Pages that link to "Item:Q2382058"
From MaRDI portal
The following pages link to Flight-by-flight fatigue crack growth life assessment (Q2382058):
Displaying 7 items.
- A comparison of crack growth behaviour in several full-scale airframe fatigue tests (Q882184) (← links)
- `WFD' - what is it and what's `LOV' got to do with it? (Q1016269) (← links)
- Damage tolerance analysis of a helicopter component (Q1016282) (← links)
- Fatigue crack growth history in damage tolerance design of aircraft structures (Q1016289) (← links)
- Determination of the fatigue crack-growth rate from the fractographic analysis of a specimen representing the aircraft wing skin (Q1016313) (← links)
- Aircraft life management using crack initiation and crack growth models - P-3C aircraft experience (Q2382054) (← links)
- An aging aircraft's wing under complex multiaxial spectrum loading: Fatigue assessment and repairing (Q2489084) (← links)