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基于结构动力学方法的气动弹性分析
引用本文:周文博,陈力奋,杨琼梁,唐国安.基于结构动力学方法的气动弹性分析[J].振动与冲击,2011,30(4):135-138.
作者姓名:周文博  陈力奋  杨琼梁  唐国安
作者单位:复旦大学力学与工程科学系,上海 200433
基金项目:国家自然科学基金资助项目
摘    要:摘 要:对于气动与弹性的耦合模型,给出气动力的频域公式,并表示成有理多项式,通过等价的变换,能够推导出与结构动力学方程完全相似的、关于求解变量的二阶常微分方程组。于是,可以在计算结构动力学框架下实现气动弹性问题的分析和计算。此方法将通用计算结构动力学程序的功能与试验或数值分析得到的气动力模型相结合,简化了气动弹性的耦合分析、提高计算效率。

关 键 词:气动弹性    非定常气动力    计算结构动力学  
收稿时间:2009-10-28
修稿时间:2010-3-2

Aeroelastic analysis based on computational structural dynamic method
ZHOU Wen-bo,CHEN Li-feng,YANG Qiong-liang,TANG Guo-an.Aeroelastic analysis based on computational structural dynamic method[J].Journal of Vibration and Shock,2011,30(4):135-138.
Authors:ZHOU Wen-bo  CHEN Li-feng  YANG Qiong-liang  TANG Guo-an
Affiliation:Department of Mechanics and Engineering Science, Fudan University, Shanghai 200433
Abstract:To simplify aeroelastic analysis utilizing the general CSD program,an approach to transform an aerodynamic model to the desired formation was presented here.For a flow-flexible structure coupled model,the aerodynamic force was given in the frequency-domain,and then could be expressed as rational polynomials.Through the equivalent transformation,the aerodynamic model could be deduced to a second order ordinary differential equation.Then,aeroelastic analysis could be achieved under the framework of computatio...
Keywords:aeroelasticity  unsteady aerodynamics  structural dynamics  
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