Stiffeners (aircraft). Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression [with list of references], by R. Barbré; [translation by W. L. Koch from] Ingenieur-archiv, v. 8. no. 2, 1937
Publication Title:
Stiffeners (aircraft). Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression [with list of references], by R. Barbré; [translation by W. L. Koch from] Ingenieur-archiv, v. 8. no. 2, 1937
Display Title:
Stiffeners (aircraft). Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression [with list of references], by R. Barbré; [translation by W. L. Koch from] Ingenieur-archiv, v. 8. no. 2, 1937
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Barbré, R. and Koch, W. L.
Date:
Aug. 1939
Publish Date ISO Format:
1939-08-01T00:00:00Z
Publication Start:
19390801
Publication End:
19390831
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
5
Publication year:
1939
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:8/904
Description:
cover title, 52 p. 4 pl. 4°
Notes:
(Technical memorandums 904.) [Processed.]
Notes:
(Technical memorandums 904.) [Processed.] † Distribution Made by Issuing Office.