTYRENE-BASED NANOCOMPOSITES Irina Semenova P098 EVALUATION OF INTERFACIAL THERMAL RESISTANCE OF AL-ALN PARTICLE DISPERSED COMPOSITES BY USING IMAGE-BASED Kenjiro Sugio P043 ELECTRICAL, THERMAL AND MECHANICAL PROPERTIES OF THERMOPLASTIC ELASTOMER COMPOSITES CONTAINING CARBON FILLERS Rajesh Theravalappil P099 CALCULATION PREPARATION AND CHARACTERIZATION OF ORGANICALLY MODIFIED LAYERED ZINC PHENYLPHOSPHONATE/POLY(1,4-BUTYLENE Li-ying Tseng P100 PREPARATION OF SICNP AND IN-SITU MG2SI HYBRID PARTICULATES REINFORCED AL-CU MATRIX COMPOSITES Shusen Wu P044 CARBONATE-CO-TEREPHTHALATE)S NANOCOMPOSITES A NOVEL W/TIN/TA COMPOUND SHAPED CHARGE LINER ZiZhi Yan P045 HIGH TEMPERATURE COMPRESSION PROPERTIES OF CFF/PPS COMPOSITE LAMINATES FABRICATED BY FILM STACKING TECHNIQUE Shixun Wang P101 STRENGTHENING OF PURE AL MATRIX COMPOSITES BY IN-SITU SYNTHESIZED NANO AL-O NEEDLE PHASE Xinxin Zhu P046 RESEARCH ON WAVES DEFECTS OF TAPE WINDING RESIN MATRIX COMPOSITES Xiaojing Wang P102 Multiscale modelling CHARACTERIZATION AND GAS SENSING PROPERTIES OF GRAPHENE NANORIBBONS/ INDIUM TRIOXIDE / POLYANILINE Ling-hui Xu P103 FINITE STRAIN PARAMETRIC HFGMC PREDICTION OF THE MICROMECHANICAL BEHAVIOR OF COMPOSITE Uri Breiman P047 NANOCOMPOSITES MULTISCALE FAILURE ANALYSIS OF 3D BRAIDED COMPOSITE STRUCTURE BY COUPLING FEM AND FFT METHOD Guodong Fang P048 PHTHALONITRILE MODIFIED MULTI-HYDROXYL PHENOLIC: SYNTHESIS, CURING AND PROPERTIES Shuangshuang Xu P104 DEVELOPMENT OF MULTISCALE DAMAGE PROPAGATION ANALYSIS METHOD FOR WOVEN LAMINATES USING A HOMOGENIZATION Gai Kubo P049 MACROSCOPIC AND MICROSCOPIC PROPERTIES OF FABRIC RUBBER COMPOSITE Xuefeng Yao P105 THEORY PREPARATION AND CHARACTERIZATION OF HIGH STRENGTH AND HIGH OIL RESISTANT FLAME RETARDANT EVA COMPOSITES FOR CABLE Yiyang Zhou P106 OVERALL ELASTOPLASTIC PROPERTY OF PARTICULATE COMPOSITE WITH STRAIN GRADIENT MATRIX Hansong Ma P050 IDENTIFICATION OF THE QUASI-STATIC BEHAVIOR OF A WOVEN COMPOSITE SENSITIVE TO THE ENVIRONMENTAL CONDITIONS USING Patrick Rozycki P051 NUMERICAL HOMOGENIZATION POSTER PROGRAM POSTER 103 P071 P091 P081 P061 P074 P077 P087 P072 P073 P075 P067 P076 P078 P079 P057 P070 P082 P062 P085 P089 P083 P086 P088 P084 P090 P069 P063 P059 P055 P064 P080 P068 P065 P066 P054 P056 P058 P060 Poster no Poster Manoj Kumar Singh Kumar Manoj Yu Mingming Hu Xunxun Ameya Kaore Chanchira Jubsilp Chanchira Shigenori Inoue Shigenori Yunchao Qi Yunchao Xiaoran Zhao Xiaoran Park Geon Tae Congyuan Tao Jae-chul Lee Liang shuangqiang Peerzada Mazhar Sugiyama Kazushi Jacob Hoffer Jacob Ingle Sagar Tamas Rev Tamas Röper Florian Shipeng Zhu Ashok Rajpurohit Atsumi Ohtsuki Atsumi Tomas Chuaqui