| Author |
Manuscripts |
Melanie DUCOFFE
Airbus Operations SAS, France
|
119 Enabling the journey towards Condition Based Maintenance for Airframe
|
Derk Daverschot
Airbus Operations GmbH, Germany
|
42 How the holistic approach for GLARE development still brings benefits
113 Crack bridging effect in hybrid reinforced fuselage structure
119 Enabling the journey towards Condition Based Maintenance for Airframe
|
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
|
25 Probabilistic lifing of a second oversize hole modification
|
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
|
