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A damage tolerance study conducted with structure relevant specimens
The B2000 linear buckling processor
A CAD-system for the design of stiffened panels in wing box structures
Flight simulation environmental fatigue crack propagation in 2024-T3 and 7475-T761 aluminium
Evaluation of non-destructive inspection methods applied to milled step-down areas
Effects of flight load spectrum variations on fatigue life of riveted specimens and crack propagation in sheet made of Alclad 7075-T6
Aluminium alloys for advanced structural applications in transport aircraft
The effect of sheet thickness on flight simulation fatigue crack propagation in 2024-T3, 7475-T761 and mill annealed Ti-6A1-4V
Flight simulation fatigue crack propagation evaluation of candidate lower wing skin materials with particular consideration of spectrum truncation
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