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Wall boundary conditions for inviscid compressible flows on unstructured meshes

机译:非结构网格上无粘性可压缩流的壁边界条件

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In this paper we revisit the problem of implementing wall boundary conditions for the Euler equations of gas dynamics in the context of unstructured meshes. Both (a) strong formulation, where the zero normal velocity on the wall is enforced explicitly and (b) weak formulation, where the zero normal velocity on the wall is enforced through the flux function are discussed. Taking advantage of both approaches, mixed procedures are defined. The new wall boundary treatments are accurate and can be applied to any approximate Riemann solver. Numerical comparisons for various flow regimes, from subsonic to supersonic, and for various approximate Riemann solvers point out that the mixed boundary procedures drastically improve the accuracy.
机译:在本文中,我们将重新讨论在非结构化网格环境中为气体动力学的欧拉方程实施壁边界条件的问题。讨论了(a)强公式(其中显式强制执行壁上的零法向速度)和(b)弱公式(其中通过通量函数强制执行在壁上的零法向速度)。利用这两种方法,可以定义混合过程。新的墙边界处理非常精确,可以应用于任何近似的黎曼求解器。从亚音速到超音速,以及各种近似的黎曼求解器,对各种流动状态的数值比较都指出,混合边界过程极大地提高了精度。

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