论文标题
在结构化网格上的三维紧凑型高阶气动方案
A three-dimensional compact high-order gas-kinetic scheme on structured mesh
论文作者
论文摘要
在本文中,首先提出了三维计算的三阶紧凑型气体运动方案,用于可压缩的Euler和Navier-Stokes溶液。该方案由于GKS中的时间依赖性气体分布函数而实现其紧凑性,不仅提供了通量,还提供了下一个电池界面处的下一个时间级别的时间准确流动变量。结果,可以通过高斯定理自然获得平均流量变量的一阶空间衍生物。然后,可以实现涉及细胞平均值及其一阶空间衍生物的三阶紧凑重建。三线性插值用于治疗一般六面体网状的可能的非链球元素。使用约束最小二乘技术来提高平滑案例的准确性。为了处理平滑和不连续的流程,在当前方案中遵循Zhu中的想法,在2018年,在当前方案中设计了新的Hweno重建。在当前方案中不需要识别陷入困境的单元格。与基于Riemann求解器的方法相反,紧凑型方案可以通过两阶段的两阶段时间离散化实现三阶时间精度,而不是三阶段的runge-kutta方法。总体而言,提出的方案在二维情况下继承了先前的方案的高精度和效率。所需的三阶精度可以通过弯曲边界获得。该方案的鲁棒性通过许多情况进行了验证,包括在无粘性和粘性流量计算中的强烈冲击。平滑和不连续案例的定量比较表明,当前的三阶方案可以与相同网格下的五阶非紧凑型GK给出竞争结果。在本方案中可以使用大约0.5的大CFL数。
In this paper, a third-order compact gas-kinetic scheme is firstly proposed for three-dimensional computation for the compressible Euler and Navier-Stokes solutions. The scheme achieves its compactness due to the time-dependent gas distribution function in GKS, which provides not only the fluxes but also the time accurate flow variables in the next time level at a cell interface. As a result, the cell averaged first-order spatial derivatives of flow variables can be obtained naturally through the Gauss's theorem. Then, a third-order compact reconstruction involving the cell averaged values and their first-order spatial derivatives can be achieved. The trilinear interpolation is used to treat possible non-coplanar elements on general hexahedral mesh. The constrained least-square technique is applied to improve the accuracy in the smooth case. To deal with both smooth and discontinuous flows, a new HWENO reconstruction is designed in the current scheme by following the ideas in Zhu, 2018. No identification of troubled cells is needed in the current scheme. In contrast to the Riemann solver-based method, the compact scheme can achieve a third-order temporal accuracy with the two-stage two-derivative temporal discretization, instead of the three-stage Runge-Kutta method. Overall, the proposed scheme inherits the high accuracy and efficiency of the previous ones in two-dimensional case. The desired third-order accuracy can be obtained with curved boundary. The robustness of the scheme has been validated through many cases, including strong shocks in both inviscid and viscous flow computations. Quantitative comparisons for both smooth and discontinuous cases show that the current third-order scheme can give competitive results against the fifth-order non-compact GKS under the same mesh. A large CFL number around 0.5 can be used in the present scheme.