Thermal Analysis Method on Complex Regenerative Cooling Structure in Supersonic Flows
HUANG Ri-xin 1,TAN Yong-hua 2,LIU Jun-yan 1,YANG Bao-e 1
Journal of Propulsion Technology . 2019, (2): 376 -381 . 

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: