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An annurate finite volume scheme for euler and navier-stokes equations on unstructured adaptive grids

机译:非结构自适应网格上欧拉和纳斯托克斯方程的年限有限体积格式

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This paper presents a finite volume cell-centered technique for computing steady state solutions of the full Euler and Navier-Stokes equations on unstructured meshes. We aim to design a scheme which is the most possible insensitive to grid distortions, while however remaining of practical interest in terms of CPU time, storage and convergence. For that purpose, we use an original quadratic reconstruction with a fixed stencil and a high order flux integration by the Gauss quadrature rule to compute the advective term of the equations. Time evolution is presently performed with an explicit multi-step Runge-Kutta scheme. A very general adaptation procedure based on h-refinement and coarsening is employed to improve the resolution of complex flow features. The accuracy of the method is demonstrated for a liner equation and for inviscid and viscous flow computations. The inviscid flow over the NACA0012 airfoil is computed at various Mach numbers. These calculations illustrate the effectiveness of the adaptation procedure. We investigate the supersonic flow over a compression ramp to validate the Navier-Stokes solver by using a hybrid grid.
机译:本文提出了一种有限体积单元中心技术,用于在非结构网格上计算完整的Euler和Navier-Stokes方程的稳态解。我们旨在设计一种对网格失真最不敏感的方案,但是在CPU时间,存储和收敛方面仍然具有实际意义。为此,我们使用具有固定模版和高斯通量积分的高斯通量积分进行原始二次重构,以计算方程的对流项。目前,时间演化是通过明确的多步Runge-Kutta方案执行的。基于h细化和粗化的非常通用的适应过程用于提高复杂流特征的分辨率。对于衬管方程以及不粘和粘性流计算,证明了该方法的准确性。通过各种马赫数计算出NACA0012机翼上的无粘性流。这些计算说明了适应程序的有效性。我们研究了压缩坡道上的超音速流,以通过使用混合网格来验证Navier-Stokes求解器。

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