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Interference fits and stress-corrosion failureIt is pointed out that any proper design of interference fit fastener, interference fit bushings, or stress coining processes should consider both the stress-corrosion susceptibility and fatigue-life improvement together. Investigations leading to such a methodology are discussed. A service failure analysis of actual aircraft parts is considered along with the stress-corrosion susceptibility of cold-working interference fit bushings. The optimum design of the amount of interference is considered, giving attention to stress formulas and aspects of design methodology.
Document ID
19770047802
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hanagud, S.
(Georgia Institute of Technology Atlanta, Ga., United States)
Carter, A. E.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Metallic Materials
Meeting Information
Meeting: Symposium on Stress corrosion - New approaches
Location: Montreal
Country: Canada
Start Date: June 22, 1975
End Date: June 27, 1975
Accession Number
77A30654
Funding Number(s)
CONTRACT_GRANT: NGR-11-002-169
Distribution Limits
Public
Copyright
Other

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