Pages that link to "Item:Q1271599"
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The following pages link to Mixed mode fatigue growth of curved cracks emanating from fastener holes in aircraft lap joints (Q1271599):
Displaying 3 items.
- Fracture and fatigue analysis of curved or kinked cracks near fastener holes (Q671731) (← links)
- Approximate methods for analyzing the growth of large cracks in fatigue damaged aircraft sheet material and lap joints (Q671733) (← links)
- Determination of the fatigue crack-growth rate from the fractographic analysis of a specimen representing the aircraft wing skin (Q1016313) (← links)