Finite Element Analysis of Aeroelasticity of Plates and Shells

Maher N. Bismarck‐Nasr

Applied Mechanics Reviews · 1992 · 99 citations · 0 references

Concepts

Abstract

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.