NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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 factor of 1.5
Document ID
19930083512
Document Type
Other
Authors
Grover, H J
(Battelle Memorial Institute)
Hyler, W S
(Battelle Memorial Institute)
Jackson, L R
(Battelle Memorial Institute)
Date Acquired
August 16, 2013
Publication Date
February 1, 1952
Report/Patent Number
NACA-TN-2639
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 19930083512.pdf STI
No Preview Available