AERO 2021 Program Workbook June 3.Xlsx

Symposium Abbreviations

AD&D AERO AMT AS&M Aircraft Design Aerodynamics Aerospace Manufacturing Aerospace Structures & Development Technologies & Materials HF&T FT&FO PROP Human Factors Flight Operations Propulsion & Training & Flight Test DATE TIME ACTIVITY Parallel Session A Parallel Session B Parallel Session C Parallel Session D Mon 12:00 ‐ 12:20 Welcome Welcoming and Opening Remarks 14 12:20 ‐ 13:15 Plenary Panel 'Enabling Electric Flight' ‐ Chair, Malcolm Imray, NRC June 13:15 ‐ 13:30 Break Networking in the 'Lobby' 13:30 ‐ 15:00 Tech Session 1 A AERO B AD&D/FT&FO/PROP C AD&D/FT&FO/PROP D AS&M/AMT Computational Hybrid Electric Hybrid Electric Additive Methods 1 Aircraft 1 Aircraft ‐ Drones Manufacturing 1 15:00 ‐ 15:15 Break Networking in the 'Lobby' 15:15 ‐ 16:45 Tech Session 2 A AERO B AD&D/FT&FO/PROP C AD&D/FT&FO/PROP D AS&M/AMT Optimization Hybrid Electric Envrionmentally‐friendly Additive Methods 1 Aircraft 2 Design Manufacturing 2 16:45 ‐ 17:15 Meet & Greet Forge / renew acquaintances with colleagues in the 'Lobby' Tues 12:00 ‐ 12:20 Award Presentation of the 2018 McKee Trophy to Kevin Horton 15 12:20 ‐ 13:15 Keynote 'National Centre for Flight Research' of the National Research Council June Kirk Shaw, Director Research and Development, Aerospace, NRC 13:15 ‐ 13:30 Break Networking in the 'Lobby' 13:30 ‐ 15:00 Tech Session 3 A AERO B AD&D C PROP D AS&M/AMT Aeroelasticity Unmanned Aerial Systems Inlet Design Composites 1 Design & Applications 15:00 ‐ 15:15 Break Networking in the 'Lobby' 15:15 ‐ 16:45 Tech Session 4 A AERO B AD&D C PROP D AS&M/AMT Mesh Adaptation Product Development & Combustion Materials & Manufacturing Operations Wed 12:00 ‐ 13:15 Plenary Panel 'Certification by Analysis: The State of the Art' ‐ Chair, Dany Paraschivoiu, NRC 16 13:15 ‐ 13:30 Break Networking in the 'Lobby' June 13:30 ‐ 15:00 Tech Session 5 A AERO B AD&D C PROP D AS&M Propulsion & Rotorcraft Unmanned Aerial Systems: Modeling & Testing Experimental Characteri‐ Aerodynamics Flight Dynamics zation & Monitoring 15:00 ‐ 15:15 Break Networking in the 'Lobby' 15:15 ‐ 16:45 Tech Session 6 A AERO B AS&M C FT&FO/HF&T D AMT Fluid Dynamics & Modelling Topology Optimization Flight Performance Intelligent Manufacturing

Thurs 12:00 ‐ 13:15 Keynote 'Enabling Improved Aircraft Performance through Floating Folding Wing Tips' 17 Dr Jonathan Cooper FRAES, Airbus Sir George White Professor of Aerospace Engineering June University of Bristol 13:15 ‐ 13:30 Break Networking in the 'Lobby' 13:30 ‐ 15:00 Tech Session 7 A AERO B AERO C FT&FO/HF&T D AMT Computational Applied Aerodynamics Human Factors Consider‐ Integrated Air Mobility Methods 2 ations in Aviation 15:00 ‐ 15:15 Break Networking in the 'Lobby' 15:15 ‐ 16:45 Tech Session 8 A AERO B AERO C FT&FO/HF&T D AS&M Optimization Supersonic & Hypersonic Human & Flight Dynamics Modelling & Simulation Methods 2 Modelling Fri 12:00 ‐ 12:20 Award Presentation of the 2020 McKee Trophy to 415 Squadron 18 12:20 ‐ 13:15 Turnbull Lecture 'The Evolving Regulatory Environment for UVS Operations' June Dr John Maris FCASI, McKee Trophy Laureate, President Marinvent Corporation 13:15 ‐ 13:30 Break Networking in the 'Lobby' 13:30 ‐ 15:00 Tech Session 9 A AERO B AD&D C AMT D AS&M Icing & Heat Transfer Numerical Methods: Composites 2 Certification & Validation Aerospace Applications 15:00 ‐ 15:15 Break Networking in the 'Lobby' 15:15 ‐ 16:45 Tech Session 10 ABCAMT D AS&M Additive Manufacturing 3 Dynamic Analysis & Testing