Tomas Eiichi Hara Holger BuettemeyerHolger Guangming Yang Helena Rocha Helena Yang He Yang PhilibertMarilyne Olga Bulderberga Olga Salem Bashmal Zhenyu Ma Sirisobrana Pongpat Andrey Aniskevich Masaki KameyamaMasaki Guokai Han Hefft Lars Thorsten Hung Shih-Lin Presenter name Presenter Furuta Yasuyuki TRIBOLOGICAL CHARACTERISTICS OF MICROWAVE PROCESSED KENAF/HDPE COMPOSITES CHARACTERISTICSTRIBOLOGICAL UNDER DRY SLIDING OF MICROWAVE WEAR THE INFLUENCE OF FABRIC ON THE WEAR-RESISTING PROPERTY OF SELF-LUBRICATING COMPOSITS ON THE WEAR-RESISTING PROPERTYTHE OF FABRIC INFLUENCE OF SELF-LUBRICATING COATINGS MULLITE/LU2SI2O7-LU2SIO5 MECHANISM OF PLASMA AND SPRAYED FAILURE CORROSION BEHAVIOR VAPOR WATER FATIGUE LIFE PREDICTION OF EPOXY COATING ON COMPOSITES SUBJECTED TO WATERDROP IMPACT WATERDROP ON COMPOSITES TO SUBJECTED LIFE PREDICTION OF EPOXY COATING FATIGUE NON-ASBESTOS POLYBENZOXAZINE COMPOSITES: FRICTION AND MECHANICAL POLYBENZOXAZINE PROPERTYNON-ASBESTOS Tribology and wear Tribology CARBON FIBER AND REINFORCED PITCH-BASED PLASTICSWEAR PROPERTIES OF PAN- WITH SIC-NANOPARTICLES THE OPTIMIZATION OF PROCESS PARAMETERS OF THREE-DIMENSIONAL OF PROCESS NEEDLED COMPOSITES PARAMETERS THE OPTIMIZATION BASED ANN ON AND GA Three-dimensional composites ANDSTUDY ANALYSIS STRENGTH ON CFRP PARAMETRIC PI-BEAM EFFECT OF TACKIFICATION ON IN-PLANE OF BIAXIAL SHEAR IN BIAS BEHAVIOURS EXTENSION WOVEN FABRICS TESTEFFECT OF TACKIFICATION RECONSTRUCTION OF MESOSCALE TEXTILE COMPOSITES MICRO-CT USING IMAGE & COMPUTER VISION ALGORITHM BUCKLING PROPERTY CONSIDERING COMPOSITE INTRALAMINAR LAMINATE OF PLAIN FABRIC WEAVE INHOMOGENEITY TENSILE PROPERTIES AND POISSON’S RATIO OF PET NEEDLE-PUNCHED NONWOVEN FABRIC PREPARED BY THERMOCOMPRESSION BY PREPARED OF PET NONWOVEN NEEDLE-PUNCHED FABRIC TENSILE PROPERTIES AND POISSON’S RATIO BONDING 3D BRAIDED AND NOTCHED COMPOSITES OF UN-NOTCHED BEHAVIOR FATIGUE PROPERTIES OF HELICOIDAL STRUCTUREIMPACT OF CARBON/EPOXY COMPOSITES Textile-based composites Textile-based SHEAR SIMULATIONS LOCAL DRAPING MULTIFACTORIAL ALGORITHM USING DEVELOPMENT OF A FAST NUMERICAL STUDY ON MECHANICAL PROPERTIES INFLUENCING BALLISTIC IMPACT BEHAVIOR OF WOVEN FABRICS USING CONSTANT CONSTANT USING OF WOVEN FABRICS NUMERICAL BEHAVIOR STUDY ON MECHANICAL PROPERTIES IMPACT INFLUENCING BALLISTIC TOUGHNESS APPROACH AXIAL COMPRESSION TESTING OF CARBON FIBERS A NOVEL TEST METHOD TO INDUCE BI-AXIAL STRESS STATES IN THIN PLY CARBON COMPOSITES UNDER COMBINED IN LONGITUDINAL THIN PLY A NOVEL TEST METHOD INDUCE TO BI-AXIAL STRESS STATES COMPRESSION AND TRANSVERSE TENSION OF HIGHMECHANICAL PERFORMANCE CHARACTERIZATION THERMAL DECOUPLING