Hybrid structures for concentrated load transmission in fibre composites: Initial experiments
Accelerated fatigue testing on hydraulic shaker
Development of advanced risk assessment methodologies for aircraft structures containing MSD/MED
A contribution of environmental investigations for Glare riveted joint sizing
A study of interaction and coalescence of micro surface fatigue cracks in aluminium 7050
Procedures for aircraft structural teardown analysis: Development of a best practices handbook
Airframe life extension by optimised shape reworking - Overview of DSTO developments
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
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
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
Helicopter structural integrity program of Polish Mi-24 Hind helicopters
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
Advances in crack growth modelling of 3D aircraft structures
Fracture behaviour of skin materials of civil airplane structures
Central material concept: towards aircraft wing structure insensitive to fatigue
Concept of the new A320 fatigue test
F-35 Joint strike fighter structural prognosis and health management: An overview
Pilatus PC-21 - A damage tolerant aircraft
Experimental validation of stress intensity factor solutions for the pin loaded lug
Fatigue life prediction of small notched TI-6AL-4V based on the theory of critical distance