16:45 ‐ 17:15 Wrap‐up Acknowledgments and a Look Ahead in the 'Lobby' Technical Session 1Mon | 13:30 ‐ 15:00

AERO AD&D/FT&FO/PROP AD&D/FT&FO/PROP AS&M/AMT

Hybrid Electric Aircraft ‐ Computational Methods 1Hybrid Electric Aircraft 1 Additive Manufacturing 1 Drones Chair: Hong Yang, Chair: Billy Allan, Chair: Jonathan Liscouet, Chairs: Marjan Molavi‐Zarandi, Bombardier Aviation Royal Military College Concordia University NRC/ Sheida Sarafan, NRC 1A-01 1B-01 1C-01 1D-01 Hybridized flux reconstruction Development of the NRC Hybrid Evaluation of drone safety and In-situ material production: multi- schemes for convection problems Electric Aircraft Testbed (HEAT) reliability material 3D manufacturing by pressing and cooking deposited powders layer-by-layer

Carlos Pereira Patrick Zdunich Edwina Arthur Antoine Missout Concordia University National Research Council Concordia University Kilncore Inc.

1A-02 1B-02 1C-02 1D-02 Implementation of communication Development of a hybrid-electric CREATeV: An evaluation of the solar In-envelope additive and subtractive hiding parallel scaled-additive aircraft simulation tool for safety charging optimization for ultra-long manufacturing for a maraging steel multigrid for implicit solvers analyses endurance flight

Syam Vangara et al Alexander Crain et al Korbin Mallette Sheida Sarafan McGill University National Research Council Ryerson University National Research Council

1A-03 1B-03 1C-03 1D-03 Frequency domain method in CFD: Performance and qualification Comparison of sizing methodologies Microstructure and mechanical from linear to nonlinear dynamics testing of an electric propulsion for high-reliability multicopters properties of β-21S Ti alloy system fabricated through laser powder bed fusion

Frederic Plante Pervez Canteenwalla et al Robin Warren Maria Macias-Sifuentes et al Polytechnique Montreal National Research Council Concordia University McGill University

1A-04 1B-04 1C-04 1D-04 High-order spectral element method A study of aircraft classification Performance prediction analysis for Additively-manufactured TPMS simulation of low Reynolds Number approaches for the certification of Aero-Naut CAM folding propellers structures for transpiration cooling flow past a 30P30N high lift Unmanned Aircraft Systems and its application into CREATeV configuration solar aircraft

Mayank Vadsola et al Nicolas Vincent-Boulay Hyunwoo Kim Kevin Zhang University of Ottawa Royal Military College Ryerson University University of Waterloo

AERO AD&D/FT&FO/PROP AD&D/FT&FO/PROP AS&M/AMT

Envrionmentally‐friendly Optimization Methods 1Hybrid Electric Aircraft 2 Additive Manufacturing 2 Design Chair: David W. Zingg, Chair: Malcolm Imray, NRC Chair: Susan Liscouet‐Hanke, Chairs: Micheal Jakubinek, University of Toronto Concordia University NRC/Julieta Barroeta Robles, McGill University 2A-01 2B-01 2C-01 2D-01 Non-stochastic robust design of Performance analysis of a hydrogen Prediction of aero-propulsive Mechanical evaluation of additively- airfoils through the imposition of fuel cell-powered general aviation performance using adaptive lookup manufactured composite materials constraints on second-order aircraft tables – application on the Cessna sensitivities Citation X business aircraft