UNITS IN BUILDING ENVELOPS CHARACTERIZATION AND STATISTICAL ANALYSIS OF SINGLE FIBER STRENGTH OF FIBERS AT VARIOUS PROCESSING STAGES PROCESSING STAGES VARIOUS OF SINGLE FIBER OF FIBERS STRENGTH AT ANALYSIS AND STATISTICAL CHARACTERIZATION AN INNOVATIVE CIRCULAR RING METHOD FOR MEASURING YOUNG’S MODULUS OF THIN FLEXIBLE MULTI-LAYERED MATERIALS CIRCULAR MATERIALS RING METHOD FOR OF THIN MEASURING FLEXIBLEAN INNOVATIVE YOUNG’S MODULUS MULTI-LAYERED (COMPRESSIVE METHOD) RESIN TREATMENT FOR RELIABLE TRANSVERSE STRUCTURESRESIN SHEAR TREATMENT ASSESSMENT STRENGTH IN AEROSPACE CFRPS UNDER THE LAMINATE OF QUASI-ISOTROPIC EFFECTS POISSON’S OF GEOMETY RATIO SEQUENCE ON APPARENT AND STACKING COMPRESSION TESTS Testing methods Testing SELECTION OF A HYBRIDSINGLE RESIN FIBER PULL-OUT COMPOSITE TEST FOR THE MATERIAL STRAIN SENSING OF EPOXY CARBON RESIN NANOTUBE/GRAPHENE POROUS USING COMPOSITE BUCKYPAPER INFLUENCE OF OPTICALINFLUENCE FIBER SENSOR PLACEMENT MONITORING FOR PROCESS ON CFRP AND LAMINATES STRUCTURAL HEALTH DAMAGE DETECTION USING DIRECT-WRITE PIEZOELECTRIC IN COMPOSITE TRANSDUCERS DETECTIONDAMAGE MATERIALS AND DIRECT-WRITE LAMB USING WAVES SMART MECHANOLUMINESCENT MEMORY SHAPE FILM FOR FLEXIBLE STRESS SENSING DAMAGE VISUAL INDICATION SYSTEM FOR POLYMER COMPOSITE STRUCTURES FOR SYSTEM POLYMER INDICATION VISUAL DAMAGE DETECTION OF DAMAGES ON COMPOSITE PLATES DUE TO LOW VELOCITY IMPACT USING CARBON FIBERS USING VELOCITYDETECTION LOW DUE TO IMPACT ON COMPOSITE OF DAMAGES PLATES CLASSIFICATION AND PROPERTIES OF THREE-DIMENSIONALCLASSIFICATION TEXTILE PREFORMS monitoring health Structural OF MICROCAPSULES IN COMPOSITES AND OF MECHANICAL MODELLING EXPERIMENTAL CHARACTERIZATION BEHAVIOR LIGHTWEIGHT DESIGN OF COMPOSITE FOR BODY ELECTRIC MICROBUS DAMPING OPTIMIZATION OF LAMINATED PLATES BASED ON COMPLEX APPROACH PLATES MODULUS OF LAMINATED DAMPINGOPTIMIZATION REDESIGN AND OPTIMIZATION OF THERMAL PROTECTION SYSTEM FOR ATMOSPHERIC REENTRY REDESIGN FORTHERMAL OF SYSTEM ATMOSPHERIC AND PROTECTION OPTIMIZATION ALGORITHM OPTIMIZATION OPTIMIZING SWARM STRUCTURES DESIGN OF TRUSS VIA PARTICLE AN AUGMENTED EXPERIMENTAL AND SIMULATION STUDY FIBRE GFRP OF EXPERIMENTAL WITH DEFLECTION AND UNDER LOCAL SIMULATION BEARING LOADS THURSDAY 15 AUGUST POSTER SESSION THURSDAY title Poster CARBON FIBER ANISOTROPIC CARD USING WEB REINFORCEDDESIGN OF SEMI-COMPLEX THERMOPLASTICS PARTS P011 P017 P051 P041 P031 P021 P013 P012 P018 P019 P014 P015 P016 P010 P001 P037 P047 P027 P052 P032 P024 P053 P042 P025 P039 P023 P033 P035 P038 P007 P022 P036 P029 P026 P034 P049 P028 P043 P045 P050 P046 P048 P030 P044 P020 P040 P002 P003 P009 P005 P006 P004 P008 