Elastic Instability of a Cylindrical Shell Under Arbitrary Circumferential Variation of Axial Stress
- 1 November 1960
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (11) , 854-858
- https://doi.org/10.2514/8.8776
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Thermal Buckling of Circular Cylindrical Shells Under Circumferential Temperature GradientsJournal of the Aerospace Sciences, 1959
- A Simple Method of Matric Structural Analysis: Part II-Effects of Taper and Consideration of CurvatureJournal of the Aeronautical Sciences, 1957
- A Simple Method of Matric Structural AnalysisJournal of the Aeronautical Sciences, 1957