Authors Index

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Author	Manuscripts
James Walker NASA	12 NASA NDE fracture critical detectable flaw sizes history and methodology
Binwen Wang Aircraft Atrength Research Institute	86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
Mengmeng Wang Wang Aircraft Strength Research Institute of China	63 Rigid loading accelerates full-scale aircraft fatigue test
Bintuan Wang	62 Study on fatigue and crack propagation of titanium alloy laminated structure
Bin Wang	138 Opmimization of hybrid composite-metal joints
Yanfei Wang Peking University	87 High strength and ductility across size scales: 3D printed metal materials with microscale heterostructure
Xin Wang Carleton University	57 Investigation of the tensile/compressive residual stresses in AISI 4340 steel under low-cycle fatigue loading
Wandong Wang	97 Bonded prestressed method for fatigue crack repair
Russell Wanhill Retired	7 The lead crack concept history 30 years on
Jacob Warner USAF A-10 ASIP	56 The A-10 Warthog damage tolerance and residual stresses in transition 29 The engineered residual stress implementation (ERSI) working group
Sven Werner Airbus Operations GmbH	143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
Gary Whelan QuesTek Innovations LLC	33 Using digital twins to accelerate qualification and certification of fatigue critical components
Xijia Wu National Research Council Canada	10 Fatigue life prediction of metallic materials using the Tanaka-Mura-Wu model
X.R Wu AECC Beijing Institute of Aeronautical Material	23 Three-dimensional weight function analyses and stress intensity factors for general surface and corner crack emaninating from circular hole

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