Boltzmann-Curtiss Description for Flows Under Translational Nonequilibrium

被引:0
|
作者
Ahmed, Mohamed M. [1 ]
Cheikh, Mohamad, I [2 ]
Chen, James [2 ]
机构
[1] Kansas State Univ, Dept Mech & Nucl Engn, Manhattan, KS 66502 USA
[2] Univ Buffalo State Univ New York, Dept Mech & Aerosp Engn, Buffalo, NY 14260 USA
关键词
LAMINAR HYPERSONIC FLOWFIELDS; MORPHING CONTINUUM; KINETIC-THEORY; EQUATION; VERIFICATION; VALIDATION;
D O I
10.1115/1.4045761
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Continuum-based theories, such as Navier-Stokes (NS) equations, have been considered inappropriate for flows under nonequilibrium conditions. In part, it is due to the lack of rotational degrees-of-freedom in the Maxwell-Boltzmann distribution. The Boltzmann-Curtiss formulation describes gases allowing both rotational and translational degrees-of-freedom and forms morphing continuum theory (MCT). The first-order solution to Boltzmann-Curtiss equation yields a stress tensor that contains a coupling coefficient that is dependent on the particles number density, the temperature, and the total relaxation time. A new bulk viscosity model derived from the Boltzmann-Curtiss distribution is employed for shock structure and temperature profile under translational and rotational nonequilibrium. Numerical simulations of argon and nitrogen shock profiles are performed in the Mach number range of 1.2-9. The current study, when comparing with experimental measurements and direct simulation Monte Carlo (DSMC) method, shows a significant improvement in the density profile, normal stresses, and shock thickness at nonequilibrium conditions than NS equations. The results indicate that equations derived from the Boltzmann-Curtiss distribution are valid for a wide range of nonequilibrium conditions than those from the Maxwell-Boltzmann distribution.
引用
收藏
页数:9
相关论文
共 50 条
  • [1] First-order approximation to the Boltzmann-Curtiss equation for flows with local spin
    Wonnell, Louis B.
    Chen, James
    JOURNAL OF ENGINEERING MATHEMATICS, 2019, 114 (01) : 43 - 64
  • [2] Three-Dimensional Discontinuous Galerkin Method for the Second-Order Boltzmann-Curtiss Constitutive Model in Continuum-Rarefied Gas Flows
    Singh, S.
    Myong, R. S.
    31ST INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS (RGD31), 2019, 2132
  • [3] Topology of the second-order constitutive model based on the Boltzmann-Curtiss kinetic equation for diatomic and polyatomic gases
    Singh, S.
    Karchani, A.
    Sharma, K.
    Myong, R. S.
    PHYSICS OF FLUIDS, 2020, 32 (02)
  • [4] First-order approximation to the Boltzmann–Curtiss equation for flows with local spin
    Louis B. Wonnell
    James Chen
    Journal of Engineering Mathematics, 2019, 114 : 43 - 64
  • [5] Lattice Boltzmann models for nonequilibrium gas flows
    Tang, Gui-Hua
    Zhang, Yong-Hao
    Emerson, David R.
    PHYSICAL REVIEW E, 2008, 77 (04):
  • [6] Lattice Boltzmann approach for complex nonequilibrium flows
    Montessori, A.
    Prestininzi, P.
    La Rocca, M.
    Succi, S.
    PHYSICAL REVIEW E, 2015, 92 (04):
  • [7] Simulation of Nonequilibrium Turbulent Flows on the Basis of the Boltzmann Equation
    Aristov, V. V.
    Rovenskaya, O. I.
    28TH INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS 2012, VOLS. 1 AND 2, 2012, 1501 : 422 - 428
  • [8] Numerical Simulations of Rarefied Gas Flow over an Aero-spiked Hypersonic Blunt Body Using the Secondorder Boltzmann-Curtiss Constitutive Model
    Chourushi, T.
    Singh, S.
    Vishnu, A. S.
    Myong, R. S.
    32ND INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS, 2024, 2996
  • [9] Computational Study of Hypersonic Rarefied Gas Flow over Re-Entry Vehicles Using the Second-Order Boltzmann-Curtiss Constitutive Model
    Chourushi, Tushar
    Singh, Satyvir
    Sreekala, Vishnu Asokakumar
    Myong, Rho Shin
    INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, 2021, 35 (08) : 566 - 593
  • [10] Discrete Boltzmann model with split collision for nonequilibrium reactive flows
    Chuandong Lin
    Kai H Luo
    Huilin Lai
    Communications in Theoretical Physics, 2024, 76 (08) : 166 - 188