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Compressible Gas Flow Inside a Two-Dimensional Uniform Microchannel

机译:二维均匀微通道内的可压缩气流

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This paper analyzes a compressible gas flow through a microchannel, and reports a complete set of first-order analytical solutions. This work represents an extension of the previous work of Arkilic on compressible flows through a microchannel. First, by comparing the magnitudes of different forces in the compressible gas flow, we obtain proper estimations for the Reynolds and Mach numbers at the channel exit. Second, based on these estimations, we obtain asymptotic analytical solutions of velocities, pressure, and temperature distributions of compressible gas flow inside the microchannel with a relaxation of the isothermal assumption, which was previously used by many researchers. Numerical simulations of compressible flows through microchannels with a compressible Navier-Stokes equation solver are performed and combined with velocity slip and temperature jump wall boundary conditions. The numerical simulation results validate the analytical results from this study.
机译:本文分析了通过微通道的可压缩气流,并报告了一整套完整的一阶分析解决方案。这项工作代表了Arkilic先前关于通过微通道的可压缩流的工作的扩展。首先,通过比较可压缩气流中不同力的大小,我们获得了通道出口处雷诺数和马赫数的适当估计。其次,基于这些估计,我们获得了等温线松弛的微通道内部可压缩气流的速度,压力和温度分布的渐近解析解,这是许多研究人员先前使用的。使用可压缩的Navier-Stokes方程求解器对通过微通道的可压缩流动进行了数值模拟,并与速度滑移和温度跃变壁边界条件相结合。数值模拟结果验证了本研究的分析结果。

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