Analytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows

被引:16
作者
HE, Zhiqiang [1 ,2 ]
JIANG, Zhongzheng [1 ]
ZHANG, Huangwei [2 ]
CHEN, Weifang [1 ]
机构
[1] Zhejiang Univ, Sch Aeronaut & Astronaut, Hangzhou 310027, Peoples R China
[2] Natl Univ Singapore, Dept Mech Engn, Singapore 117576, Singapore
基金
中国国家自然科学基金;
关键词
Knudsen number; Microscale flow; Non-equilibrium; Nonlinear constitutive rela-tions; Rarefied gas; GAS-KINETIC SCHEME; SHOCK STRUCTURE; GENERALIZED HYDRODYNAMICS; BOLTZMANN-EQUATION; BURNETT EQUATIONS; UNIFIED ALGORITHM; CONTINUUM; TRANSITION; SIMULATIONS; COMPUTATION;
D O I
10.1016/j.cja.2020.06.023
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
It is well known that Navier-Stokes equations are not valid for those high-Knudsen and high-Mach flows, in which the local thermodynamically non-equilibrium effects are dominant. To extend the non-equilibrium describing the ability of macroscopic equations, Nonlinear Coupled Constitutive Relation (NCCR) model was developed from Eu?s generalized hydrodynamic equations to substitute linear Newton?s law of viscosity and Fourier?s law of heat conduction in conservation laws. In the NCCR model, how to solve the decomposed constitutive equations with reasonable computational cost is a key ingredient of this scheme. In this paper, an analytic method is proposed firstly. Compared to the iterative procedure in the conventional NCCR model, the analytic method not only obtains exact roots of the decomposed constitutive polynomials, but also preserves the nonlinear constitutive relations in the original framework of NCCR methods. Numerical tests to assess the efficiency and accuracy of the proposed method are conducted for argon shock structures, Couette flows, two-dimensional hypersonic flows over a cylinder and threedimensional supersonic flows over a three-dimensional sphere. These superior advantages of the current method are expected to render itself a powerful tool for simulating the hypersonic rarefied flows and microscale flows of high Knudsen number for engineering applications. ? 2020 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
引用
收藏
页码:136 / 153
页数:18
相关论文
共 67 条
[1]   Generalized hydrodynamics and shock waves [J].
AlGhoul, M ;
Eu, BC .
PHYSICAL REVIEW E, 1997, 56 (03) :2981-2992
[2]   DENSITY PROFILES IN ARGON AND NITROGEN SHOCK-WAVES MEASURED BY ABSORPTION OF AN ELECTRON-BEAM [J].
ALSMEYER, H .
JOURNAL OF FLUID MECHANICS, 1976, 74 (APR6) :497-513
[3]  
[Anonymous], 2018, ADV SOME HYPERSONIC
[4]  
[Anonymous], 2008, THESIS U MICHIGAN
[5]   RUFFINI,PAOLO CONTRIBUTIONS TO THE QUINTIC [J].
AYOUB, RG .
ARCHIVE FOR HISTORY OF EXACT SCIENCES, 1980, 23 (03) :253-277
[6]   BGK-Burnett equations for flows in the continuum-transition regime [J].
Balakrishnan, R ;
Agarwal, RK ;
Yun, KY .
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 1999, 13 (04) :397-410
[7]   Burnett simulation of flow and heat transfer in micro Couette flow using second-order slip conditions [J].
Bao, F. B. ;
Lin, J. Z. ;
Shi, X. .
HEAT AND MASS TRANSFER, 2007, 43 (06) :559-566
[8]  
Bird G. A., 1994, MOL GAS DYNAMICS DIR
[9]   ASPECTS OF STRUCTURE OF STRONG SHOCK WAVES [J].
BIRD, GA .
PHYSICS OF FLUIDS, 1970, 13 (05) :1172-&
[10]   PREDICTING FAILURE OF THE CONTINUUM FLUID EQUATIONS IN TRANSITIONAL HYPERSONIC FLOWS [J].
BOYD, ID ;
CHEN, G ;
CANDLER, GV .
PHYSICS OF FLUIDS, 1995, 7 (01) :210-219