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Fatigue of notched Ti-8Al-1Mo-1V titanium alloy at room temperature and 550 deg F /560 deg K/ with flight-by-flight loading representative of a supersonic transportLoad and temperature effects on fatigue strength of notched titanium alloy sheet for supersonic transport operation
Document ID
19690020229
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Illg, W. (NASA Langley Research Center Hampton, VA, United States)
Imig, L. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1969
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-5294
Report Number: NASA-TN-D-5294
Accession Number
69N29607
Funding Number(s)
CONTRACT_GRANT: 129-03-06-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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