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A third order gas-kinetic scheme for unstructured grid

机译:非结构化网格的三阶气体动力学方案

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In order to study the high order gas-kinetic scheme on unstructured grid, we combine the third order gas-kinetic flux solver with the compact least-square reconstruction (CIS) method together. The CLS method can achieve arbitrary high order compact reconstruction using the stencil from the whole computational domain implicitly. A large sparse linear system resulted from the CLS reconstruction method is solved by applying the generalized minimal residual algorithm (GMRES). To accelerate the convergence, the Reverse-CuthillMcKee (RCM) algorithm and the incomplete lower-upper (ILU) factorization method are implemented. Different from the traditional flux solver, the gas-kinetic scheme developed by Xu is of high spatial and temporal accuracy. Applying the second order Taylor expansion of the initial gas distribution function and equilibrium state at cell interface, the flux solver can be extended to third order accuracy directly. The accuracy of present method is validated by several numerical cases such as the advection of density perturbation problem, isotropic vortex propagation problem, Sod shock-wave problem, Lax shock tube test case, Shu-Osher problem, shock-vortex interaction, lid-driven cavity flow, and flat plate boundary layer. The advantages of this high order gas-kinetic scheme are exhibited in some benchmarks including incompressible flow and supersonic compressible flow, inviscid flow and viscous flow. (C) 2019 Elsevier Ltd. All rights reserved.
机译:为了研究非结构化网格的高阶气体动力学方案,我们将三阶气体动力学通量求解器与紧凑型最小二乘重建(CIS)法相结合。 CLS方法可以通过隐式使用来自整个计算域的模板实现任意高阶紧凑的重建。通过施加广义最小残余算法(GMRES)来解决来自CLS重建方法的大稀疏线性系统。为了加速收敛,实现了反向切割频率(RCM)算法和不完整的下上部(ILU)分解方法。不同于传统的助焊剂求解器,徐开发的气体动力学方案具有高空间和时间精度。在电池接口处应用初始气体分布函数和平衡状态的二阶泰勒膨胀,通量求解器可以直接延伸到第三顺序精度。目前方法的准确性通过若干数值案例验证,例如密度扰动问题的平流,各向同性涡旋传播问题,SOD冲击波问题,疏松冲击管测试盒,舒奥斯赫问题,冲击涡流相互作用,盖驱动腔流量,平板边界层。这种高阶气体动力学方案的优点在一些基准中展出,包括不可压缩的流动和超音速可压缩流动,缺陷流和粘性流动。 (c)2019 Elsevier Ltd.保留所有权利。

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