Finite element method applied to the supersonic flutter of circular cylindrical shells
- 1 January 1976
- journal article
- Published by Wiley in International Journal for Numerical Methods in Engineering
- Vol. 10 (2) , 423-435
- https://doi.org/10.1002/nme.1620100212
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- Some flutter solutions using finite elementsAIAA Journal, 1970
- Aeroelastic stability characteristics of cylindrical shells considering imperfections and edge constraint.AIAA Journal, 1969
- Application of matrix displacement methods in the study of panel flutter.AIAA Journal, 1969
- Nonlinear analysis of shells of revolution by the matrix displacement method.AIAA Journal, 1968
- Some aspects of cylindrical shell panel flutter.AIAA Journal, 1968
- Comparing theory and experiment for the supersonic flutter of circular cylindrical shells.AIAA Journal, 1967
- Direct stiffness method analysis of shells of revolution utilizing curved elements.AIAA Journal, 1966
- Supersonic flutter of circular cylindrical shells subjected to internal pressure and axial compression.AIAA Journal, 1966
- ANALYSIS OF AXISYMMETRICAL SHELLS BY THE DIRECT STIFFNESS METHODAIAA Journal, 1963
- The QR Transformation--Part 2The Computer Journal, 1962