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UNSTRUCTURED GRID APPROACH TO NUMERICAL SIMULATION OF VISCOUS FLOW AROUND MULTIELEMENT AIRFOILS

机译:非结构化网格方法达到多元翼型粘液流量的数值模拟

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The new direct action scheme is elaborated for approximation of two-dimensional Navier-Stokes equations on high cell aspect ratio (CAR) unstructured grids. This scheme employs the Voronoi cells as control volumes. For convective and viscous terms the scheme produces the conventional cross-type scheme on triangulated rectangular grids. The scheme approximates the additional integral representing the conservation of angular momentum. An accuracy of approximation of direct action scheme can be estimated by error functional specified at each grid point. This functional estimates the quality of unstructured grid for direct action scheme. The matrix dissipation is used for dumping odd-even instability of centered scheme. It combines the accuracy of upwind schemes with robustness and efficiency of centered ones. The construction of highly stretched Delaunay triangulations consists of two steps. At the first step nearly orthogonal structured high CAR grid is generated near bodies and wakes. At the second step this grid is smoothly continued inside the computational domain by incremental insertion technique. The calculation of turbulent viscous flows around single and multielement airfoils were performed by the presented method with Spalart-Allmaras one equation turbulence model incorporated in it.
机译:详细阐述了新的直接动作方案,用于逼近高电池纵横比(汽车)非结构化网格上的二维Navier-Stokes方程。该方案采用Voronoi细胞作为对照体积。对于对流和粘性术语,该方案在三角形矩形网格上产生传统的跨型方案。该方案近似于表示角动量守恒的附加积分。可以通过每个网格点指定的误差函数估计直接动作方案的近似的准确性。这种功能估计了直接行动方案的非结构化网格的质量。矩阵耗散用于倾倒偶然的甚至是居中方案的不稳定性。它结合了载入方案的准确性,以中心的稳健性和效率。高度拉伸的Delaunay三角结构的构造包括两个步骤。在第一步,几乎正交的结构高车网格在靠近尸体和唤醒。在第二步,通过增量插入技术,该网格在计算域内平稳地继续。通过用Spalart-Allmaras一种相结合的Spalart-Allmaras进行施用的方法,进行单一和多元素翼型的湍流粘性流动的计算。

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