Type-VI and Type-V Shock-Shock Interactions on Double-Wedge Geometries Using AUSM+ on Unstructured Grid

P. Halder, K. Sinhamahapatra, Navtej Singh
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引用次数: 5

Abstract

The Euler equations are solved on unstructured triangular meshes for hypersonic flow over double-wedge geometries. The driving algorithm is an upwind biased cell centered finite volume method. AUSM+ method is used to split the fluxes. Edney (1968) studied the shock interactions by impinging an externally generated planar oblique shock on the bow shock generated by a cylinder. Depending upon the parametric conditions Edney classified the shock interactions in different types. Two interaction topologies, namely Type-VI and Type-V and the transition from Type-VI to Type-V are studied in details. Both six-shock and seven-shock configurations of Type-V interaction are presented.
非结构网格上双楔几何的vi型和v型冲击-冲击相互作用
在非结构三角形网格上求解了双楔几何高超声速流动的欧拉方程。驱动算法是一种迎风偏置单元中心有限体积法。采用AUSM+方法分割通量。Edney(1968)通过将外部产生的平面斜激波撞击圆柱体产生的弓形激波来研究激波相互作用。Edney根据参数条件将激波相互作用划分为不同类型。详细研究了Type-VI和Type-V两种交互拓扑以及Type-VI向Type-V的过渡。给出了v型相互作用的六激波和七激波构型。
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