Finite element analysis of composite panel flutter
β Scribed by I. Lee; M.H. Cho
- Publisher
- Elsevier Science
- Year
- 1991
- Tongue
- English
- Weight
- 612 KB
- Volume
- 39
- Category
- Article
- ISSN
- 0045-7949
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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