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基于矩约束的离散统一气体动力学格式的无滑移边界条件新方案

Novel Schemes of No-Slip Boundary Conditions for the Discrete Unified Gas Kinetic Scheme Based on the Moment Constraints.

作者信息

Guo Wenqiang, Hou Guoxiang

机构信息

Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China.

Laboratory of Aerodynamics in Multiple Flow Regimes, China Aerodynamics Research and Development Center, Mianyang 621000, China.

出版信息

Entropy (Basel). 2023 May 10;25(5):780. doi: 10.3390/e25050780.

Abstract

The boundary conditions are crucial for numerical methods. This study aims to contribute to this growing area of research by exploring boundary conditions for the discrete unified gas kinetic scheme (DUGKS). The importance and originality of this study are that it assesses and validates the novel schemes of the bounce back (BB), non-equilibrium bounce back (NEBB), and Moment-based boundary conditions for the DUGKS, which translate boundary conditions into constraints on the transformed distribution functions at a half time step based on the moment constraints. A theoretical assessment shows that both present NEBB and Moment-based schemes for the DUGKS can implement a no-slip condition at the wall boundary without slip error. The present schemes are validated by numerical simulations of Couette flow, Poiseuille flow, Lid-driven cavity flow, dipole-wall collision, and Rayleigh-Taylor instability. The present schemes of second-order accuracy are more accurate than the original schemes. Both present NEBB and Moment-based schemes are more accurate than the present BB scheme in most cases and have higher computational efficiency than the present BB scheme in the simulation of Couette flow at high Re. The present Moment-based scheme is more accurate than the present BB, NEBB schemes, and reference schemes in the simulation of Poiseuille flow and dipole-wall collision, compared to the analytical solution and reference data. Good agreement with reference data in the numerical simulation of Rayleigh-Taylor instability shows that they are also of use to the multiphase flow. The present Moment-based scheme is more competitive in boundary conditions for the DUGKS.

摘要

边界条件对于数值方法至关重要。本研究旨在通过探索离散统一气体动力学格式(DUGKS)的边界条件,为这一不断发展的研究领域做出贡献。本研究的重要性和创新性在于,它评估并验证了DUGKS的新型反弹(BB)、非平衡反弹(NEBB)和基于矩的边界条件,这些边界条件基于矩约束,在半步长时将边界条件转化为对变换后的分布函数的约束。理论评估表明,DUGKS目前的NEBB和基于矩的格式都可以在壁边界实现无滑移条件,且无滑移误差。通过对库埃特流、泊肃叶流、顶盖驱动方腔流、偶极壁碰撞和瑞利 - 泰勒不稳定性的数值模拟验证了当前格式。二阶精度的当前格式比原始格式更精确。在大多数情况下,当前的NEBB和基于矩的格式都比当前的BB格式更精确,并且在高雷诺数下库埃特流的模拟中比当前的BB格式具有更高的计算效率。与解析解和参考数据相比,在泊肃叶流和偶极壁碰撞的模拟中,当前基于矩的格式比当前的BB、NEBB格式和参考格式更精确。在瑞利 - 泰勒不稳定性的数值模拟中与参考数据的良好一致性表明,它们对多相流也有用。当前基于矩的格式在DUGKS的边界条件方面更具竞争力。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef88/10217328/555833841ab1/entropy-25-00780-g001.jpg

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