NASA technical notes. D-111. Fatigue strengths of aircraft materials: Axial-load fatigue tests on edgenotched sheet specimens of 2024-T3 and 7075-T6 aluminum alloys and of SAE 4130 steel with notch radii of 0.004 and 0.070 inch [with list of references]; by H. J. Grover, W. S. Hyler, and L. R. Jackson.
Publication Title:
Fatigue strengths of aircraft materials: Axial-load fatigue tests on edgenotched sheet specimens of 2024-T3 and 7075-T6 aluminum alloys and of SAE 4130 steel with notch radii of 0.004 and 0.070 inch [with list of references]; by H. J. Grover, W. S. Hyler, and L. R. Jackson.
Display Title:
NASA technical notes. D-111. Fatigue strengths of aircraft materials: Axial-load fatigue tests on edgenotched sheet specimens of 2024-T3 and 7075-T6 aluminum alloys and of SAE 4130 steel with notch radii of 0.004 and 0.070 inch [with list of references]; by H. J. Grover, W. S. Hyler, and L. R. Jackson.
Series Title:
NASA technical notes.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Grover, H. J., Hyler, W. S., and Jackson, L. R.
Date:
Sept. 1959
Publish Date ISO Format:
1959-09-01T00:00:00Z
Publication Start:
19590901
Publication End:
19590930
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
4
Publication year:
1959
SuDoc number:
NAS 1.14:D-(nos.)
Description:
cover title, 25 p. + [3] leaves, il. 4°
Notes:
[Processed.]
Notes:
[Processed.] Φ For Sale by OTS, Commerce Dept. Paper, 75c.