Abstract

Thermally induced non-equilibrium gas flows have been simulated in the present study by coupling kinetic and extended thermodynamic methods. Three different types of thermally induced gas flows, including temperature-discontinuity- and temperature-gradient-induced flows and radiometric flow, have been explored in the transition regime. The temperature-discontinuity-induced flow case has shown that as the Knudsen number increases, the regularised 26 (R26) moment equation system will gradually loss its accuracy and validation. A coupling macro- and microscopic approach is employed to overcome these problems. The R26 moment equations are used at the macroscopic level for the bulk flow region, while the kinetic equation associated with the discrete velocity method (DVM) is applied to describe the gas close to the wall at the microscopic level, which yields a hybrid DVM/R26 approach. The numerical results have shown that the hybrid DVM/R26 method can be faithfully used for the thermally induced non-equilibrium flows. The proposed scheme not only improves the accuracy of the results in comparison with the R26 equations, but also extends their capability with a wider range of Knudsen numbers. In addition, the hybrid scheme is able to reduce the computational memory and time cost compared to the DVM.

Highlights

  • The advent of micro-electro-mechanical systems (MEMS) and the associated fabrication technologies has inspired a renewed impetus in understanding thermally driven flows [1,2,3,4]

  • Our newly developed hybrid discrete velocity method (DVM)/regularised 26 (R26) method is suitable for Kn ≤ 1, especially when the computational domain is much larger than the near-wall region

  • Knudsen numbers and the results employed at the macroscopic level, the Boltzmann model equation associated with the have using results

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Summary

Thermodynamic Methods

Weiqi Yang 1,2,3 , Xiao-Jun Gu 2, *, David R. Emerson 2 , Yonghao Zhang 3 and Shuo Tang 1. Scientific Computing Department, STFC Daresbury Laboratory, Warrington WA4 4AD, UK. James Weir Fluids Laboratory, Department of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow G1 1XJ, UK

Introduction
Extended Thermodynamic Governing Equations
Kinetic Equation and the Shakhov Model
Entropy and H-Theorem
Numerical Test Cases
Velocity
Radiometric Flow
For the casegood of Kn
The left
InKn each left andleft right results using the
Temperature profiles
Conclusions
Full Text
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