Volume 46 Issue 10
Oct.  2025
Turn off MathJax
Article Contents
PENG Aoping, WU Junlin, LI Zhihui. Numerical Evaluation of a Novel Multi-Relaxation Kinetic Model for Gas Mixture Flows[J]. Applied Mathematics and Mechanics, 2025, 46(10): 1245-1255. doi: 10.21656/1000-0887.450175
Citation: PENG Aoping, WU Junlin, LI Zhihui. Numerical Evaluation of a Novel Multi-Relaxation Kinetic Model for Gas Mixture Flows[J]. Applied Mathematics and Mechanics, 2025, 46(10): 1245-1255. doi: 10.21656/1000-0887.450175

Numerical Evaluation of a Novel Multi-Relaxation Kinetic Model for Gas Mixture Flows

doi: 10.21656/1000-0887.450175
Funds:

The National Science Foundation of China(12332013

11902339)

  • Received Date: 2024-06-14
  • Rev Recd Date: 2025-03-04
  • Available Online: 2025-11-13
  • To study the flow mechanism of the gas mixture transport phenomenon in all flow regimes, a multi relaxation collision model equation suitable for gas mixture was developed out of the Boltzmann equation as the basic equation in the gas kinetic theory, and the expression of the collision relaxation frequency pertinent to the DSMC method was established. Then under the framework of the gas kinetic unified algorithm, a multi-component 1D shock wave structure problem with high particle mass and mole fraction ratios was simulated, and compared with the DSMC results. The comparison shows that, the proposed model equation can simulate the macroscopic parameter changes of the gas mixture and its components in the shock wave, and can analyze the diffusion rules of each component of the gas mixture. The validity and correctness of the multi relaxation model equation were verified. The simulation results indicate that, the diffusion effect of the components with the smallest molecular weight is the most significant, but the effect of other components is relatively small, and the flow non-equilibrium effect mainly comes from the component with the largest molecular weight; the thermal diffusion caused by temperature gradients is more sensitive to molecular mass in shock wave, and the mass diffusion caused by component concentration gradients makes components separate, which produces a significant non-equilibrium effect downstream of shock wave. At the same time, the addition of medium-mass molecules in the multi-component mixed gas increases the diffusion of large-mass molecules and magnifies the separation effect.
  • loading
  • [2]BOYD I D, SCHWARTZENTRUBER T E. Nonequilibrium Gas Dynamics and Molecular Simulation[M]. Cambridge: Cambridge University Press, 2017.
    查普曼 S, 考林T G. 非均匀气体的数学理论[M]. 刘大有, 王伯懿, 译. 北京: 科学出版社, 1985. (CHAPMAN S, COWLING T G. The Mathematical Theory of Non-Uniform Gases[M]. LIU Dayou, WANG Boyi, transl. Beijing: Science Press, 1985. (Chinese version))
    [3]秦文瑾, 韩天祥, 张振东, 等. 喷雾碰壁燃烧数值模拟研究[J]. 应用数学和力学, 2023,44(9): 1087-1096. (QIN Wenjin, HAN Tianxiang, ZHANG Zhendong, et al. Numerical simulation study of spray wall impingement combustion[J]. Applied Mathematics and Mechanics,2023,44(9): 1087-1096. (in Chinese))
    [4]卞荫贵, 徐立功. 气动热力学[M]. 2版. 合肥: 中国科学技术大学出版社, 2010. (BIAN Yingui, XU Ligong. Aerothermodynamics[M]. 2nd ed. Hefei: University of Science and Technology of China Press, 2010. (in Chinese))
