New Design Criteria for Predicting Buckling of Cylindrical Shells under Axial Compression
- 1 October 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (10), 1062-1067
- https://doi.org/10.2514/3.59767
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
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- Buckling of imperfect elliptical cylindrical shells under axial compressionAIAA Journal, 1971
- Design criteria for axially loaded cylindrical shellsJournal of Spacecraft and Rockets, 1970
- Buckling of axisymmetric imperfect circular cylindrical shells underaxial compressionAIAA Journal, 1969
- The Effect of General Imperfections on the Buckling of Cylindrical ShellsJournal of Applied Mechanics, 1969
- Buckling under axial compression of long cylindrical shells with random axisymmetric imperfectionsQuarterly of Applied Mathematics, 1969
- The Influence of Stiffener Geometry and Spacing on the Buckling of Axially Compressed Cylindrical and Conical ShellsPublished by Springer Nature ,1969
- Buckling and Initial Postbuckling Behavior of Oval Cylindrical Shells Under Axial CompressionJournal of Applied Mechanics, 1968
- On the stability of eccentrically stiffened cylindrical shells under axial compressionInternational Journal of Solids and Structures, 1967
- Axial buckling of pressurized imperfect cylindrical shellsAIAA Journal, 1965