Funder
National Natural Science Foundation of China
Ministry of Education
Reference26 articles.
1. Investigation on high angle of attack characteristics of hypersonic space vehicle;Huang;Sci. China, Technol. Sci.,2012
2. Optimization of entry-vehicle shapes during conceptual design;Dirkx;Acta Astronaut.,2014
3. A comparison of airfoil shape parameterization techniques for early design optimization;Sripawadkul,2010
4. A universal parametric geometry representation method – “CST”;Kulfan,2007
5. Aerodynamic shape optimization using the adjoint Euler equations;Straathof;Eng. Comput.,2013
Cited by
70 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献