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An approach to metal fatigueCumulative fatigue damage based on investigation of fatigue limit associated with crack, crack propagation rate, and stress interaction cycle in metals
Document ID
19650015674
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Redfern, J. H. (Curtiss-Wright Corp. Caldwell, NJ, United States)
Schulte, W. C. (Curtiss-Wright Corp. Caldwell, NJ, United States)
Stulen, F. B. (Curtiss-Wright Corp. Caldwell, NJ, United States)
Date Acquired
August 2, 2013
Publication Date
June 1, 1965
Subject Category
Materials, Metallic
Report/Patent Number
NASA-CR-246
Report Number: NASA-CR-246
Accession Number
65N25275
Funding Number(s)
CONTRACT_GRANT: NAS1-3170
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CRACK PROPAGATION
STRESS CYCLE
METAL FATIGUE
FATIGUE LIFE

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