Pages that link to "Item:Q1016313"
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The following pages link to Determination of the fatigue crack-growth rate from the fractographic analysis of a specimen representing the aircraft wing skin (Q1016313):
Displaying 4 items.
- A comparison of crack growth behaviour in several full-scale airframe fatigue tests (Q882184) (← 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)
- Flight-by-flight fatigue crack growth life assessment (Q2382058) (← links)