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壁板边界松驰下颤振非线性动力特性分析
引用本文:肖艳平,杨翊仁,叶露.壁板边界松驰下颤振非线性动力特性分析[J].振动与冲击,2014,33(3):157-161.
作者姓名:肖艳平  杨翊仁  叶露
作者单位:1. 中国民航飞行学院飞行技术学院,四川,广汉 618307 2. 西南交通大学力学与工程学院,四川,成都 610031
基金项目:中央高校基本科研业务费专项资金资助(2010Z707)项目;中国民航飞行学院面上项目(J2010-77)
摘    要:采用分离变量法和伽辽金法建立三维壁板的非线性气动弹性运动方程,用一阶活塞理论模拟壁板所受的气动力,分析了壁板的颤振边界及稳定性,进而取边界松弛因子,动压和面内力为分叉参数,研究壁板颤振时的分叉及混沌等复杂动力学特性。计算结果表明:边界松弛下壁板颤振系统表现出丰富的动力学行为,其分叉特性很复杂。随着边界松弛因子的增大, 静态稳定区域缩小,而屈曲和混沌区域增大,系统稳定性降低。

关 键 词:壁板  颤振  活塞理论  边界条件  分叉  
收稿时间:2012-9-28
修稿时间:2013-3-11

Nonlinear Dynamic Analysis of Panel Flutter on Boundary Conditions Relaxation
Xiao Yanping,Yang Yiren,Ye Lu.Nonlinear Dynamic Analysis of Panel Flutter on Boundary Conditions Relaxation[J].Journal of Vibration and Shock,2014,33(3):157-161.
Authors:Xiao Yanping  Yang Yiren  Ye Lu
Affiliation:1. School of Flight Technology, Civil Aviation Flight University of China, Guanghan, Sichuan, 618307 , China2. School of Mechanics and Engineering , Southwest Jiaotong University , Chengdu ,Sichuan,610031 , China
Abstract:An investigation on nonlinear dynamics of panel with boundary condition relaxation is carried out in this paper. The flutter differential equations of a three-dimension panel are set up by using separation of variables and Galerkin method. The first piston theory is employed to calculate the aerodynamic load on the panel. At first, the flutter boundary and stability for the flat pane are analyzed. Then Using the temperature, dynamic pressure and in-plane load as bifurcation parameters, their bifurcations and chaos behaviors were studied. The results demonstrate the rich dynamic behaviors of the panel with boundary condition relaxation and complex dynamic characteristic with variation of bifurcation parameters. Both the buckled region and chaotic region increase as the relaxation of boundary conditions and the stability of system decreases.
Keywords:panelflutterpiston theoryboundary conditionbifurcation
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