Almir Tricic et al Germain Jaillier Anca Stepan Julieta Barroeta Robles Clarkson University Université de Sherbrooke École de technologie supérieure National Research Council

2A-02 2B-02 2C-02 2D-02 Dynamic geometry control for more Preliminary feasibility analysis on Systems radiation consideration for Effect of infill density on the automated aerodynamic shape the use of hydrogen fuel cells for a thermal risk assessment in mechanical properties of additive optimization hybrid-electric aircraft testbed conceptual design manufactured parts made from PLA

Gregg Streuber Evan Gibney Tanmay Bhise Hayat El Fazani University of Toronto National Research Council Concordia University Carleton University

2A-03 2B-03 2C-03 2D-03 Full-space approach to constrained Electrically-powered flight-safe Improvement of the regional jet An insight into process-structure- aerodynamic shape optimization ceramic CRJ700 winglet design based on property relationships in laser morphing wing principles powder bed fusion of aerospace alloys

Doug Shi-Dong et al Shuo Yan et al Marine Segui Mohamed Balbaa McGill University University of Ottawa École de technologie supérieure McMaster University

2A-04 2B-04 2C-04 2D-04 Aerodynamic optimization of Mission profile performance Aerodynamic design optimization of Surface post-processing for additive unsteady chaotic flows analysis of an on-ground serial a transonic strut-braced-wing manufactured parts: reducing hybrid-electric drivetrain for regional jet class aircraft surface roughness and improving aircraft propulsion fatigue life with electrospark deposition

Hamid Karbasian Madeline McQueen Timothy Chau Pablo Enrique Concordia University Ryerson University University of Toronto University of Waterloo Institute for Aerospace Studies AD&D AERO AMT AS&M Aircraft Design Aerodynamics Aerospace Manufacturing Aerospace Structures & Development Technologies & Materials HF&T FT&FO PROP Human Factors Flight Operations Propulsion & Training & Flight Test Technical Session 3Tues | 13:30 ‐ 15:00

AERO AD&D PROP AS&M/AMT

Unmanned Aerial Systems: Aeroelasticity Inlet Design Composites 1 Design & Applications Chair: Dominique Poirel, Chair: Stephane Dufresne, Chair: James Crone, Chairs: Marc Palardy‐Sim, Royal Military College Bombardier Aerospace Pratt & Whitney Canada NRC/Hadi Nazaripoor, University of Alberta 3A-01 3B-01 3C-01 3D-01 Numerical simulation on gust Design lessons from Concordia's Automation scheme implementing Resistance welding of discontinuous response of a 1-DOF wing in stall 2020-20201 AERO490 Capstone on passive flow control in numerical S- long fibre thermoplastic composites flutter the design of an autonomous UAV duct analysis for transplant organ transportation

Xiaoyang Zhang Nicolae Rogojina Courtney Rider Marc Palardy-Sim Royal Military College Concordia University Royal Military College National Research Council

3A-02 3B-02 3C-02 3D-02 Gust performance predictions of Low-speed computational Performance evaluation of internal Structural design optimization for flexible aircraft aerodynamics and design flow in a Y-duct intake at high CFRP in a personal aerial vehicle optimization of fuselage subsonic mach number propulsor boom enlargements in support of autonomous cargo aircraft

Michael Melville Jeremy Wang Asad Asghar Andrew Hardman Ryerson University University of Waterloo Royal Military College Queen's University

3A-03 3B-03 3C-03 3D-03 Viscous and transonic dynamic Autonomous strategic defence: An Adaptability of the human larynx Reliability evaluation of manual and aeroelastic simulations of wings adaptive clustering approach to the functionality in aircraft engine automated tap testing for disbond using non-linear frequency domain n-Invader Capture Order Problem design detection in honeycomb structures potential solvers

