Pages that link to "Item:Q671731"
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The following pages link to Fracture and fatigue analysis of curved or kinked cracks near fastener holes (Q671731):
Displaying 3 items.
- Analysis of cracks in aging aircraft structures, with and without composite-patch repairs (Q1207273) (← links)
- Mixed mode fatigue growth of curved cracks emanating from fastener holes in aircraft lap joints (Q1271599) (← links)
- Theoretical modeling of crack arrest by inserting interference fit fasteners (Q1412696) (← links)