空气动力学学报2001，Vol.19Issue(1)：97-102,6.
基于欧拉方程的机翼设计方法及应用
Wing design method and application based on Euler equations
摘要
Abstract
In this thesis, Based on three dimensional wing inverse designtheory proposed by Takanashi, a wing inverse design method based on Euler equation and “direct-inverse iteration，residual-correction “concept is presented. The O-O mesh around wing is generated by the improved transfinite method. The Euler equation analysis method is used to resolve flow field. The method has been applied to the low speed wing design for a unmanned aircraft and to a supercritical wing design successfully关键词
机翼设计/正-反迭代/余量修正/Euler方程/无限插值分类
航空航天引用本文复制引用
杨旭东,乔志德,朱兵..基于欧拉方程的机翼设计方法及应用[J].空气动力学学报,2001,19(1):97-102,6.
