Plate buckling analysis using a fully compatible finite element.
- 1 March 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (3), 527-529
- https://doi.org/10.2514/3.5142
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Hypersonic viscous drag effects on blunt slender conesAIAA Journal, 1964
- Derivation of element stiffness matrices by assumed stress distributionsAIAA Journal, 1964
- Effect of mass injection on the drag of a slender cone in hypersonic flowAIAA Journal, 1964
- BASIS FOR DERIVATION OF MATRICES FOR THE DIRECT STIFFNESS METHODAIAA Journal, 1963