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.

Issue Section:
Review Articles
Topics:
Aeroelasticity, Finite element analysis, Plates (structures), Shells, Finite element methods, Stability
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Copyright © 1992
 by American Society of Mechanical Engineers
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