Inverse design of a curved wall compression hypersonic inlet based on Genetic Algorithms
苏纬仪,张堃元,金志光
Journal of Propulsion Technology . 2011, (5): 601 -605 . 

Founded in 1980
Competent department: China Aerospace Science and Industry Group Co., Ltd
Sponsor: China Aerospace Science and industry group No.31 Research Institute
ISSN: 1001-4055
Journal of Propulsion Technology © 2021
E-mail: tjjs@sina.com
www.tjjscasic.com
Support: 010-62662699
Access Statistics

General Visit:

Visit Today:

Currently Online: