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DSMC-Based Shear-Stress/Velocity-Slip Boundary Condition for Navier-Stokes Couette-Flow Simulations

机译:基于DSMC的剪切应力/速度滑动边界条件,适用于Navier-Stokes Coute-Flow模拟

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Direct Simulation Monte Carlo (DSMC) simulations are used to develop a shear-stress/velocity-slip boundary condition for Navier-Stokes (NS) simulations of low-speed isothermal Couette flow. In this boundary condition, the wall shear stress equals the product of the difference between the gas and wall velocities and a momentum transfer coefficient. This momentum transfer coefficient depends on two dimensionless parameters that determine its behavior in the near-continuum and transitional regimes, respectively. For a given gas, these parameters are determined by comparing the NS Couette-flow shear-stress expression to DSMC shear-stress values for free-molecular to near-continuum pressures with three values of the accommodation coefficient. The parameter values for argon, helium, nitrogen, air, and inverse-power-law (IPL) interactions from hard-sphere to Maxwell lie within narrow ranges. For the hard-sphere interaction, the DSMC-based results are in excellent agreement with previously published analytical approximations.
机译:直接仿真蒙特卡罗(DSMC)模拟用于为Navier-Stokes(NS)模拟的剪切应力/速度滑动边界条件进行低速等温沟槽流动。在这种边界条件下,壁剪切应力等于气体和壁速度之间的差异和动量传递系数。这种动量传递系数取决于两种无量纲参数,可分别确定其在近连续和过渡方案中的行为。对于给定的气体,通过将NS Coute-Fource剪切应激表达与具有三个容纳系数的三个值的三个值进行比较,通过将NS Coute-Fourfet-Flow剪切应激表达与DSMC剪切应力值进行比较来确定这些参数。氩气,氦气,氮气,空气和逆幂(IPL)与麦克斯韦尔的相互作用的参数值在窄范围内。对于硬球相互作用,基于DSMC的结果与先前公布的分析近似值非常一致。

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