Research of Compressible Turbulence Model in Shock Wave/Boundary-Layer Interaction Flow at a Compression Corner
SONG You-fu 1,XU Jing-lei 1,ZHANG Yang 2,BAI Jun-qiang 2,LI Meng 1
Journal of Propulsion Technology . 2017, (2): 281 -288 . 

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: