Buckling of axially compressed cylindrical shells with ring-stiffened edges.
- 1 October 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (10) , 1859-1862
- https://doi.org/10.2514/3.3800
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Primary and Afterglow Emission from Low-Temperature Gaseous Nitrogen Excited by Fast ElectronsThe Journal of Chemical Physics, 1966
- INFLUENCE OF IMPERFECTIONS AND EDGE RESTRAINT ON THE BUCKLING OF AXIALLY COMPRESSED CYLINDERSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Computer analysis of asymmetric free vibrations of ring-stiffened orthotropic shells of revolution.AIAA Journal, 1965
- The buckling of a free edge of an axially-compressed circular cylindrical shellQuarterly of Applied Mathematics, 1962
- ELECTRON BEAM FLUORESCENCE PROBE FOR MEASURING THE LOCAL GAS DENSITY IN A WIDE FIELD OF OBSERVATIONCanadian Journal of Physics, 1958
- Electron Shadowgraphs and Afterglow Pictures of Gas Jets at Low DensitiesJournal of Applied Physics, 1953