Experiment on thrust adjustment characteristics of fluidic nozzle throat

被引：0
|
作者：
Guo, Chang-Chao [1 ]
Yu, Xin-Yu [2 ]
Li, Bo [1 ]
Xie, Kan [1 ]
Wei, Zhi-Jun [1 ]
Wang, Ning-Fei [1 ]
机构：
[1] School of Aerospace Engineering, Beijing Institute of Technology, Beijing,100081, China
[2] Beijing Aerospace Propulsion Institute, China Aerospace Science and Technology Corporation, Beijing,100076, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2015年 / 30卷 / 04期
关键词：
D O I：
10.13224/j.cnki.jasp.2015.04.029
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：999 / 1007
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