Effects of Diffuser Throat Length and Divergence Angle on Performance of Centrifugal Compressor with Pipe Diffuser
HAN Ge 1,2,LU Xin-gen 1,ZHAO Sheng-feng 1,YANG Cheng-wu 1,2,ZHU Jun-qiang 1
Journal of Propulsion Technology . 2014, (12): 1607 -1614 . 

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: