Aluminum alloys. Direct-stress fatigue strength for 17S-T aluminum alloy throughout range from ½ to 500,000,000 cycles of stress [with one reference]; by E. C. Hartmann and G. W. Stickley.
Publication Title:
Aluminum alloys. Direct-stress fatigue strength for 17S-T aluminum alloy throughout range from ½ to 500,000,000 cycles of stress [with one reference]; by E. C. Hartmann and G. W. Stickley.
Display Title:
Aluminum alloys. Direct-stress fatigue strength for 17S-T aluminum alloy throughout range from ½ to 500,000,000 cycles of stress [with one reference]; by E. C. Hartmann and G. W. Stickley.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Hartmann, E. C. and Stickley, G. W.
Date:
Sept. 1942
Publish Date ISO Format:
1942-09-01T00:00:00Z
Publication Start:
19420901
Publication End:
19420930
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
4
Publication year:
1942
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/865
Description:
cover title, 6 p. 3 pl. 4°
Notes:
(Technical notes 865.) [Processed.]
Notes:
(Technical notes 865.) [Processed.] † Distribution Made by Issuing Office.