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
Pietro Aceti Politecnico di Milano	140 Meso-scale models to analyse the interactions of damage modes in composites laminates
Oluwamayokun B. Adetoro	138 Opmimization of hybrid composite-metal joints
Alessandro Airoldi Politecnico di Milano	140 Meso-scale models to analyse the interactions of damage modes in composites laminates
René C. Alderliesten Aerospace Engineering, TU Delft	22 Experimental investigation of planar delamination behavior of composite laminates under out-of –plane loading 36 Towards understanding residual strength and damage evolution in damaged composite laminates 51 Compression after impact fatigue damage growth in CFRP - What does no-growth really mean? 127 Can we predict fatigue crack growth without the help of Paris? 142 On the mechanism of cyclic crack propagation in AA2024 T3 alloy. 148 Combined mechanical and environmental ageing of FRPs - Hygrothermal fatigue case study
Sébastien Amiable airbus	52 A new approach to accidental damage on aircraft metallic structure
Emiel Amsterdam NLR	32 Back to basics for the fatigue crack growth rate in metallic alloys
Dallen Andrew Hill Engineering	56 The A-10 Warthog damage tolerance and residual stresses in transition 29 The engineered residual stress implementation (ERSI) working group 28 The integrated maintenance system (IMx+)
Ana Marcia Antunes University of Sao Paulo, Brazil	78 Effects of the secondary aging heat treatment T6I4 on fracture toughness and fatigue crack growth resistance of AA7050 alloy
Joana Antunes	144 Friction stir welds with enhanced fatigue strength and life via laser peening
Takahira Aoki Department of Aeronautics and Astronautics, The University of Tokyo	21 A numerical scheme for fatigue simulation of laminated composites using CZM-XFEM
Yuichiro Aoki Japan Aerospace Exploration Agency	130 Optimal design and static load testing of tow-steered aircraft fuselage frames
Mariano Arbelo ITA - Instituto Tecnológico de Aeronáutica	146 Crack growth analysis of fiber metal laminates stiffened panels 75 Towards deriving loads spectra representing operational life: Equivalent flight profile versus single flight profiles
Hitoshi Arizono Japan Aerospace Exploration Agency	130 Optimal design and static load testing of tow-steered aircraft fuselage frames
Moriah Ausherman SAFE Inc	136 Evaluation of cold spray for aircraft repair

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