Authors Index

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Author	Manuscripts
Michael J. Candon RMIT University	116 A prognostics and health management approach for aircraft control surface free-play
Joseph Cardinal Southwest Research Institute	37 Past, present, and future stress intensity factor solutions for crack at holes
Cauê Carvalho Engineering School of Lorena, University of São Paulo (EEL/USP)	72 Numerical and experimental analyses of the stress field ahead of fatigue cracks in laser-treated AA2198-T851 alloy
Reewanshu Chadha Federal Aviation Administration	107 Bonded repair size limit studies of representation composite wing panel
Carlos Chaves Embraer S.A.	45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies 101 Characterization of MSD in emerging metallic structures in fuselage lap joints 115 On the development of statistical knock-down factors for WFD assessment
Xianmin Chen Aircraft Atrength Research Institute	86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
Andrew Clark USAF 417 SCMS/GUEA, Landing Gear Systems	110 Tools and methods for landing gear fatigue analysis with surface treatment effects
Paul Clark Southwest Research Institute	134 A-10 implementing prognostics with the digital thread
Stephen Clay	96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
Alain Colle Bell Helicopter	120 Bell 525 Vertical Fin / Aft Fuselage and Tailboom Composite/Metallic Hybrid Certification Fatigue Testing
Gabriel Cotrim de Cesare Peinado 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
Nathan Crosby Principal Engineer	11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling
Haichao Cui	62 Study on fatigue and crack propagation of titanium alloy laminated structure
Lujun Cui	138 Opmimization of hybrid composite-metal joints
Wei Cui	26 Experimental study on the effect of different fatigue loading method on the property of metal cantilever beam

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