Numerical analysis on three-dimensional flow in 2-D mixed-compression supersonic inlet

被引：0
|
作者：
Wang, G.H. [1 ]
Li, J.X. [1 ]
Cai, T.M. [1 ]
机构：
[1] Coll. of Astron., North. Polytech. Univ., Xi'an 710072, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2001年 / 22卷 / 02期
关键词：
Advection upstream splitting - Attack angle - Back pressure - Baldwin Lomax Turbulent model - Flight mach number - Flying altitude - MacCormack time splitting - Mixed compression inlet - Outlet - Supersonic inlet - Vector splitting;
D O I：
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学科分类号：
摘要：
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页码：118 / 121
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