Poster no Poster Carolina Furtado Carolina Baixue Chang Baixue Musaddaq Azeem Musaddaq Tongzhou Zhu Tongzhou Derya Ozyurt Sun Jian Wang Yanan Wei Liang Wei Saeed Fazeli Fareed Tamaddoni Tamaddoni Fareed Jahromi Yunqian Zhang Yunqian Song Jungil Dong-min KimDong-min Peiyan Yang Peiyan Xiaoyu Zhang Mengchuan Xu Mengchuan Bing Xiao Anbazhagan Subramani Anbazhagan Abhendra Singh Abhendra Mae Oiwa Mae Harrison Lin Harrison Chong Li LiYinggang Sooyoung Lee Ghilane Bragagnolo Ghilane Ignacio Carranza Guisado Carranza Ignacio Hu Jiqiang Jayantha Epaarachchi Jayantha Yu Zhou Yu Aristeidis Tsiamis Aristeidis Simona Lavric Simona Larry Reyes Salumeh Issazadeh Callum Branfoot Cai Wanan Florian Röper Florian James MazzaJames Wei Feng Wei Yanan Zhang Yanan Taeyoung Kim Taeyoung Haoyi Li Lilla Simon-Stőger Oisik Das Sanjeev Rao Thomas Pozegic Thomas Haibo Yang Haibo Bianka Nagy Filip Salling Rasmussen Anatoly KoptelovAnatoly Li Yujun Waqas Ali Waqas Olivier Almeida De Chiung-Shiann Huang Chiung-Shiann Presenter name Presenter VIRTUAL CALCULATION OF THE B-BASIS ALLOWABLES OF NOTCHED COMPOSITE OF NOTCHED LAMINATES OF THE B-BASIS ALLOWABLES VIRTUAL CALCULATION AN ASYMPTOTIC SOLUTION TO DENSITY DISTRIBUTION OF GRADED CELLULAR MATERIALS WITH A CONSTANT IMPACT LOAD IMPACT DENSITY TO SOLUTION AN ASYMPTOTIC WITH A CONSTANT DISTRIBUTION OF GRADED CELLULAR MATERIALS Structural analysis and optimisation analysis Structural OF PET DBD PLASMA USING HYDROPHILIZATION ANALYSIS OF INTERFACE STRENGTH AND FAILURE MODE OF INDENTED SMA WIRE COMPOSITES AND STRENGTH FAILURE OF INTERFACE ANALYSIS SYNTHESIS OF GRAPHENE QUANTUM DOTS FROM LOW COST MATERIALS AND FABRICATION OF NANOCOMPOSITES AND FABRICATION SYNTHESIS OF GRAPHENE COST MATERIALS FROM LOW QUANTUM DOTS A MORPHING WINGTIP STRUCTURE LASER ENABLED FUNCTIONAL INDUCED COMPOSITES GRAPHENE FOR LIQUID MONITORING PAPERS PREPARATION AND CHARACTERIZATION OF THE RADIATION CROSSLINKED MEMORY SHAPE EVA/HDPE OF THE RADIATION AND CHARACTERIZATION PREPARATION Smart composite structures HARMONIC AND TRANSIENT COMPOSITE STEPPED RESPONSE DYNAMIC BEAM OF A SMART LAMINATED SELF-HEALING PROPERTIES OF CARBON-BLACK IMPREGNATED THERMOPLASTIC PROCESSED DEPOSITIONSELF-HEALING VIA PROPERTIES FUSED OF CARBON-BLACK POLYURETHANE IMPREGNATED MODELLING MANUFACTURING AND COMPARISON OF SPRINGBACKED CARBON FIBER AND REINFORCED COMPARISON MANUFACTURING THERMOPLASTIC SANDWICH STRUCTURES TUBESEFFECT OF VASCULAR DESIGN ON MECHANICAL AND SELF-HEALING PROPERTIES OF CFRP COMPOSITES Self-healing LINSEED OIL HEALING USING AGENT SELF-HEALING COATING PROTECTIVE MICROCAPSULE-BASED NUMERICAL SIMULATION OF IMPACT PERFORMANCE FOR PMI FOAM