Aeroelastic stability characteristics of cylindrical shells considering imperfections and edge constraint.
- 1 May 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (5) , 912-919
- https://doi.org/10.2514/3.5244
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Some aspects of cylindrical shell panel flutter.AIAA Journal, 1968
- Application of Galerkin's method to the dynamic analysis of structures.AIAA Journal, 1967
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- OSCILLATORY PRESSURES IN AN IDEALIZED BOUNDARY LAYER WITH AN APPLICATION TO THE PANEL FLUTTER OF CYLINDRICAL SHELLSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- SOME RECENT CONTRIBUTIONS TO PANEL FLUTTER RESEARCHAIAA Journal, 1963
- On Nonlinear Eiegenvalue Problems for MatricesJournal of the Society for Industrial and Applied Mathematics, 1958
- On the Numerical Solution of Characteristic Equations in Flutter AnalysisJournal of the ACM, 1958
- Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial CompressionJournal of Applied Mechanics, 1950