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Thermal rarefied gas flow investigations through micro/nano backward-facing step : Comparison of DSMC and CFD subject to hybrid slip and jump boundary conditions

机译:通过微/纳米后向步骤进行热稀有气体流量研究:混合滑移和跃变边界条件下DSMC和CFD的比较

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摘要

This paper evaluates the suitability of a newly developed hybrid “Langmuir-Maxwell” and “Langmuir-Smoluchowski” slip/jump boundary conditions in the Navier-Stokes-Fourier equations for nano/micro backward-facing step geometry flow which experiences separation and reattachment. Additionally, this paper investigates the effect of different parameters such as step pressure ratio, inflow temperature and wall temperature on the separation zone in the nano/micro step geometry. We chose nitrogen as the working gas and use two DSMC solvers to assess the accuracy of the CFD solutions. DSMC results showed that the increase of the inlet temperatures extends the length of the separation zone and raises the mass flow rate. The change of pressure ratio does not affect the separation length while the increase of the step wall temperature decreases the length of this zone for both CFD and DSMC results. Compared to the DSMC results, the hybrid slip/jump boundary conditions predict better surface pressure, surface gas temperature and slip velocity in the separation zone than the standard Maxwell/Smoluchowski boundary conditions.
机译:本文评估了新开发的混合“ Langmuir-Maxwell”和“ Langmuir-Smoluchowski”滑移/跳跃边界条件在Navier-Stokes-Fourier方程中对经历分离和重新附着的纳米/微后向台阶几何流动的适用性。此外,本文研究了不同参数(例如阶跃压力比,流入温度和壁温)对纳米/微阶几何中分离区的影响。我们选择氮气作为工作气体,并使用两个DSMC求解器来评估CFD解决方案的准确性。 DSMC结果表明,入口温度的升高延长了分离区的长度,并提高了质量流速。对于CFD和DSMC结果,压力比的变化不会影响分离长度,而台阶壁温度的升高会减小该区域的长度。与DSMC结果相比,混合滑移/跳跃边界条件预测的分离区中的表面压力,地表气体温度和滑移速度要比标准Maxwell / Smoluchowski边界条件更好。

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