FILLED CORRUGATED BOARD SANDWICH BOARD PERFORMANCE STRUCTURE FOR PMI CORRUGATED FOAM FILLED OF IMPACT NUMERICAL SIMULATION OF COMPOSITE HONEYCOMB SANDWICH AND NUMERICAL REGARDING CHARACTERIZATION THE INDENTATION ANALYTICAL STRUCTURES MECHANICAL PROPERTIES AND ENERGY ABSORPTION CAPABILITY OF HYBRID HONEYCOMB SUPERSTRUCTURE DECONSOLIDATION BEHAVIOR OF CARBON FIBER REINFORCED BEHAVIOR THERMOPLASTICSDECONSOLIDATION AS CORE IN SANDWICH STRUCTURE DESIGN EXPLORATION OF MULTI-LAYER SANDWICH STRUCTURES TRANSVERSE TO LOADING OF MULTI-LAYER DESIGN EXPLORATION DAMAGE PREDICTION IN QUASI-STATICALLY INDENTED SANDWICH COMPOSITE STRUCTURES MODEL A TWO-REGION USING PLATE PREDICTION INDAMAGE QUASI-STATICALLY FRACTURE BEHAVIOR AND FACE SHEET BUCKLING ANALYSIS OF CFRP/HONEYCOMB SANDWICH PANELS SUBJECTED TO BENDING TO LOAD OF CFRP/HONEYCOMB SUBJECTED SANDWICH SHEET PANELS BUCKLING AND ANALYSIS FRACTURE FACE BEHAVIOR ADHESION OF DISSIMILAR POLYMER-METAL COMPOSITE MATERIAL BY MECHANICAL BY INTERLOCKING COMPOSITE MATERIAL ADHESION OF DISSIMILAR POLYMER-METAL NONLINEAR LOW-VELOCITY IMPACT RESPONSE OF SANDWICH BEAMS WITH FUNCTIONALLY GRADED NEGATIVE POISSON’S RATIO POISSON’S RATIO GRADED NEGATIVE RESPONSE OF SANDWICH BEAMS WITH IMPACT FUNCTIONALLY NONLINEAR LOW-VELOCITY HONEYCOMB CORE RESPONSES OF HONEYCOMB SANDWICH IMPACT PANELS REPEATED MODIFIED OF SANDWICH DCB TESTS FOR STRUCTURES MEASURING THE INTERFACE MODE I FRACTURE TOUGHNESS AT Sandwich structures and materials structures Sandwich FLEXURAL OF FOAM CORED SANDWICH BEHAVIOUR STRUCTURES REINFORCEMENTS WITH THROUGH-THICKNESS STUDY OF THE ENERGY ABSORPTION CAPABILITY OF SANDWICH STRUCTURES SHEETS WITH FOAM CORE AND CFRP FACE RESPONSE OF AS4/PEEK COMPOSITE LATTICE STRUCTRUES UNDER THE COMPRESSION LOADING VELOCITY AND LOW IMPACT LOW VELOCITY IMPACT RESPONSE OF CORRUGATED CORE SANDWICH PANELS - EFFECT OF IMPACTOR GEOMETRY - EFFECT OF IMPACTOR CORE SANDWICH PANELS RESPONSE VELOCITY OF CORRUGATED LOW IMPACT POLYANILINE/PHENOL-DIVINYLBENZENE RESIN FOR CFRP COMPOSITE WITH ENHANCED ELECTRICAL AND MECHANICALPOLYANILINE/PHENOL-DIVINYLBENZENE PROPERTIES LIQUID PROCESSABLE, THERMALLY STABLE, HYDROPHOBIC PHENOLIC-TRIAZINE RESINS FOR ADVANCED COMPOSITE HYDROPHOBIC PHENOLIC-TRIAZINE APPLICATIONS RESINS FOR STABLE, ADVANCED LIQUID PROCESSABLE, THERMALLY MELAMINE-MELTBLOWN NONWOVEN A HIGH-PERFORMANCE MATERIAL COMBINING FOR NONWOVEN THE A HIGH-PERFORMANCE FIRST TIME MATERIAL THERMOSETMELAMINE-MELTBLOWN MELAMINE WITH EXCELLENT THERMAL PROPERTIES AND ACOUSTIC OF ARYL ETHERANTIPLASTICSATION EPOXIES NEW THERMOSET MATRIX BASEDNEW ON BISOXAZOLINES THERMOSET MATRIX Resin and polymersResin PROCESSING