Implicit high-order gas-kinetic schemes for compressible flows on three-dimensional unstructured meshes II: Unsteady flows

IF 3.8 2区 物理与天体物理 Q2 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Yaqing Yang , Liang Pan , Kun Xu
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Abstract

For the simulations of unsteady flow, the global time step becomes really small with a large variation of local cell size. In this paper, an implicit high-order gas-kinetic scheme (HGKS) is developed to alleviate the restrictions on the time step for unsteady simulations. In order to improve the efficiency and keep the high-order accuracy, a two-stage third-order implicit time-accurate discretization is proposed. In each stage, an artificial steady solution is obtained for the implicit system with the pseudo-time iteration. In the iteration, the classical implicit methods are adopted to solve the nonlinear system, including the lower-upper symmetric Gauss-Seidel (LUSGS) and generalized minimum residual (GMRES) methods. To achieve the spatial accuracy, the HGKSs with both non-compact and compact reconstructions are constructed. For the non-compact scheme, the weighted essentially non-oscillatory (WENO) reconstruction is used. For the compact one, the Hermite WENO (HWENO) reconstruction is adopted due to the updates of both cell-averaged flow variables and their derivatives. The expected third-order temporal accuracy is achieved with the two-stage temporal discretization. For the smooth flow, only a single artificial iteration is needed. For uniform meshes, the efficiency of the current implicit method improves significantly in comparison with the explicit one. For the flow with discontinuities, compared with the well-known Crank-Nicholson method, the spurious oscillations in the current schemes are well suppressed. The increase of the artificial iteration steps introduces extra reconstructions associating with a reduction of the computational efficiency. Overall, the current implicit method leads to an improvement in efficiency over the explicit one in the cases with a large variation of mesh size. Meanwhile, for the cases with strong discontinuities on a uniform mesh, the efficiency of the current method is comparable with that of the explicit scheme.
三维非结构网格上可压缩流动的隐式高阶气体动力学方案 II:非稳态流动
对于非稳态流动的模拟,由于局部单元大小变化较大,全局时间步长会变得非常小。本文开发了一种隐式高阶气体动力学方案(HGKS),以减轻非稳态模拟对时间步长的限制。为了提高效率并保持高阶精度,本文提出了一种两阶段三阶隐式时间精确离散法。在每个阶段,通过伪时间迭代获得隐式系统的人工稳定解。在迭代过程中,采用了经典的隐式方法来求解非线性系统,包括下-上对称高斯-赛德尔(LUSGS)和广义最小残差(GMRES)方法。为了实现空间精度,我们构建了非紧凑型和紧凑型重建的 HGKS。在非紧凑型方案中,使用了加权基本非振荡(WENO)重建法。对于紧凑型方案,由于需要更新单元平均流量变量及其导数,因此采用了赫米特 WENO(HWENO)重建。两阶段时间离散化达到了预期的三阶时间精度。对于平滑流动,只需要一次人工迭代。对于均匀网格,与显式方法相比,当前隐式方法的效率显著提高。对于不连续流动,与著名的 Crank-Nicholson 方法相比,当前方案中的假振荡得到了很好的抑制。人工迭代步数的增加会带来额外的重构,从而降低计算效率。总体而言,在网格尺寸变化较大的情况下,当前的隐式方法比显式方法提高了效率。同时,对于均匀网格上的强不连续性情况,当前方法的效率与显式方案相当。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Journal of Computational Physics
Journal of Computational Physics 物理-计算机:跨学科应用
CiteScore
7.60
自引率
14.60%
发文量
763
审稿时长
5.8 months
期刊介绍: Journal of Computational Physics thoroughly treats the computational aspects of physical problems, presenting techniques for the numerical solution of mathematical equations arising in all areas of physics. The journal seeks to emphasize methods that cross disciplinary boundaries. The Journal of Computational Physics also publishes short notes of 4 pages or less (including figures, tables, and references but excluding title pages). Letters to the Editor commenting on articles already published in this Journal will also be considered. Neither notes nor letters should have an abstract.
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