A review of the finite element method applied to the problem of supersonic aeroelastic stability of nonlinear flat plates, linear, and nonlinear curved plates is presented. Some new contributions in the field are given and future trends are discussed.

Issue Section:
Part 2: Dynamics and Vibration
Topics:
Aeroelasticity, Finite element analysis, Plates (structures), Shells, Finite element methods, Flat plates, Stability
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Copyright © 1996
 by American Society of Mechanical Engineers
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