In this work, the rarefied Couette flow of diatomic gases with thermal nonequilibrium effects is investigated by the direct simulation Monte Carlo (DSMC) method, and a macroscopic computational model is developed to consider the local rarefaction effects for diatomic gases in the near-continuum regime. The nonlinear transport properties of the diatomic gases are studied, indicating that effective viscosity and effective translational thermal conductivity in the shear nonequilibrium state are affected by translational nonequilibrium effects, which obey the same laws for both monatomic and diatomic gases. The transport coefficients of internal energy modes are affected by both translational nonequilibrium and internal energy relaxation, therefore, the effective rotational and vibrational thermal conductivities are related to the effective viscosity through a modified Eucken relation that accounts for internal energy relaxation. Conclusively, effective constitutive relations are newly established as a function of the shear nonequilibrium parameter and the modified Eucken factors for thermal nonequilibrium flows, and these are integrated into the macroscopic two-temperature model. Subsequently, it is assessed in the simulation of hypersonic flows over flat plates and cylinders at various Knudsen numbers. The results show that the surface shear stress and heat flux obtained by the proposed model agree well with the DSMC results, indicating significantly improved performance compared to the conventional Navier-Stokes two-temperature model for hypersonic flows in the near-continuum regime.
机构:
Tianjin Univ, Sch Mech Engn, Lab High Speed Aerodynam, Tianjin 300072, Peoples R China
Tianjin Key Lab Modern Engn Mech, Tianjin 300072, Peoples R ChinaTianjin Univ, Sch Mech Engn, Lab High Speed Aerodynam, Tianjin 300072, Peoples R China
Chen, Jie
Ou, Jihui
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Tianjin Univ, Sch Mech Engn, Lab High Speed Aerodynam, Tianjin 300072, Peoples R ChinaTianjin Univ, Sch Mech Engn, Lab High Speed Aerodynam, Tianjin 300072, Peoples R China
Ou, Jihui
Zhao, Lei
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Tianjin Univ, Sch Mech Engn, Lab High Speed Aerodynam, Tianjin 300072, Peoples R China
China Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R ChinaTianjin Univ, Sch Mech Engn, Lab High Speed Aerodynam, Tianjin 300072, Peoples R China
Zhao, Lei
31ST INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS (RGD31),
2019,
2132
机构:
Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
Guo, Jinghui
Wang, Xiaoyong
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机构:
Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R ChinaBeihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
Wang, Xiaoyong
Li, Sijia
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Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
Li, Sijia
Lin, Guiping
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Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China