NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Effect of stress ratio on fatigue-crack growth in 7075-T6 and 2024-T3 aluminum-alloy specimensStress ratio effects on fatigue crack growth in sheet aluminum alloys
Document ID
19690025326
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
August 1, 1969
Subject Category
Materials, Metallic
Report/Patent Number
NASA-TN-D-5390
Report Number: NASA-TN-D-5390
Accession Number
69N34704
Funding Number(s)
CONTRACT_GRANT: 126-14-15-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available