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Effects of flight load spectrum variations on fatigue life of riveted specimens and crack propagation in sheet made of Alclad 7075-T6
Environmental effects on crack grwoth in flight-simulation tests on 2024-T3 and 7075-T6 material Supplement: Compilation of test data from an investigation on the effect of environment on crack growth under flight-simulation loading
The significance of cladding for fatigue of aluminium alloys in aircraft structures
Fracture toughness and fatigue properties of the new aluminium alloy 7475-T76
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