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
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
Fatigue life evaluation on tension type fitting
Fatigue lifetime improvement of arrestment hook shanks by application of laser peening
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
Detailed strain field analyses of fatigue cracks in friction stir welded joints
Durability and damage tolerance of bonded repairs to metallic fuselage structure
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
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
Helicopter structural integrity program of Polish Mi-24 Hind helicopters
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
Fatigue & damage tolerance of hybrid materials & structures - Some myths, facts & fairytales