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Fatigue Strengths of Aircraft Materials : Axial-load Fatigue Tests on Notched Sheet Specimens of 24S-T3 and 75S-T6 Aluminum Alloys and of SAE 4130 Steel with Stress-concentration Factors of 2.0 and 4.0
Document ID
19930083340
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Grover, H J (Battelle Memorial Institute)
Bishop, S M (Battelle Memorial Institute)
Jackson, L R (Battelle Memorial Institute)
Date Acquired
August 16, 2013
Publication Date
June 1, 1951
Report/Patent Number
NACA-TN-2389
Report Number: NACA-TN-2389
Accession Number
93R12630
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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