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

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作者
Wang, G.H. [1 ]
Li, J.X. [1 ]
Cai, T.M. [1 ]
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[1] Coll. of Astron., North. Polytech. Univ., Xi'an 710072, China
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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;
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页码:118 / 121
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