Technical notes. 2389. 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 [with list of references]: by H. J. Grover, S. M. Bishop, 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 factors of 2.0 and 4.0 [with list of references]: by H. J. Grover, S. M. Bishop, and L. R. Jackson.
Display Title:
Technical notes. 2389. 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 [with list of references]: by H. J. Grover, S. M. Bishop, 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., Bishop, S. M., and Jackson, L. R.
Date:
June 1951
Publish Date ISO Format:
1951-06-01T00:00:00Z
Publication Start:
19510601
Publication End:
19510630
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
7
Publication year:
1951
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 64 p.+[3] leaves, il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.