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Fracture toughness of wide 2014-T6 aluminum sheet at -320 deg FEffect of aluminum alloy test specimen size on fracture toughness at high stress ratios
Document ID
19670018968
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Orange, T. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1967
Subject Category
Materials, Metallic
Report/Patent Number
NASA-TN-D-4017
Report Number: NASA-TN-D-4017
Accession Number
67N28297
Funding Number(s)
CONTRACT_GRANT: 124-08-08-19-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STRESS AND LOAD
ALUMINUM ALLOY
FRACTURE TOUGHNESS

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