Finite Element Analysis of Aeroelasticity of Plates and Shells

[+] Author and Article Information
Maher N. Bismarck-Nasr

Divisão de Engenharia Aeronáutica, Instituto Tecnológico de Aeronáutica, Centro Técnico Aeroespacial, São José dos Campos, SP, 12228-900, Brazil

Appl. Mech. Rev 45(12), 461-482 (Dec 01, 1992) (22 pages) doi:10.1115/1.3119783 History: Online April 30, 2009


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.

Copyright © 1992 by American Society of Mechanical Engineers
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