Pages that link to "Item:Q882184"
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The following pages link to A comparison of crack growth behaviour in several full-scale airframe fatigue tests (Q882184):
Displaying 6 items.
- `WFD' - what is it and what's `LOV' got to do with it? (Q1016269) (← links)
- Damage tolerance demonstration testing for the Australian F/A-18 (Q1016276) (← links)
- Fatigue crack growth history in damage tolerance design of aircraft structures (Q1016289) (← links)
- 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)