Numerical analysis of rotationally symmetric shells under transient loadings
- 1 April 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (4) , 637-643
- https://doi.org/10.2514/3.6241
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- Symmetric Bending of the General Shell of Revolution by Finite Difference MethodsJournal of Mechanical Engineering Science, 1961
- A New Derivation of the Equations for the Deformation of Elastic ShellsAmerican Journal of Mathematics, 1941