Proceedings

ICAF 2023
Delft, The Netherlands, 2023
Home Program Author Index Search

Authors Index

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [R] [S] [T] [V] [W] [X] [Y] [Z]
Author Manuscripts
Andrew Halfpenny
Hottinger Bruel & Kjaer Ltd
110 Tools and methods for landing gear fatigue analysis with surface treatment effects
Toko Hamaguchi
IHI
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
Bryce Harris
USAF
38 The inherent need for holistic structural integrity application and progress
Linden Harris
Airbus, UK
141 Will the metaverse transcend the status quo?
Daichi Haruyama
IHI
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole
Dingni He
26 Experimental study on the effect of different fatigue loading method on the property of metal cantilever beam
Yuting He
Air Force Engineering University, China
6 On the theory of aerocraft structural operational integrity control
Sebastian Heimbs
TU Braunschweig - Institute of Aircraft Design and Lightweight Structures (IFL)
71 Influence of the layer thickness on the very high cycle fatigue behaviour of composite materials
Johan Birnie Hernández
University of Bologna
117 Simulation of crack growth in adhesively bonded joints via cohesive zone models
Ryo Higuchi
Department of Aeronautics and Astronautics, The University of Tokyo
77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
21 A numerical scheme for fatigue simulation of laminated composites using CZM-XFEM
Michelle Hill
Hottinger Bruel & Kjaer Ltd
110 Tools and methods for landing gear fatigue analysis with surface treatment effects
111 Fatigue performance and cyclic deformation behaviour of titanium TI-6AL-4V additively manufactured by wire + ARC directed energy deposition
Josh Hodges
Hill Engineering
28 The integrated maintenance system (IMx+)
David Hoeppner
University of Utah
38 The inherent need for holistic structural integrity application and progress
Masahiro Hojo
JAXA
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole
Tatsuhito Honda
IHI
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole
Rong-Can Hong
Department of Aeronautics and Astronautics, The University of Tokyo
21 A numerical scheme for fatigue simulation of laminated composites using CZM-XFEM
Peter Horst
TU Braunschweig - Institute of Aircraft Design and Lightweight Structures (IFL)
71 Influence of the layer thickness on the very high cycle fatigue behaviour of composite materials
Atsushi Hosoi
Waseda University, Japan
83 Giga-Cycle Fatigue Properties of Transverse Crack Initiation in Cross Ply CFRP Laminates Using Ultrasonic Fatigue Testingn
Naoki Hosoya
Shibaura Institute of Technology
77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
Laura Hunt
Southwest Research Institute
15 Utilizing condemnations, retirements and mods to improve the structural risk analysis of the T-38: turning trash into treasure
Christopher Hurst
Manager, Structural Integrity
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [R] [S] [T] [V] [W] [X] [Y] [Z]