Supersonic flutter of circular cylindrical heterogeneous orthotropic thin panels of finite length
- 1 November 1968
- journal article
- Published by Elsevier in Journal of Sound and Vibration
- Vol. 8 (3) , 494-512
- https://doi.org/10.1016/0022-460x(68)90253-8
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Supersonic flutter of a circular cylindrical shell of finite length in an axisymmetrical modeInternational Journal of Solids and Structures, 1965
- Nonlinear theories for thin shellsQuarterly of Applied Mathematics, 1963
- The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical ShellsJournal of the Aerospace Sciences, 1961
- Supersonic Panel Flutter of a Cylindrical Shell of Finite LengthJournal of the Aerospace Sciences, 1961
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956