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Investigation of fatigue crack growth in Ti- 8Al-1Mo-1V /duplex-annealed/ specimens having various widthsAxial-load fatigue crack propagation tests on duplex annealed titanium alloy specimens having various widths
Document ID
19670009636
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hudson, C. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1967
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3879
Report Number: NASA-TN-D-3879
Accession Number
67N18965
Funding Number(s)
CONTRACT_GRANT: 126-14-03-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TITANIUM ALLOY
FATIGUE TEST
CRACK PROPAGATION

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