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
Detailed strain field analyses of fatigue cracks in friction stir welded joints
Durability and damage tolerance of bonded repairs to metallic fuselage structure
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