空气动力学学报2012，Vol.30Issue(5)：653-657,674,6.
基于 Euler 方程的返回舱气动外形优化设计方法研究
The study of the reentry capsule shape optimization method based on the solving of the Euler equations
李治宇 1杨彦广 1袁先旭 1唐志共1
作者信息
- 1. 中国空气动力研究与发展中心,四川绵阳 621000
- 折叠
摘要
Abstract
The work in this paper is based on the optimization software, using the exactly optimization technique. The hypersonic aerodynamic performance is calculated by numerically solving the Euler equations and the maximum surface heat flux is calculated by solving the Fay-Riddell equation. To test our method, the CTV is optimized. The Spaceship reentry capsule has been optimized as a particular instance. This research work can be as the groundwork for the reentry capsule optimization.关键词
返回舱/优化设计/Euler方程/遗传算法Key words
reentry capsule/ optimization/ Euler equations/ Genetic Algorithm分类
航空航天引用本文复制引用
李治宇,杨彦广,袁先旭,唐志共..基于 Euler 方程的返回舱气动外形优化设计方法研究[J].空气动力学学报,2012,30(5):653-657,674,6.
