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Large-eddy simulation of curved-geometry flows using contravariant components of velocity

机译:利用速度的反分量对弯曲几何流动进行大涡模拟

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摘要

The current large-eddy simulation (LES) research makes use of the contravariant components as the dependent variables on a staggered grid system for the discretisation of the governing equations in curvilinear coordinates. This technology provides a possibility to investigate efficiently turbulent flows in complex geometries. To test and validate the recently developed in-house LES code, LESSGA (Large-Eddy Simulation on a Staggered Grid Arrangement), numerical simulations were performed for turbulent flows in a concentric annular pipe and transitional flows past an airfoil. In this article, the computed results of flows in a concentric annular pipe with a radius ratio of a = R_(inner)/R_(outer) = 0.5 at Re_t = 100- 200 and flows past an SD7003 airfoil at Re_c = 60,000 and angle of attack a = 48 are compared with available experimental and DNS data. Technical difficulties experienced are also discussed.
机译:当前的大涡模拟(LES)研究利用交错分量作为交错网格系统上的因变量,以便在曲线坐标系中离散化控制方程。这项技术为研究复杂几何形状中的湍流提供了可能。为了测试和验证最近开发的内部LES代码LESSGA(交错网格布置的大涡模拟),对同心环形管道中的湍流和经过机翼的过渡流进行了数值模拟。在本文中,在Re_t = 100-200时,半径比为a = R_(内)/ R_(外)= 0.5的同心环形管中流动的计算结果,在Re_c = 60,000和角度下流过SD7003翼型的计算结果将攻击次数a = 48与可用的实验数据和DNS数据进行比较。还讨论了遇到的技术困难。

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