Finite Element Analysis of Aeroelasticity of Plates and Shells

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Date
1992
Author
Maher N. Bismarck-Nasr
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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.
URI
http://yetl.yabesh.ir/yetl/handle/yetl/109549
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