Matthieu Parenteau Noah Zepp et al Amey Rangbulla Muzibur Khan Polytechnique Montréal University of Toronto University of Toronto National Research Council Institute for Aerospace Studies 3A-04 3B-04 3C-04 3D-04 A model-order reduction approach The business case and game- Effect of residual stress due to low- for flutter analysis changing economics of autonomous velocity impact damage on the in- fixed-wing aircraft plane compressive strength in aluminum honeycomb sandwich panels

Brandon Lowe Andy Ortaaslan Tony Badea University of Toronto N/A Royal Military College

AERO AD&D PROP AS&M/AMT

Product Development & Mesh Adaptation Combustion Materials & Manufacturing Operations Chair: Charles Tatossian, Chair: Pat Piperni, Chair: Billy Allan, Chairs: Ehsan Toyserkani, Bombardier Aviation Clarkson University Royal Military College University of Waterloo/ Vladimir Pankov, NRC 4A-01 4B-01 4C-01 4D-01 Automatic mesh optimization of Methods to improve product Computational framework for the Bioinspired strategies to design direct simulation Monte Carlo development timeliness prediction of radiative heat transfer tough ceramics methods for hypersonic flows in sooting turbulent diffusion flames with tabulated chemistry

Shrutakeerti MV Shourav Ahmed Joachim Sarr et al Hamidreza Yazdani Sarvestani McGill University McGill University University of Toronto National Research Council Institute for Aerospace Studies 4A-02 4B-02 4C-02 4D-02 Dynamic load balancing for a HP- Using semantic modelling to provide RANS-based Two-Equation Model Machine learning algorithms in adaptive discontinuous Galerkin insight into the aircraft modification with tabulated chemistry for the accelerating the design of Wave Equation solver product development process prediction of soot formation in architectured ceramic materials turbulent non-premixed flames

Catherine Mavriplis Andrea Cartile Clinton Groth et al Erfan Fatehi University of Ottawa Concordia University University of Toronto National Research Council Institute for Aerospace Studies 4A-03 4B-03 4C-03 4D-03 Industrial-scale mesh adaptation Turboprop design analysis in Eulerian-based maximum-entropy Fabrication of coatings with based on a point cloud size-field regional route networks considering moment closures for modelling enhanced wear and impact carbon pricing economics polydisperse liquid fuel sprays resistance using a duplex approach

Siva Nadarajah et al Stewart Reid Kevin Brooks et al Vladimir Pankov McGill University Royal Military College University of Toronto National Research Council

4A-04 4B-04 4C-04 4D-04 A dynamically load-balanced Far-field aero-acoustic prediction Eulerian-Lagrangian CFD- Ultra-durable icephobic coatings for vorticity-based polynomial using high-order implicit large eddy microphysics modeling of ground- passive ice protection of leading adaptation for moving and simulation level aircraft-emitted aerosol edge surfaces deforming domains formation

Ramin Ghoreishi Mohsen Hamedi Sébastien Cantin Naiheng Song Concordia University Concordia University École de technologie supérieure National Research Council

AERO AD&D PROP AS&M

Propulsion & Rotorcraft Unmanned Aerial Systems: Experimental Characterization Modeling & Testing Aerodynamics Flight Dynamics & Monitoring Chair: Mark Cunningham, Chair: Ruxandra Botez, École Chair: Asad Asghar, Chairs: Marc Genest, NRC/ Pratt & Whitney Canada de technologie supérieure Royal Military College Ali Bonakdar, Siemens Canada

5A-01 5B-01 5C-01 5D-01 Aerodynamic shape optimization of UAS-S4 flight dynamics model Development of a low-bypass Experimental study of the a boundary layer-ingesting S-Duct prediction based on data turbofan real degraded-engine hybridization effect on bolt-hole augmentation and support vector model elongation of multi-bolted single-lap regression composite joints using DIC

Christopher Chiang Seyed Mohammad Hashemi Juan Angulo Reyes Masoud Mehrabian University of Toronto École de technologie supérieure Royal Military College Polytechnique Montréal

5A-02 5B-02 5C-02 5D-02 Actuator line method for helicopter Longitudinal swing angle control for An accurate generic turbofan aero- Online monitoring of laser powder rotors Computations in various a fixed-wing UAV with a slung load thermodynamic model for design bed fusion based process on flight conditions trade-off studies acoustic emission signatures and machine learning

