DEFLECTIONS OF AN INFLATED CIRCULAR-CYLINDRICAL CANTILEVER BEAM
- 1 July 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (7) , 1652-1655
- https://doi.org/10.2514/3.1873
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Stability of a Console Cylindrical Shell Under Bending by a Transverse Force With Twisting and Internal PressureARS Journal, 1961
- The Stability of Thin-Walled Unstiffened Circular Cylinders Under Axial Compression Including the Effects of Internal PressureJournal of the Aeronautical Sciences, 1957
- Buckling of Thin-Walled Circular Cylinders Under Axial Compression and Internal PressureJournal of the Aeronautical Sciences, 1957