USAAVLABS technical reports. 69-62. Effect of test machine extenslonal rigidity on initial buckling load of unreinforeed circular cylindrical shells in axial compression; by S. C. Bailey [and] W. H. Horton.
Publication Title:
Effect of test machine extenslonal rigidity on initial buckling load of unreinforeed circular cylindrical shells in axial compression; by S. C. Bailey [and] W. H. Horton.
Display Title:
USAAVLABS technical reports. 69-62. Effect of test machine extenslonal rigidity on initial buckling load of unreinforeed circular cylindrical shells in axial compression; by S. C. Bailey [and] W. H. Horton.
Series Title:
USAAVLABS technical reports.
Corporate Agency Authors:
Army Department and Defense Dept.
Sort Author:
Army Department
Authors:
Bailey, S. C. and Horton, W. H.
Author place:
Washington, DC
Author zip:
20310
Date:
Nov. 1971
Publish Date ISO Format:
1971-11-01T00:00:00Z
Publication Start:
19711101
Publication End:
19711130
Corporate/Agency Author:
Army Department
Publication month:
2
Publication year:
1971
SuDoc number:
D 117.8/2:(nos.)
Description:
cover title, [1]+xi+59+[2] p. il. 4°
Notes:
[Task 1F162202A17002. Contract DA 44-177-AMC-115(T), prepared by Stanford University, Department of Aeronautics and Astronautics, Stanford, Calif.] and [Eustis Directorate, Army Air Mobility Research and Development Laboratory, Fort Eustis, Va.)
Notes:
[Eustis Directorate, Army Air Mobility Research and Development Laboratory, Fort Eustis, Va.) ‡ Official Use. Not Available.