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

机译:非结构网格方法在多元素翼型绕流中的数值模拟

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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作用方案,以在高单元长宽比(CAR)非结构化网格上近似二维Navier-Stokes方程。该方案采用Voronoi细胞作为控制体积。对于对流和粘性项,该方案在三角矩形网格上生成常规的交叉类型方案。该方案近似表示表示角动量守恒的附加积分。可以通过在每个网格点指定的误差函数来估计直接行动方案的近似精度。此功能可估计直接行动方案的非结构化网格的质量。矩阵耗散用于倾倒中心方案的奇偶不稳定性。它结合了迎风方案的准确性和居中方案的鲁棒性和效率。高度拉伸的Delaunay三角剖分的构造包括两个步骤。第一步,在物体和尾流附近生成近乎正交的结构化高CAR网格。在第二步中,此网格通过增量插入技术在计算域内平稳地继续。利用提出的方法,结合Spalart-Allmaras一方程湍流模型,对单翼和多翼机翼周围的湍流粘性流进行了计算。

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