Effect of Compressibility on Velocity Profile and Friction Factor of Gaseous Laminar Flows in a Microtube

IF 1.8 3区 工程技术 Q3 ENGINEERING, MECHANICAL
S. Murakami, Kaoru Toyoda, Y. Asako
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引用次数: 2

Abstract

Laminar flow of nitrogen gas in a microtube was simulated numerically to obtain velocity profile and Fanning friction factor in a quasi-fully developed region. The numerical procedure based on Arbitrary-Lagrangian-Eulerian method solved two-dimensional compressible momentum and energy equations. The computations were performed for a wide range of Reynolds number in laminar flow regime with adiabatic wall condition. It was found that the velocity profile deviates from the parabola as Mach number increases, and the product of Fanning friction factor and Reynolds number is not a constant but a function of only Mach number. To explain the compressibility effect, a new theoretical flow model which gives the velocity profile of gaseous laminar flows in a microtube was proposed under the assumption of purely axial flow. The theoretical velocity profile is taking radial-direction density change into account, and coincides with the numerically obtained velocity profile. The proposed flow model also shows that the Fanning friction factor of a compressible flow in a microtube is expressed by a quadratic function of Mach number. The coefficient of the Mach squared term is 40% of the numerically obtained correlation. The compressibility effect on friction factor of gaseous laminar flows in a microtube partly results from velocity profile change which must occur to keep the mass velocity profile when density changes in radial direction. The remainder of the compressibility effect can be considered to result from actual mass transfer in the radial direction whose existence was demonstrated by the numerical results.
可压缩性对微管内气体层流速度分布和摩擦系数的影响
对氮气在微管中的层流进行了数值模拟,得到了准完全发育区域的速度分布和范宁摩擦系数。基于任意拉格朗日-欧拉方法的数值计算程序求解了二维可压缩动量和能量方程。在具有绝热壁条件的层流流态下,对大范围的雷诺数进行了计算。随着马赫数的增加,速度分布偏离抛物线,范宁摩擦系数与雷诺数的乘积不是一个常数,而只是马赫数的函数。为了解释可压缩性效应,在纯轴向流动假设下,提出了一种新的理论流动模型,给出了微管内气体层流的速度分布。理论速度剖面考虑了径向密度变化,与数值计算速度剖面吻合。该流动模型还表明,微管内可压缩流动的范宁摩擦系数可以用马赫数的二次函数表示。马赫平方项的系数是数值计算得到的相关系数的40%。微管内气体层流的可压缩性对摩擦因数的影响部分是由于当密度在径向方向发生变化时,为了保持质量速度分布,必须发生速度分布的变化。剩余的可压缩性效应可以认为是由径向的实际传质引起的,其存在已被数值结果所证实。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
4.60
自引率
10.00%
发文量
165
审稿时长
5.0 months
期刊介绍: Multiphase flows; Pumps; Aerodynamics; Boundary layers; Bubbly flows; Cavitation; Compressible flows; Convective heat/mass transfer as it is affected by fluid flow; Duct and pipe flows; Free shear layers; Flows in biological systems; Fluid-structure interaction; Fluid transients and wave motion; Jets; Naval hydrodynamics; Sprays; Stability and transition; Turbulence wakes microfluidics and other fundamental/applied fluid mechanical phenomena and processes
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