On separating the effect of corrosion on inter-lamellar fatigue on thin sheet AA7079-T6
Three dimensional crack growth prediction
Hybrid structure solution for the A400M wing attachment frames
Glare teardowns from the MegaLiner Barrel (MLB) fatigue test
First diamond: `Damage tolerance' for the structural honeymoon
Damage tolerance philosophy for bonded aircraft structures
High cycle fatigue of laser beam deposited Ti-6Al-4V and inconel 718
Bonded repair for fuselage damage: An overall benefit to commercial aviation
Properties of fatigue crack propagation in friction stir welded 2024-T3 aluminum alloy
Fatigue and damage tolerance aspects of metal laminates
Structural integrity of a wing upper skin with exfoliation corrosion
On the crack growth behaviour under simple compressive loads of 2024-T3 aluminium alloy
Practical applications of improvements in FML crack bridging theory
A test concept for future aircraft fuselage panels
Towards automated flight-maneuver-specific fatigue analysis
A case study of multiple-site fatigue crack growth in the F-18 Hornet bulkhead
An experimental investigation on the fatigue performance of riveted lap joints
Design and testing of advanced composite load introduction structure for aircraft high lift devices
Enhanced teardown of ex-service F/A-18A/B/C/D centre fuselages
Marker loads for quantitative fractography of fatigue cracks in aerospace alloys
Helicopter structural integrity program of Polish Mi-24 Hind helicopters
Fatigue & damage tolerance of hybrid materials & structures - Some myths, facts & fairytales
Introduction to service of an artificial neural network based fatigue monitoring system
Bonded composite patch to repair metallic structures: Disbond propagation testing and modelling
An experimental approach to investigate detailed failure mechanisms in fibre metal laminates
Evaluation, modification and damage tolerance of an in-service aircraft critical area
Substantiations of an airborne composite radome mounted on an aircraft dome
Delamination growth at interfaces in hybrid materials and structures under various opening modes
Development of fatigue life monitoring of RMAF fighter airplanes
An analytical model for load transfer in a mechanically fastened, double-lap joint
Fatigue crack growth in thick plate 7050 aluminum
Crack growth in fiber metal laminates under variable amplitude loading
Arall and Glare FML's: Three decades of bridging the gap between theory and operational practice
Investigation on the design of bonded structures for increased damage tolerance
Low cycle lifetime prediction of AL2024 alloy
Compilation of damage findings from multiple recent teardown analysis programs
30 Years of damage tolerance - Have we got it right?
Survey of structural repairs and alterations in transport category airplanes