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Fatigue-crack-propagation and fracture- toughness characteristics of 7079 aluminum- alloy sheets and plates in three aged conditionsFatigue crack propagation and fracture toughness characteristics of 7079 aluminum alloys in underage, peak age, and overaged conditions
Document ID
19680006007
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Porter, T. R. (Boeing Co. Renton, WA, United States)
Smith, S. H. (Boeing Co. Renton, WA, United States)
Sump, W. D. (Boeing Co. Renton, WA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1968
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-996
Report Number: NASA-CR-996
Accession Number
68N15476
Funding Number(s)
CONTRACT_GRANT: NAS1-6474
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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