30 Years of damage tolerance - Have we got it right?
A case study of multiple-site fatigue crack growth in the F-18 Hornet bulkhead
Accelerated fatigue testing on hydraulic shaker
A contribution of environmental investigations for Glare riveted joint sizing
Advances in crack growth modelling of 3D aircraft structures
Airframe life extension by optimised shape reworking - Overview of DSTO developments
An analytical model for load transfer in a mechanically fastened, double-lap joint
An experimental approach to investigate detailed failure mechanisms in fibre metal laminates
An experimental investigation on the fatigue performance of riveted lap joints
Arall and Glare FML's: Three decades of bridging the gap between theory and operational practice
A study of interaction and coalescence of micro surface fatigue cracks in aluminium 7050
A test concept for future aircraft fuselage panels
Bonded composite patch to repair metallic structures: Disbond propagation testing and modelling
Bonded repair for fuselage damage: An overall benefit to commercial aviation
Central material concept: towards aircraft wing structure insensitive to fatigue
Compilation of damage findings from multiple recent teardown analysis programs
Concept of the new A320 fatigue test
Crack growth in fiber metal laminates under variable amplitude loading
Damage tolerance philosophy for bonded aircraft structures