Reda Merabet Seyedreza Fattahi Massoum Manuel Gurrola-Arrieta Dalia Mahmoud Polytechnique Montréal University of Toronto École de technologie supérieure McMaster University Institute for Aerospace Studies 5A-03 5B-03 5C-03 5D-03 Progress towards rapid non-linear Neural network-based robust System integration and engine test An instrumented shot peening test potential flow method for rotary- dynamic soaring of a 22KN oxidiser-rich staged rig for single and repeated wing aerodynamics combustion rocket engine controlled impact conditions

Vincent Proulx-Cabana Eric Kim Sadben Khan Simon Breumier Polytechnique Montréal Royal Military College C6 Launch Systems Polytechnique Montréal

5A-04 5B-04 5C-04 5D-04 Simulating the perturbation effects Aerodynamic effect in 3D multi-UAV General Electric CF34-8C5B1 Deep learning for defect detection within an under-expanded cooperative hunting turbofan parameter estimation: new and characterization in composite supersonic jet approach using artificial neural laminates inspected by pulsed networks and flight tests thermography

Frederick Ferguson Shichen Fan Rojo Princy Andrianantara Mohammadhossein Ahmadi et al North Carolina A&T State University University of Toronto École de technologie supérieure Université Laval Institute for Aerospace Studies AD&D AERO AMT AS&M Aircraft Design Aerodynamics Aerospace Manufacturing Aerospace Structures & Development Technologies & Materials HF&T FT&FO PROP Human Factors Flight Operations Propulsion & Training & Flight Test Technical Session 6Wed | 15:15 ‐ 16:45

AERO AS&M FT&FO/HF&T AMT

Fluid Dynamics & Modelling Topology Optimization Flight Performance Intelligent Manufacturing

Chair: François Bisson, Chairs: Priti Wanjara, NRC/ Chair: Malcolm Imray, NRC Chairs: Rachid Guiassa, Airbus Canada Mathieu Brochu, McGill Pratt & Whitney Canada/ University Sam Gerges, Omnirobotic 6A-01 6B-01 6C-01 6D-01 A correlation-based algebraic Efficient heat management via Development of microgravity flight 3D perception: the gateway to transition model for flow over rough topology optimization: a diffuse and sciences regime recognition autonomous robotic manufacturing surfaces a sharp method software

Mehrdad Noei Yazdian Marc-Etienne Lamarche-Gagnon Marc Alexander François Simard École de technologie supérieure National Research Council National Research Council Omnirobotic

6A-02 6B-02 6C-02 6D-02 Effects of surface imperfections on Topology optimization for the Preparation for and first flight of the Realtime unmanned cyber-physical the stability of boundary layers design of additively-manufactured Celera 500 system to improve productivity, part cooling channels quality and tool life in drilling processes

Ming Teng Farshad Navah et al Bjarni Tryggvason Mahmoud Hassan Queen's University National Research Council MILAD Technology Inc National Research Council

6A-03 6B-03 6C-03 6D-03 An extended assessment of camber Multi-material topology Aircraft takeoff performance Closed-door metrology in multi-axis morphing analysis for the optimization of an eVTOL PAV wing machining center aerodynamic performance of the considering additive manufacturing UAS-S45 airfoil

Musavir Bashir Tim Sirola et al Bjarni Tryggvason Rachid Guiassa École de technologie supérieure Queen's University MILAD Technology Inc Pratt & Whitney Canada

6A-04 6B-04 6C-04 6D-04 Sideslip effects on a square plate Topology optimization for DfAM Multiple L-band LEO satellites based Model-based prediction of robot’s under freestream turbulence with build area constraints doppler shift/INS Integrated behavior in milling operations of Navigation System with flight test aeronautic parts demonstration

Stephanie Hartlin Rosalie Morin (et al) Hamza Benzerrouk et al Christopher Lapointe McGill University Queen's University École de technologie supérieure École de technologie supérieure

