USAAVLABS technical reports. 69-83. Unified theory for bending and buckling of sandwich shells—application to axially compressed, circular cylindrical shells [with list of literature cited]; by G. Bartelda, J. Mayers.
Publication Title:
Unified theory for bending and buckling of sandwich shells—application to axially compressed, circular cylindrical shells [with list of literature cited]; by G. Bartelda, J. Mayers.
Display Title:
USAAVLABS technical reports. 69-83. Unified theory for bending and buckling of sandwich shells—application to axially compressed, circular cylindrical shells [with list of literature cited]; by G. Bartelda, J. Mayers.
Series Title:
USAAVLABS technical reports.
Corporate Agency Authors:
Army Department and Defense Dept.
Sort Author:
Army Department
Authors:
Bartelda, G. and Mayers, J.
Author place:
Washington, DC
Author zip:
20310
Date:
July 1971
Publish Date ISO Format:
1971-07-01T00:00:00Z
Publication Start:
19710701
Publication End:
19710731
Corporate/Agency Author:
Army Department
Publication month:
6
Publication year:
1971
SuDoc number:
D 117.8/2:(nos.)
Description:
[1]+xiv+107+[2] p. il. 4°
Notes:
[Task 1F162204A17002, contract DA 44-177-AMC-115(T). Prepared by Department of Aeronautics and Astronautics, Stanford University. Stanford. Calif.] and (Eustis Directorate, U.S. Army Air Mobility Research and Development Laboratory, Fort Eustis, Va.)
Notes:
(Eustis Directorate, U.S. Army Air Mobility Research and Development Laboratory, Fort Eustis, Va.) ‡ Official Use. Not Available.