Finite element analysis of Supersonic panel flutter
β Scribed by G. Sander; C. Bon; M. Geradin
- Publisher
- John Wiley and Sons
- Year
- 1973
- Tongue
- English
- Weight
- 760 KB
- Volume
- 7
- Category
- Article
- ISSN
- 0029-5981
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
In this article the classical analysis of the static pressure e!ect on #uttering panels is extended to cases of pulse and step excitations. A high order "nite-element methodology is applied within the non-linear elastic, linear aerodynamic theories and a dynamic analysis is performed on a reference
## Abstract This paper presents the results of an aeroelastic optimization study. In this study the weight of a large aspect ratio panel immersed in high Mach number supersonic flow is minimized subject to the requirement that a critical aeroelastic parameter for flutter be held within specified li