Finite element analysis of aeroelasticity of plates and shells
- Instituto Tecnologico de Aeronautica, Sao Jose dos Campos (Brazil)
A review of the finite element method applied to the problem of supersonic aeroelastic stability of plates and shells is presented. The review is limited to linear models. Some new contributions in the field are presented and future trends are discussed. 105 refs., 18 figs., 6 tabs.
- Sponsoring Organization:
- USDOE
- OSTI ID:
- 433519
- Journal Information:
- Applied Mechanics Reviews, Vol. 45, Issue 12; Other Information: PBD: Dec 1992
- Country of Publication:
- United States
- Language:
- English
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