AERO AERO FT&FO/HF&T AMT

Human Factors Considerations Computational Methods 2 Applied Aerodynamics Integrated Air Mobility in Aviation Chair: Brian Vermeire, Chair: Götz Bramesfeld, Chair: Malcolm Imray, NRC Chairs: Bruno Monsarrat, Concordia University Ryerson University NRC/ Amir Hajzargarbashi, NRC 7A-01 7B-01 7C-01 7D-01 Low-Reynolds Number direct Unsteady aerodynamic performance Development of a real-time desktop Keynote: Integrated aerial mobility numerical simulation of an iced NLF- of a tethered autogyro flight simulator for stratospheric program status update 0414 airfoil airships

Catherine Mavriplis Aditya Agarwal et al Mohsen Rostami et al Charles Vidal University of Ottawa Concordia University Ryerson University National Research Council

7A-02 7B-02 7C-02 7D-02 Towards detached eddy simulation Experimental study of the Development and evaluation of Keynote: Integrated aerial mobility of massively separated flows in high- aerodynamic loads on the airframe flight deck using augmented reality program status update lift configurations of a multirotor UAV

Hong Yang Devin Barcelos Pratik Pradhan et al Charles Vidal Bombardier Aviation Ryerson University Ryerson University National Research Council

7A-03 7B-03 7C-03 7D-03 CHAMPS: CHApel Multi-Physics CRJ 700 Stall Dynamics: Visualization of multi-functional Robust tracking for UAV using Simulation software Identification using Neural aircraft cabin Dempster-Shafer theory based on Networks continuous-discrete Gauss Hermite H_infinity filtering under uncertainties

Matthieu Parenteau et al Yvan Tondji Aditya Venkatesh et al Abulasad Elgamoudi Polytechnique Montréal École de technologie supérieure Ryerson University École de technologie supérieure

7A-04 7B-04 7C-04 7D-04 Asynchronous point-block Extending the parameters for the National Research Council and smoothers for computational fluid performance evaluations of leading International Test Pilot School dynamics on graphics processing edge tubercles Canada: An overview of professional units Canadian rotary-wing flight test aircrew training

Siva Nadarajah Satpreet Singh Sidhu et al Marc Alexander McGill University Royal Military College National Research Council

AERO AERO FT&FO/HF&T AS&M

Supersonic & Hypersonic Optimization Methods 2 Human & Flight Dynamics Modelling & Simulation Modelling Chair: Pat Piperni, Chair: François Bisson, Chair: Joon Chung, Chairs: Marjan Molavi‐Zarandi, Clarkson University Airbus Canada Ryerson University NRC/ Naiheng Song, NRC 8A-01 8B-01 8C-01 8D-01 Adjoint solver for large-scale high- Finite element modeling of gas- A historical and technical survey of Numerical simulation of thermo- speed aerodynamics cases on multi- surface interactions in hypersonic flight research of the NRC Bell 206 mechanical behavior of CFRP element unstructured meshes flight research aircraft composite laminate subjected to laser paint removal process using varying beam profiles

Syam Vangara et al John Huang Marc Alexander Rahul Shah McGill University McGill University National Research Council Carleton University

8A-02 8B-02 8C-02 8D-02 High-fidelity gradient-free Numerical study of the transition Multi-phase trajectory optimization Damage modelling of a laminated optimization of low-pressure from regular to mach reflection on for airliners’ formation flight composite panel subjected to low turbine cascades smooth wedges and semicircular considering TCAS constraints velocity impact cylinders

Anthony Aubry et al Marcel Grzeszczyk et al Shirin Dolatabadi Gang Li et al Concordia University University of Toronto University of Toronto National Research Council Institute for Aerospace Studies Institute for Aerospace Studies 8A-03 8B-03 8C-03 8D-03 Toward aerodynamic shape Input/output analysis of hypersonic Applications of geometric deep Practical formulation of Kane’s optimization for the design of boundary layers using the One-Way learning to flight dynamics Method for finite element natural-laminar-flow wings Navier-Stokes (OWNS) equations modelling representation of rigid-flexible systems

