Finite-Element Solution of the Supersonic Flutter of Conical Shells
- 1 October 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (10) , 1148-1150
- https://doi.org/10.2514/3.61291
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Finite-element panel flutter in three-dimensional supersonic unsteady potential flowAIAA Journal, 1977
- Finite element method applied to the flutter of two parallel elastically coupled flat platesInternational Journal for Numerical Methods in Engineering, 1977
- Aeroelasticity of Plates and ShellsJournal of Applied Mechanics, 1976
- Orthogonality Check and Correction of Measured ModesAIAA Journal, 1976
- Finite element method applied to the supersonic flutter of circular cylindrical shellsInternational Journal for Numerical Methods in Engineering, 1976
- Discrete element approach to flutter of skew panels with in-plane forces under yawed supersonic flowAIAA Journal, 1970
- Some flutter solutions using finite elementsAIAA Journal, 1970
- Orthogonalization of measured modes and calculation of influence coefficients.AIAA Journal, 1969