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两种用于NS-DSMC耦合方法的连续失效参数对比

唐振宇 蔡国飙

唐振宇, 蔡国飙. 两种用于NS-DSMC耦合方法的连续失效参数对比[J]. 北京航空航天大学学报, 2014, 40(3): 389-393. doi: 10.13700/j.bh.1001-5965.2013.0252
引用本文: 唐振宇, 蔡国飙. 两种用于NS-DSMC耦合方法的连续失效参数对比[J]. 北京航空航天大学学报, 2014, 40(3): 389-393. doi: 10.13700/j.bh.1001-5965.2013.0252
Tang Zhenyu, Cai Guobiao. Comparison analysis between two continuum breakdown parameters applied in coupled NS-DSMC method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 389-393. doi: 10.13700/j.bh.1001-5965.2013.0252(in Chinese)
Citation: Tang Zhenyu, Cai Guobiao. Comparison analysis between two continuum breakdown parameters applied in coupled NS-DSMC method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 389-393. doi: 10.13700/j.bh.1001-5965.2013.0252(in Chinese)

两种用于NS-DSMC耦合方法的连续失效参数对比

doi: 10.13700/j.bh.1001-5965.2013.0252
详细信息
  • 中图分类号: O354

Comparison analysis between two continuum breakdown parameters applied in coupled NS-DSMC method

  • 摘要: NS-DSMC(Navier Stokes-Direct Simulation Monte Carlo)耦合方法是计算连续-稀薄跨流域流动的主要方法,应用过程中如何确定连续流域和稀薄流域的界面是此方法的关键问题之一,界面位置通常通过连续失效参数来判定.为合理选择连续失效参数,对目前广泛使用的两种连续失效参数KnQ和B参数进行了理论上的分析和比较,表明虽然他们建立的出发点不同,但在数学形式上具有一定相似性.通过圆柱绕流问题的数值试验进一步验证了两种连续失效参数具有一定对应关系.KnQB两种连续失效参数在NS-DSMC耦合方法中应用效果相差不大,但KnQ 的阈值0.05适用范围较广,而B参数的阈值对不同流动问题会有变化.

     

  • [1] 沈青.稀薄气体动力学[M].北京:国防工业出版社,2003: 83-88 Shen Qing.Rarefied gas dynamics[M].Beijing:National Defence Industry Press,2003:83-88 (in Chinese)
    [2] Bird G A.Molecular gas dynamics and the direct simulation of gas flow[M].Oxford:Clarendon,1994
    [3] Hash D B,Hassan H A.A decoupled DSMC/Navier-Stokes analysis of a transitional flow experiment[R].AIAA-96-0353,1996
    [4] 蔡国飙,王慧玉,庄逢甘.真空羽流场的N-S和DSMC耦合数值模拟[J].推进技术,1998,19(4):57-61 Cai Guobiao,Wang Huiyu,Zhuang Fenggan.Coupled numerical simulation with N-S and DSMC on vacuum plum effect[J].Journal of Propulsion Technology,1998,19(4):57-61(in Chinese)
    [5] Schwartzentruber T E,Boyd I D.A hybrid particle-continuum method applied to shock waves[J].Journal of Computational P- hysics,2006,215(2):402-416
    [6] Bird G A.Breakdown of translational and rotational equilibrium in gaseous expansions[J].AIAA Journal,1970,8(11):1998-2003
    [7] Lian Y Y,Chen Y S,Tseng K C,et al.Improved parallelized hybrid DSMC-NS method[J].Computers & Fluids,2011,45(1): 254-260
    [8] Boyd I D,Chen G,Candler G V.Predicting failure of the continuum fluid equations in transitional hypersonic flows[J].Phys Fluids,1995,7(1):210-219
    [9] Wang W L,Boyd I D.Continuum breakdown in hypersonic viscous flows[R].AIAA 2002-0651,2002
    [10] Garcia A L,Bell J B,Crutchfield W Y,et al.Adaptive mesh and algorithm refinement using direct simulation Monte Carlo[J].Journal of Computational Physics,1999,154(1):134-155
    [11] Abbate G,Kleijn C R,Thijsse B J.Hybrid continuum/molecular simulations of transient gas flows with rarefaction[J].AIAA Journal,2009,47(7):1741-1749
    [12] Schwartzentruber T E,Scalabrin L C,Boyd I D.A modular particle-continuum numerical method for hypersonic non-equilibrium gas flows[J].Journal of Computational Physics,2007, 225(1):1159-1174
    [13] Tang Z,He B,Cai G.Investigation on a coupled CFD/DSMC method for continuum-rarefied flows[C]//Mareschal M,Santos A.AIP Conf Proc 1501.Zaragoza,Spain:American Institute of Physics,2012:535-540
    [14] Schwartzentruber T E,Scalabrin L C,Boyd I D.Multiscale particle-continuum simulations of hypersonic flow over a planetary probe[J].Journal of Spacecraft and Rockets,2008,45(6):1196-1206
    [15] Sun Q,Boyd I D,Candler G V.A hybrid continuum/particle approach for modeling subsonic,rarefied gas flows[J].Journal of Computational Physics,2004,194(1):256-277
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出版历程
  • 收稿日期:  2013-05-10
  • 网络出版日期:  2014-03-20

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