Michael Piotrowski Omar Kamal Oreoluwa Ajayi Alexander Schock University of Toronto California Institute of Technology NeuralVol Aeronautics Inc Carleton University

8A-04 8B-04 8C-04 8D-04 Assessment of interpolation-based Canadian air travel during a model-reduction approaches for the pandemic: the past, present, and the transonic flow regime future

Donovan Blais et al Paul Lebbin McGill University National Research Council

AERO AD&D AMT AS&M

Numerical Methods: Icing & Heat Transfer Composites 2 Certification & Validation Aerospace Applications Chair: François Morency, Chair: Stephane Dufresne, Chairs: Micheal Jakubinek, Chairs: Dany Paraschivoiu, École de technologie Bombardier Aerospace NRC/Yadienka Martinez‐Rubi, NRC/ Hossein Monajati, LISI supérieure NRC Aerospace Canada 9A-01 9B-01 9C-01 9D-01 Development of an aircraft icing Enhancing performance for target Keynote: Carbon and boron nitride Certification by Analysis for suite using chapel programming tracking estimation algorithm using nanotube composites for structural Structures language Dempster– Shafer fusion approach materials and functional coatings and continuous-discrete Gauss Hermite filtering

Hélène Papillon Laroche Abulasad Elgamoudi Yadienka Martinez-Rubi Dany Paraschivoiu Polytechnique Montréal École de technologie supérieure National Research Council National Research Council

9A-02 9B-02 9C-02 9D-02 Numerical modeling of thermal Single event upset characterization Keynote: Carbon and boron nitride Finite element-based fatigue protection systems ablation in of Microsemi RISC-V softcores on nanotube composites for structural damage analysis approach for hypersonic flight Polarfire FPGAs materials and functional coatings aircraft structures with multiple initial damages and material variability

Guangwei Liu Devin Ramaswami et al Yadienka Martinez-Rubi Ayhan Ince McGill University University of Saskatchewan National Research Council Concordia University

9A-03 9B-03 9C-03 9D-03 On the impact of internal heat Advanced composite forming: an Fatigue failure analysis of an IN718 sources in high-speed vehicles using alternative forming technology airplane bolt conjugate heat transfer analysis

Syed Imthiaz Ahamed Meysam Rahmat Hossein Monajati University of Waterloo National Research Council LISI Aerospace Canada

9A-04 9B-04 9C-04 9D-04 Integrated design optimization On measuring interface loads in scheme for fiber reinforced additive structural full-scale testing - manufacturing planning, calibration and data processing

Noah Ray Calista Biondic Queen's University National Research Council

AMT AS&M

Additive Manufacturing 3Dynamic Analysis & Testing

Chair: Chair: Chairs: Irina Garces, Chairs: Ahmed Damir, NRC/ University of Alberta/ Gabriel Côté, NRC Hamid Akbarzadeh, McGill U 10A-01 10B-01 10C-01 10D-01 Aerostructures design-to-additive Explicit dynamic modeling of a manufacturing using novel powder- composite aircraft seat concept metal fabrication procedure subject to dynamic certification tests

Nabil Saad Logan Kupchanko Inno-Centre Queen's University

10A-02 10B-02 10C-02 10D-02 The effect of crystallographic An efficient Bayesian model orientation on the mechanical selection algorithm for a pitching properties of laser-powder-bed- airfoil model undergoing limit cycle fusion-processed Hastelloy X oscillations

Oscar Sanchez-Mata et al Abhijit Sarkar et al McGill University Carleton University

10A-03 10B-03 10C-03 10D-03 Heat source modelling for multiscale Structural dynamics of a tethered laser powder bed fusion additive kite used for harnessing high- manufacturing altitude winds

Yohann Vautrin Amar Fayyad K. Akberali National Research Council Concordia University

10A-04 10B-04 10C-04 10D-04 High-temperature 3D printing and Piezoelectric (PE) technology and electrolysis of lunar regolith: multicomponent force measurement challenges and solutions for landing gear drop testing

Antoine Missout William Zwolinski et al Kilncore inc. Kistler Canada