Technical note 1249-1463 (with omissions). 1439. Compressive strength of 24 S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having ratio of stiffener thickness to skin thickness equal to 1.00 [with list of references]; by William A. Hickman and Norris F. Dow.
Publication Title:
Compressive strength of 24 S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having ratio of stiffener thickness to skin thickness equal to 1.00 [with list of references]; by William A. Hickman and Norris F. Dow.
Display Title:
Technical note 1249-1463 (with omissions). 1439. Compressive strength of 24 S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having ratio of stiffener thickness to skin thickness equal to 1.00 [with list of references]; by William A. Hickman and Norris F. Dow.
Series Title:
Technical note 1249-1463 (with omissions).
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Hickman, William A. and Dow, Norris F.
Date:
Sept. 1947
Publish Date ISO Format:
1947-09-01T00:00:00Z
Publication Start:
19470901
Publication End:
19470930
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
4
Publication year:
1947
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/1249,etc.
Description:
cover title, 20 p. il. 2 p. of pl. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.