Statistical simulation of low-speed rarefied gas flows

Molecular-based numerical schemes, such as the direct simulation Monte Carlo (DSMC) method, are more physically appropriate for rarefied gas flows in microelectromechanical systems (MEMS). It is difficult for them to be statistically convergent, however, because the statistical fluctuation becomes insurmountably large at the low Mach numbers that are characteristic of MEMS. An information preservation (IP) technique is proposed to address this issue. This technique assigns each simulated molecule in the DSMC method two velocities. One is the molecular velocity used to compute the molecular motion following the same steps as the DSMC method. The other is called information velocity. It corresponds to the collective velocity of an enormous number of real molecules that the simulated molecule represents. Using the information velocity to compute macroscopic velocity and shear stress may remove the statistical fluctuation source inherent in the DSMC method that results from the randomness of the thermal velocity. The LP technique has been applied to benchmark problems, namely Couette, Poiseuille, and Rayleigh flows, in the entire Knudsen regime. The characteristic velocities in these flows range from 0.01 to 1 m/s, much smaller than the thermal velocity of about 340 m/s at room temperature. The meaningful results are obtained at a sample size of 10(3)-10(4), in comparison with a sample size of 10(8) or more required for the DSMC method at such a range of flow velocity. This results in a tremendous gain in CPU time. The velocity distributions, surface shear stress, and mass flux given by the IP calculations compare quite well with exact solutions at the continuum and free molecular limits, and with the numerical solutions of the linearized Boltzmann equation and experimental data in the transition regime.

[1]  Taku Ohwada,et al.  Numerical analysis of the plane Couette flow of a rarefied gas on the basis of the linearized Boltzmann equation for hard-sphere molecules , 1990 .

[2]  E. Oran,et al.  Computations of High-Speed, High Knudsen Number Microchannel Flows , 1997 .

[3]  E. Atlee Jackson,et al.  Kinetic Theory of the Impulsive Motion of an Infinite Plane , 1958 .

[4]  Chih-Ming Ho,et al.  MICRO-ELECTRO-MECHANICAL-SYSTEMS (MEMS) AND FLUID FLOWS , 1998 .

[5]  Hiroaki Matsumoto,et al.  Variable soft sphere molecular model for air species , 1992 .

[6]  Hassan Hassan,et al.  Role of Boundary Conditions in Monte Carlo Simulation of MEMS Devices , 1997 .

[7]  R. Nance,et al.  Role of Boundary Conditions in Monte Carlo Simulation of Microelectromechanical Systems , 1998 .

[8]  Edward S. Piekos,et al.  DSMC modeling of micromechanical devices , 1995 .

[9]  Jay N. Zemel,et al.  Gas flow in micro-channels , 1995, Journal of Fluid Mechanics.

[10]  K. Breuer,et al.  Numerical Modeling of Micromechanical Devices Using the Direct Simulation Monte Carlo Method , 1996 .

[11]  Henry Helvajian,et al.  Microengineering aerospace systems , 1999 .

[12]  Kazuo Aoki,et al.  Numerical analysis of the Poiseuille and thermal transpiration flows between two parallel plates on the basis of the Boltzmann equation for hard‐sphere molecules , 1989 .

[13]  Graeme A. Bird,et al.  MONTE-CARLO SIMULATION IN AN ENGINEERING CONTEXT , 1980 .

[14]  M. Knudsen Die Gesetze der Molekularstrmung und der inneren Reibungsstrmung der Gase durch Rhren , 1909 .

[15]  B. Z. Cybyk,et al.  Direct Simulation Monte Carlo: Recent Advances and Applications , 1998 .

[16]  K. Breuer,et al.  Gaseous slip flow in long microchannels , 1997 .

[17]  T. G. Cowling,et al.  The mathematical theory of non-uniform gases : notes added in 1951 , 1951 .

[18]  E. Gross,et al.  Kinetic Theory of Linear Shear Flow , 1958 .