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Simulations of Micro Channel Gas Flows with Domain Decomposition Technique for Kinetic and Fluid Dynamics Equations

机译:用域分解技术模拟微通道气流的动力学和流体动力学方程。

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In the last 20 years many research papers have been reported about the development of domain decompositions for the kinetic and the fluid dynamic equations, see for example. From large to small scale geometries one may experience different degrees of rarefaction of a gas. The degrees of rarefaction of a gas can be measured by the Knudsen number Kn = λ/L, where λ is the mean free path and L is the characteristic length, for example the channel width. For Kn < 0.001, the flow is in the continuum regime, the compressible Navier-Stokes equations with no-slip boundary conditions are solved. For 0.001 < Kn < 0.1, the flow is in the slip regime, where the Navier-Stokes equations with velocity-slip and temperature jump conditions are solved. For Kn > 0.1 a kinetic type approach, based on the Boltzmann equation is required. We note that the kinetic approach is valid in the whole range of rarefaction of a gas. At standard conditions the mean free path of a gas in a micro- or nano channel is of the order L or larger, so the Knudsen number is no longer small. Therefore, the fluid dynamic equations, the compressible Euler or Navier-Stokes equations, cannot predict the flows correctly in a small scale geometry.
机译:在过去的20年中,已经报道了许多有关动力学方程和流体动力学方程的区域分解发展的研究论文,例如参见。从大型几何到小型几何,人们可能会遇到不同程度的气体稀化。气体的稀疏度可以通过克努森数Kn =λ/ L来测量,其中λ是平均自由程,L是特征长度,例如通道宽度。当Kn <0.001时,流体处于连续状态,求解了无滑移边界条件的可压缩Navier-Stokes方程。当0.001 <Kn <0.1时,流动处于滑移状态,求解带速度滑移和温度跳跃条件的Navier-Stokes方程。对于Kn> 0.1,需要基于Boltzmann方程的动力学方法。我们注意到,动力学方法在气体稀疏的整个范围内都是有效的。在标准条件下,微通道或纳通道中气体的平均自由程约为L或更大,因此Knudsen数不再小。因此,流体动力学方程,可压缩的Euler方程或Navier-Stokes方程无法在小规模几何结构中正确预测流量。

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