The Tide Is High Ton Fijen Answers Your Questions on the Development of Tidal Lagoon Schemes in Britain
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3D Fibre Reinforced Polymer Composites L
3D Fibre Reinforced Polymer Composites L. Tong, A.P. Mouritz and M.K. Bannister Elsevier 3D Fibre Reinforced Polymer Composites Elsevier Science Internet Homepage - http://www.elsevier.com Consult the Elsevier homepage for full catalogue information on all books, journals and electronic products and services. Elsevier Titles of Related Interest VALERY V. VASILEV & EVGENY V. MOROZOV Mechanics and Analysis of Composite Materials ISBN 0 08 042702 2 JANG-KYO KIM & YIU WING MAI Engineered Interfaces in Fiber Reinforced Composites ISBN: 0 08 042695 6 J.G. WILLIAMS & A. PAVAN Fracture of Polymers, Composites and Adhesives ISBN 0 08 0437 10 9 D.R. MOORE, A. PAVAN & J.G. WILLIAMS Fracture Mechanics Testing Methods for Polymers Adhesives and Composites ISBN 0 08 043689 7 A. BAKER, F. ROSE & R. JONES Advances in the Bonded Composite Repair of Metallic Aircraft ISBN: 0 08 042699 9 Related Journals: Composite Structures - www.elsevier.com/locate/comustruct Composites Part A: Applied Science and Manufacturing - www.elsevier.com/locate/comuositesa Composites Part B: Engineering - www.elsevier.com/locate/comuositesb Composites Science and Technology - www.elsevier.com/locate/comuscitech Major Reference Work: Comprehensive Composite Materials - www.elsevier.com/locate/isbn/0080429939 To contact the Publisher Elsevier Science welcomes enquiries concerning publishing proposals: books, joumal special issues, conference proceedings, etc. All formats and media can be considered. Should you have a publishing proposal you wish to discuss, please contact, without obligation, the publisher responsible for Elsevier's Composites and Ceramics programme: Emma Hurst Assistant Publishing Editor Elsevier Science Ltd The Boulevard, Langford Lane Phone: +44 1865843629 Kidlington, Oxford Fax: +44 1865 843931 OX5 IGB, UK E.mail: e.hurst @elsevier.com General enquiries, including placing orders, should be directed to Elsevier's Regional Sales Offices - please access the Elsevier homepage for full contact details (homepage details at the top of this page). -
Fatigue Behavior of 3D Braided Composites Containing an Open-Hole
polymers Article Fatigue Behavior of 3D Braided Composites Containing an Open-Hole Shuangqiang Liang 1,2 , Qihong Zhou 1, Haiyang Mei 3, Ge Chen 1,* and Frank Ko 2 1 Department of Mechanical Engineering, Donghua University, Shanghai 200051, China; [email protected] (S.L.); [email protected] (Q.Z.) 2 Department of Material Engineering, University of British Columbia, Vancouver, BC V6T 1Z4, Canada; [email protected] 3 School of Mechatronic Engineering, Harbin Institute of Technology, Harbin 150001, China; [email protected] * Correspondence: [email protected] Received: 9 July 2020; Accepted: 18 August 2020; Published: 21 September 2020 Abstract: The static and dynamic mechanical performances of notched and un-notched 3D braided composites were studied. The effect of longitudinal laid-in yarn was investigated in comparison with low braiding angle composites. The specimens were fatigue tested for up to millions of cycles, and the residual strength of the samples that survived millions of cycles was tested. The cross-section of the 3D braided specimens was observed after fatigue loading. It was found that the static and fatigue properties of low angle 3D braided behaved better than longitudinally reinforced 3D braided composites. For failure behavior, pure braids contain damage better and show less damage area than the braids with longitudinal yarns under fatigue loading. More cracks occurred in the 3D braided specimen with axial yarn cross-section along the longitudinal and transverse direction. Keywords: textiles; 3D braided; notched; fatigue; failure 1. Introduction Three-dimensional braided composites, due to their proven damage tolerance, delamination free properties, and the ability to generate complex network structures in composites, continue to attract academic and industrial researchers’ interest in a wide variety of matrix types, covering carbon (CCC), ceramics (CMC), metal (MMC) and polymer (PMC) matrix composites [1]. -
Textile Reinforced Structural Composites for Advanced Applications
