Effects of side-inlet angle on the performance of boron-based propellant ducted rocket

被引：0
作者：
Li, Ze-Yong [1 ]
Hu, Jian-Xin [1 ]
Xia, Zhi-Xun [1 ]
Wang, Zhen-Guo [1 ]
机构：
[1] College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
来源：
Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology | 2008年 / 30卷 / 02期
关键词：
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页码：1 / 4
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