    [5]HASH D, HASSAN H. A decoupled DSMC/Navier-Stokes analysis of a transitional flow experiment[C]//34th Aerospace Sciences Meeting and Exhibit. Reno, NV, USA: AIAA, 1996: AIAA1996-353.
    [6]李中华, 党雷宁, 李志辉, 等. 天宫飞行器过渡流区高超声速绕流N-S/DSMC耦合计算[J]. 载人航天, 2020,26(5): 543-549. (LI Zhonghua, DANG Leining, LI Zhihui, et al. N-S/DSMC hybrid numerical simulation for hypersonic transitional flow around disintegrated objects of Tiangong vehicle[J]. Manned Spaceflight,2020,26(5): 543-549. (in Chinese))
    [7]BAILO R, REY T. Projective and telescopic projective integration for non-linear kinetic mixtures[J]. Journal of Computational Physics,2022,458: 111082.
    [8]LIU C, XU K. Unified gas-kinetic wave-particle methods Ⅳ: multi-species gas mixture and plasma transport[J]. Advances in Aerodynamics,2021,3(1): 9.
    [9]BRULL S. An ellipsoidal statistical model for a monoatomic and a polyatomic gas mixture[J]. Communications in Mathematical Sciences,2021,19(8): 2177-2194.
    [10]BRULL S. An ellipsoidal statistical model for gas mixtures[J]. Communications in Mathematical Sciences,2015,13(1): 1-13.
    [11]LIU S, LIANG Y. Asymptotic-preserving Boltzmann model equations for binary gas mixture[J]. Physical Review E,2016,93(2): 023102.
    [12]BARANGER C, DAUVOIS Y, MAROIS G, et al. A BGK model for high temperature rarefied gas flows[J]. European Journal of Mechanics B: Fluids,2020,80: 1-12.
    [13]ANDRIES P, AOKI K, PERTHAME B. A consistent BGK-type model for gas mixtures[J]. Journal of Statistical Physics,2002,106(5): 993-1018.
    [14]TODOROVA B N, WHITE C, STEIJL R. Numerical evaluation of novel kinetic models for binary gas mixture flows[J]. Physics of Fluids,2020,32: 016102.
    [15]LI Z H, ZHANG H X. Study on gas kinetic unified algorithm for flows from rarefied transition to continuum[J]. Journal of Computational Physics,2004,193(2): 708-738.
    [16]PENGA P, LI Z H, WU J L, et al. Implicit gas-kinetic unified algorithm based on multi-block docking grid for multi-body reentry flows covering all flow regimes[J]. Journal of Computational Physics,2016,327: 919-942.
    [17]吴俊林, 李志辉, 彭傲平, 等. Boltzmann-Rykov模型的有限体积方法计算[J]. 应用数学和力学, 2014,35(2): 121-129. (WU Junlin, LI Zhihui, PENG Aoping, et al. Calculation of Boltzmann-Rykov model equation by finite volume method[J]. Applied Mathematics and Mechanics,2014,35(2): 121-129. (in Chinese))
    [18]BOBYLEV A V, BISI M, GROPPI M, et al. A general consistent BGK model for gas mixtures[J]. Kinetic & Related Models,2018,11(6): 1377-1393.
    [19]沈青. 稀薄气体动力学[M]. 北京: 国防工业出版社, 2003. (SHEN Qing. Rarefied Gas Dynamics[M]. Beijing: National Defense Industry Press, 2003. (in Chinese))
    [20]BIRD G A. Molecular Gas Dynamics and the Direct Simulation of Gas Flows[M]. Oxford: Oxford University Press, 1994.
    [21]KOLODNER I. Moment description of gas mixture-Ⅰ: 7980[R]. New York University Report, 1957.
    [22]彭傲平. 大型航天器跨流域非平衡玻尔兹曼模型方程统一算法应用研究[D]. 绵阳: 中国空气动力研究与发展中心, 2017. (PENG Aoping. Application and study of gas-kinetic unified algorithm based on non-equilibrium Boltzmann model equation for large-scale spacecraft covering all flow regimes[D]. Miangyang: China Aerodynamics Research and Development Center, 2017 (in Chinese))
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (29) PDF downloads(5) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return