Comparison of theory and experiment for nonlinear flutter of loaded plates
- 1 November 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (11) , 2022-2030
- https://doi.org/10.2514/3.6041
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Application of matrix displacement methods in the study of panel flutter.AIAA Journal, 1969
- Modal equations for the nonlinear flexural vibrations of a cylindrical shellInternational Journal of Solids and Structures, 1968
- Nonlinear flutter of loaded platesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Flutter of simply supported, parallelogrammic, flat panels in supersonic flow.AIAA Journal, 1967
- Matrix displacement analysis of plates and shellsArchive of Applied Mechanics, 1966
- Flutter of Thin Plates under Combined Shear and Normal Edge ForcesAIAA Journal, 1963
- THE EFFECT OF A CAVITY ON PANEL VIBRATIONAIAA Journal, 1963
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957