The Fatigue Behavior of Fastener Joints

Event
Wichita Aviation Technology Congress & Exhibition
Authors Abstract
Content
The fatigue behavior of Hilok fastener joints under constant amplitude loading has been investigated experimentally. The effects of load transfer in an unbalanced joint configuration was characterized in terms of a stress severity factor relative to the open-hole configuration. The experimental data indicates that the clamp-up forces dominate the performance of fastener joints with the open-hole fatigue life being the lower bound at the stress levels investigated. The failure modes were observed to transition from a net-section type failure across the minimum section to a fretting induced failure at some distance from the hole. The experimental data has been used to develop stress severity factors to be used as a measure of the fatigue quality of the fastener joints.
Meta TagsDetails
DOI
https://doi.org/10.4271/2008-01-2259
Pages
10
Citation
Raju, K., Smith, B., Caido, F., Gomez, C. et al., "The Fatigue Behavior of Fastener Joints," Aerospace 1(1):675-684, 2009, https://doi.org/10.4271/2008-01-2259.
Additional Details
Publisher
Published
Aug 19, 2008
Product Code
2008-01-2259
Content Type
Journal Article
Language
English