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飞行器壁板颤振的无限维非线性分析
引用本文:郭乾荣.飞行器壁板颤振的无限维非线性分析[J].航空学报,1988,9(11):554-577.
作者姓名:郭乾荣
作者单位:上海交通大学
摘    要: 一、无限维Hopf分叉定理和中心不变流形定理 由于偏微分方程的矢量场(在任一适当的Banach空间中)常常不是光滑函数,Marsden-McCracken利用(相)流的光滑性提出了流的Hopf分叉定理和中心流形定理。这里的流都是半(相)流,也就是半群。

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收稿时间:1987-06-27;

AN INFINITE DIMENSIONAL NONLINEAR ANALYSIS OF PANEL FLUTTER
Guo Qianrong.AN INFINITE DIMENSIONAL NONLINEAR ANALYSIS OF PANEL FLUTTER[J].Acta Aeronautica et Astronautica Sinica,1988,9(11):554-577.
Authors:Guo Qianrong
Institution:Shanghai Jiaotong University
Abstract:The equation of motion of panel flutter is a nonlinear partial differential equation. It is usually treated approximately by a system of ordinary differential equations. In this paper the author makes an infinite dimensional nonlinear analysis for panel flutter; ( 1 ) using the infinite dimensional Hopf bifurcation theory to find the bifurcation values, and ( 2 ) using center manifold theory to determine the stability of the bifurcating periodic motions.
Keywords:panel flutter  hopf bifurcation  center manifold theory  
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