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基于变域变分有限元的翼型反设计
引用本文:陈池,刘高联.基于变域变分有限元的翼型反设计[J].空气动力学学报,2004,22(4):443-446,469.
作者姓名:陈池  刘高联
作者单位:上海大学、上海市应用数学和力学研究所,上海,200072
基金项目:国家自然科学基金资助项目(编号:50136030).
摘    要:反问题作为一种自由(未知)边界问题近年来得到了广泛的研究。变域变分通过把自由边界结合在变分泛函中,使其与求解流场的控制方程结合起来,从而自由边界求解和流场分析可以完全耦合进行。本文采用变域变分和可变形有限元来设计可压缩和不可压缩翼型,计算显示即使在初始翼型的一侧为三角形时仍能得到满意的结果。文中还采用了两种计算网格(H型和O型)来设计翼型,比较了它们的精度,计算表明本方法完全能用于翼型的反设计。

关 键 词:变分  自由边界  泛函  求解  不可压缩  反问题  控制方程  翼型  反设计  流场分析
文章编号:0258-1825(2004)04-0443-05

Inverse design of airfoil based on variable-domain variational FEM
CHEN Chi,LIU Gao-lian.Inverse design of airfoil based on variable-domain variational FEM[J].Acta Aerodynamica Sinica,2004,22(4):443-446,469.
Authors:CHEN Chi  LIU Gao-lian
Abstract:Inverse problems are widely discussed nowadays. Variable-domain variational principles can couple the variable domain into functional, which makes it possible to calculate the flow field with the variable-domain simultaneously. The variable-domain variational principle and variable finite element method are used hereinafter to design compressible and incompressible foils. The results show that even if the initial foil type is a triangle, it can still lead to good results. Furthermore, two grid types (H and O) are used in the calculation, which shows that the O-type grid can get better results. It can be seen from all the results that the present method is correct and highly applicable.
Keywords:Inverse design  airfoil  finite element method  variable-domain variational calculus
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