Technical notes. 2639. 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 [with list of refer ences]; by H. J. G rover. W. S. Hyler, and L. R. Jackson.
Publication Title:
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 [with list of refer ences]; by H. J. G rover. W. S. Hyler, and L. R. Jackson.
Display Title:
Technical notes. 2639. 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 [with list of refer ences]; by H. J. G rover. W. S. Hyler, and L. R. Jackson.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Grover, H. J., Hyler, W. S., and Jackson, L. R.
Date:
Feb. 1952
Publish Date ISO Format:
1952-02-01T00:00:00Z
Publication Start:
19520201
Publication End:
19520228
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
11
Publication year:
1952
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 22+[6] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.