Ideal Thermodynamic Cycle and Performance Analysis of 2-Stage Pulse Detonation Engine
张强,何立明,陈鑫,荣康
Journal of Propulsion Technology . 2012, (4): 499 -504 . 

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: