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A Comparison of Data Reduction Methods for Average Friction Factor Calculation of Adiabatic Gas Flows in Microchannels

机译:微通道绝热气流平均摩擦系数计算的数据约简方法比较

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摘要

In this paper, a combined numerical and experimental approach for the estimation of the average friction factor along adiabatic microchannels with compressible gas flows is presented. Pressure-drop experiments are performed for a rectangular microchannel with a hydraulic diameter of 295 μm by varying Reynolds number up to 17,000. In parallel, the calculation of friction factor has been repeated numerically and results are compared with the experimental work. The validated numerical model was also used to gain an insight of flow physics by varying the aspect ratio and hydraulic diameter of rectangular microchannels with respect to the channel tested experimentally. This was done with an aim of verifying the role of minor loss coefficients for the estimation of the average friction factor. To have laminar, transitional, and turbulent regimes captured, numerical analysis has been performed by varying Reynolds number from 200 to 20,000. Comparison of numerically and experimentally calculated gas flow characteristics has shown that adiabatic wall treatment (Fanno flow) results in better agreement of average friction factor values with conventional theory than the isothermal treatment of gas along the microchannel. The use of a constant value for minor loss coefficients available in the literature is not recommended for microflows as they change from one assembly to the other and their accurate estimation for compressible flows requires a coupling of numerical analysis with experimental data reduction. Results presented in this work demonstrate how an adiabatic wall treatment along the length of the channel coupled with the assumption of an isentropic flow from manifold to microchannel inlet results in a self-sustained experimental data reduction method for the accurate estimation of friction factor values even in presence of significant compressibility effects. Results also demonstrate that both the assumption of perfect expansion and consequently wrong estimation of average temperature between inlet and outlet of a microchannel can be responsible for an apparent increase in experimental average friction factor in choked flow regime.
机译:本文提出了一种结合数值和实验方法的方法,用于估算绝热微通道中具有可压缩气流的平均摩擦系数。通过改变最大雷诺数为17,000的水力直径为295μm的矩形微通道进行压降实验。同时,数值上重复了摩擦系数的计算,并将结果与​​实验工作进行了比较。经过验证的数值模型还可以通过改变矩形微通道相对于实验通道的纵横比和水力直径来获得流动物理学的见解。这样做的目的是验证次要损耗系数在估计平均摩擦因数中的作用。为了捕获层流,过渡和湍流状态,已通过将雷诺数从200更改为20,000进行了数值分析。数值计算和实验计算的气体流动特性的比较表明,绝热壁处理(Fanno流动)比沿微通道的气体等温处理能更好地使平均摩擦系数值与传统理论一致。对于微流,不建议使用文献中可用的较小损耗系数的常数,因为它们会从一个组件变为另一个组件,并且要对可压缩流进行精确估算,需要将数值分析与实验数据精简结合起来。这项工作中提出的结果表明,沿通道长度的绝热壁处理以及假设从歧管到微通道入口的等熵流的假设如何导致一种可独立维持的实验数据缩减方法,即使在管道中也能准确估算摩擦系数值。存在明显的压缩效果。结果还表明,完全膨胀的假设以及因此对微通道入口和出口之间的平均温度的错误估计都可能导致cho流状态下实验平均摩擦系数的明显增加。

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