Linking Riveting Process Parameters to the Fatigue Performance of Riveted Aircraft Structures

Volume: 37, Issue: 1, Pages: 130 - 137
Published: Jan 1, 2000
Abstract
The onset of widespread fatigue damage in riveted aircraft structure has been linked to sharp gradients of stress arising from contact between rivets and rivet holes. In addition, the mechanics of load transfer in lap joint structure (and resulting damage) is influenced by the through-thickness restraint offered by the installed rivet. Finally, the propagation of fatigue cracks at and around the rivet/hole interface is tied to the residual...
Paper Details
Title
Linking Riveting Process Parameters to the Fatigue Performance of Riveted Aircraft Structures
Published Date
Jan 1, 2000
Volume
37
Issue
1
Pages
130 - 137
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