Investigation of cold expansion of short edge margin holes with pre-existing cracks in 2024-T351 aluminium alloy
Author:
Affiliation:
1. A-10 Aircraft Structural Integrity Program; Hill AFB; UT 84056-5811 USA
2. Department of Mechanical Engineering; University of Utah; Salt Lake City UT 84112 USA
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1111/ffe.12123/fullpdf
Reference30 articles.
1. F. T. Inc 2002 FTI process specification 8101D cold expansion of holes using the standard split sleeve system and countersink cold expansion (CsCx™)
2. Brot , A. Nathan A. 1985 Increasing fatigue and fatigue crack growth lives of short edge margin holes 13th Symposium of the International Committee on Aeronautical Fatigue
3. Expansion of cracked fastener holes as a measure for extension of lifetime to repair;Buxbaum;Eng. Fract. Mech.,1987
4. Retardation of cracks emanating from fastener holes;Petrak;Eng. Fract. Mech.,1974
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