AND HEALING COMPOSITES EPOXIES OF DIELS-ALDER AND THEIR FIBRE-REINFORCED POLYMER THE PREPARATION, OF HYPERBRANCHED BENZOXAZINE RESINS DERIVED FROM A2 + AND POLYMERIZATION SYNTHESIS,THE CHARACTERIZATION ONE-POT B3 MONOMERS BONDED COMPOSITE REPAIRS UNDER CONDITIONS DRY/COLDBONDED AND COMPOSITE HOT/WET ENVIRONMENTAL REPAIRS NEW MATERIAL REMOVAL TOOLS AND PROCESSES TO SAFELY EXPEDITE MAINTENANCE ON COMPOSITE AND SAFELY TOOLS PROCESSES STRUCTURES TO REMOVAL NEW MATERIAL Repair COMPOSITES OF IN-SERVICE REPAIRED AND RELIABILITYFAILURE ANALYSIS REAL-TIME SINGLE MOLECULAR STUDY OF A PRETREATED CELLULOSE HYDROLYSIS MODE AND INDIVIDUAL ENZYME MOVEMENT HYDROLYSIS SINGLE MOLECULAR CELLULOSE REAL-TIME STUDY OF A PRETREATED EFFECT OF CFRP OF A BRIMMED-DIFFUSER ON VORTEX-INDUCED SHROUD FOR A WIND VIBRATION TURBINE MELT ELECTROSPINNING: AN ECO-FRIENDLY WAY OF NANOFIBER AND GRAPHITIZED FIBRE PREPARATIONS USING NANOCELLULOSE NANOCELLULOSE USING OF NANOFIBER AND GRAPHITIZED FIBRE PREPARATIONS WAY ELECTROSPINNING: AN ECO-FRIENDLY MELT NOVELTY IN RECYCLING OF WASTE ELASTOMERS IN IN RECYCLING EXPERIMENTAL BLENDS COMPATIBILIZERS HDPE/PP BY OF WASTE NOVELTY Renewable Carbon Renewable BIOCHAR: COMPOSITE A POTENTIAL CONSTITUENT UPCYCLING OF AEROSPACE CARBON SCRAP: IMPACT OF MATERIAL PROPERTIES OF MATERIAL CARBON SCRAP: IMPACT UPCYCLING OF AEROSPACE DEVELOPMENT OF HIGH PERFORMANCE ALIGNED DISCONTINUOUS FIBRE MODIFICATION COMPOSITES: FIBRE SURFACE NUMERICAL SIMULATION OF FLOW OF RUBBER COMPOUNDS IN PARTIALLY FILLED INTERNAL FILLED MIXER OF RUBBER COMPOUNDS OF FLOW NUMERICALIN SIMULATION PARTIALLY Recycling and sustainability AND RECYCLED PET BASED OF NOVELINFLUENCE ADDITIVES TYPES IN BLENDS OF PA OF OLEFIN-MALEIC-ANHYDRIDE COPOLYMER A CHARACTERIZATION STUDY RELATING CROSS-SECTIONAL DISTRIBUTION STUDY RELATING OF FIBRE FRACTIONA CHARACTERIZATION AND VOLUME PERMEABILITY MACHINE-DRIVEN EXPERIMENTATION FOR SOLVING CHALLENGING CONSOLIDATION PROBLEMS CHALLENGING CONSOLIDATION FOR SOLVING MACHINE-DRIVEN EXPERIMENTATION GRADIENT EFFECTMODELING THE TEMPERATURE ON THE CURE-INDUCED CFRP OF LAMINATES DISTORTION L-SHAPED Process modelling Process FIBER THERMOPLASTIC LONG OF CHOPPED COMPOSITE 1D SQUEEZE ANALYSIS FLOW IN PROCESS THE MANUFACTURING OF THERMOPLASTIC OF IR USED LAMPS REFLECTOR WITH INTEGRATED MODELING STRATEGY COMPOSITE TAPES Computational and finite element methods element and finite Computational GRADED AND OF THE CRACKED MLS-RITZ FUNCTIONALLY OF LOADED METHOD THREE-DIMENSIONAL VIBRATIONS TO APPLICATIONS PLATES MATERIAL Poster title Poster THURSDAY 15 AUGUST POSTER SESSION THURSDAY

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