Finite element analysis of Supersonic panel flutter
- 1 January 1973
- journal article
- research article
- Published by Wiley in International Journal for Numerical Methods in Engineering
- Vol. 7 (3) , 379-394
- https://doi.org/10.1002/nme.1620070313
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Error bounds for eigenvalue analysis by elimination of variablesJournal of Sound and Vibration, 1971
- Kinematically consistent unsteady aerodynamic coefficients in supersonic flowInternational Journal for Numerical Methods in Engineering, 1970
- Some flutter solutions using finite elementsAIAA Journal, 1970
- A conforming finite element for plate bendingInternational Journal of Solids and Structures, 1968
- Finite elements applied to panel flutter.AIAA Journal, 1967
- Theoretical considerations of panel flutter at high supersonic Mach numbers.AIAA Journal, 1966
- Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0.AIAA Journal, 1965
- Inadequacy of nodal connections in a stiffness solution for plate bendingAIAA Journal, 1965
- SOME RECENT CONTRIBUTIONS TO PANEL FLUTTER RESEARCHAIAA Journal, 1963
- Das Iterationsverfahren bei nicht selbstadjungierten linearen EigenwertaufgabenMathematische Zeitschrift, 1944