An Experimental Study of Boundary Layer Separation Flow Control Strategy to Low Pressure Turbine Blade at Steady Inflow State
SUN Shuang 1,2,LEI Zhi-jun 2,LI Wei 2,DONG Li-hui 1,FU Yu 1,ZHANG Qing 1
Journal of Propulsion Technology . 2016, (6): 1074 -1083 . 

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: