Performance investigation by wind tunnel for S-shaped subsonic inlet

被引：0
|
作者：
Yuan, Ning [1 ]
Liu, Zhen-De [1 ]
Yu, Shou-Zhi [1 ]
机构：
[1] 31st Res. Inst., Beijing 100074, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2002年 / 23卷 / 01期
关键词：
Mach number - Missile propulsion - Pressure recovery coefficient - Subsonic inlet;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：24 / 26
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