Chapter 4 Textile Reinforced Structural Composites for Advanced Applications Nesrin Sahbaz Karaduman, Yekta Karaduman, Huseyin Ozdemir and Gokce Ozdemir Additional information is available at the end of the chapter http://dx.doi.org/10.5772/intechopen.68245 Abstract Textile-reinforced composites are increasingly used in various industries such as aero- space, construction, automotive, medicine, and sports due to their distinctive advantages over traditional materials such as metals and ceramics. Fiber-reinforced composite mate- rials are lightweight, stiff, and strong. They have good fatigue and impact resistance. Their directional and overall properties can be tailored to fulfill specific needs of different end uses by changing constituent material types and fabrication parameters such as fiber volume fraction and fiber architecture. A variety of fiber architectures can be obtained by using two- (2D) and three-dimensional (3D) fabric production techniques such as weav- ing, knitting, braiding, stitching, and nonwoven methods. Each fiber architecture/textile form results in a specific configuration of mechanical and performance properties of the resulting composites and determines the end-use possibilities and product range. This chapter highlights the constituent materials, fabric formation techniques, production methods, as well as application areas of textile-reinforced composites. Fiber and matrix materials used for the production of composite materials are outlined. Various textile production methods used for the formation of textile preforms are explained. Composite fabrication methods are introduced. Engineering properties of textile composites are reviewed with regard to specific application areas. The latest developments and future challenges for textile-reinforced composites are presented. Keywords: textile-reinforced composites, fiber architectures, textile production methods, advanced applications, engineering properties © 2017 The Author(s). -
Development of 3D Braiding Concept for Multi-Axial Textile Preforms
Development of 3D Braiding Concept for Multi-Axial Textile Preforms A thesis submitted to The University of Manchester for the degree of PhD in the Faculty of Engineering and Physical Sciences 2015 KHAYALE JAN Textile Composite Group SCHOOL OF MATERIALS Table of Contents Development of 3D Braiding Concept for Multi-Axial Textile Preforms ................................... 1 List of Figures .............................................................................................................................. 5 Abstract ...................................................................................................................................... 11 Declaration................................................................................................................................. 12 Copyright Statement ................................................................................................................. 13 Dedication .................................................................................................................................. 14 Acknowledgement ..................................................................................................................... 15 1 CHAPTER 1 INTRODUCTION ................................................................................................ 16 1.1 Brief Account of Textile Preforms and Preforming Techniques ................................. 16 1.2 Research Aims ............................................................................................................ -
Continuum Damage Mechanics Models and Their Applications To
Continuum Damage Mechanics Models and Their Applications to Composite Components of Aero-Engines A thesis for the degree of Doctor of Philosophy Tian-Hong Yu 2016 Composites Research Group, Faculty of Engineering, The University of Nottingham, Nottingham NG7 2RD, UK Acknowledgements First of all, I would like to thank my supervisor, Prof. Shuguang Li, who shared valuable expertise and provided important guidance to me throughout the course of this research project, which enabled me to achieve significant progress in the last three years. His attention to detail, patience and academic professionalism not only ensured the delivery of high quality supervision to my research project, but also inspired me to tackle technical problems with persistence and confidence, from which I will benefit for the rest of my life. I would also like to express my gratitude to my co-supervisors. My gratitude goes to Dr. Elena Sitnikova, for her helpful feedbacks on my research work and her comprehensive advice on my thesis writing, and to Dr. Richard Brooks, for his effort to help sourcing the materials for the experimental work. The generous support from AVIC Commercial Aircraft Engine Co. Ltd. (ACAE), both financially and technically, which made this research project possible, is gratefully acknowledged. My gratitude also goes to my fellow research team members from ACAE, for their support and the quality time we spent together working for a joint research program. Moreover, I am forever in debt to my parents for the understanding, encouragement and support they provided to me in the last few years, which allowed me to focus on my PhD study.