Finite elements applied to panel flutter.
- 1 December 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (12) , 2267-2270
- https://doi.org/10.2514/3.4422
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Consistent matrix formulations for structural analysis using finite-element techniques.AIAA Journal, 1965
- Errata: "Plastic Buckling of Axially Compressed Cylindrical Shell"AIAA Journal, 1965
- Distributed mass matrix for plate element bendingAIAA Journal, 1965
- A Finite Element Approach to Plate Vibration ProblemsJournal of Mechanical Engineering Science, 1965
- Plastic buckling of axially compressed cylindrical shellsAIAA Journal, 1965
- THE FINITE ELEMENT METHOD FOR ANALYSIS OF ELASTIC ISOTROPIC AND ORTHOTROPIC SLABS.Proceedings of the Institution of Civil Engineers, 1964