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
Melanie DUCOFFE Airbus Operations SAS, France	119 Enabling the journey towards Condition Based Maintenance for Airframe
Derk Daverschot Airbus Operations GmbH	113 Crack bridging effect in hybrid reinforced fuselage structure 119 Enabling the journey towards Condition Based Maintenance for Airframe 42 How the holistic approach for GLARE development still brings benefits
Zvi Deutch	96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
Rueben Dinakar Airbus India	143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
BL Dinesh National Aerospace Laboratories, Bangalore, India	143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
Juliana Diniz Mattos ITA - Instituto Tecnológico de Aeronáutica	75 Towards deriving loads spectra representing operational life: Equivalent flight profile versus single flight profiles
Éric Dionne National Research Council of Canada	25 Probabilistic lifing of a second oversize hole modification
Éric Dionne National Research Council of Canada	59 EXPERIMENTAL STRENGTH AND FATIGUE ASSESSMENT OF A DISBONDED F/A-18 A/B/C/D INNER WING STEP LAP JOINT
Ben Dixon Defence Science and Technology Group	19 The outcomes of research into nucleation and small fatigue crack growth in aluminium alloy 7085-T7452
Dengke Dong Aircraft Atrength Research Institute	86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
Hongna Dui	3 Optimization of selecting strain measurement locations for distributed load recovery from strain measurements

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