Pages that link to "Item:Q2489084"
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The following pages link to An aging aircraft's wing under complex multiaxial spectrum loading: Fatigue assessment and repairing (Q2489084):
Displaying 6 items.
- Fatigue, residual strength and non-destructive tests of an aging aircraft's wing detail (Q1016306) (← links)
- Aircraft life management using crack initiation and crack growth models - P-3C aircraft experience (Q2382054) (← links)
- Flight-by-flight fatigue crack growth life assessment (Q2382058) (← links)
- Fatigue test of lightweight composite wing structure (Q2506554) (← links)
- Fatigue crack growth of bonded composite repairs in gigacycle regime (Q2506577) (← links)
- (Q3731268) (← links)