Transient Dean flow in a composite annular duct with porous walls partially filled with porous material

IF 5.4 2区 工程技术 Q1 ENGINEERING, AEROSPACE Propulsion and Power Research Pub Date : 2022-03-01 DOI:10.1016/j.jppr.2021.12.004
Basant K. Jha, Taiwo S. Yusuf
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引用次数: 2

Abstract

This work presents a semi-analytical solution of transient Dean flow in a composite annular duct with porous walls partially filled with porous materials. The flow is set up as a result of the imposed pressure gradient in the azimuthal (θ) direction while both the outer and the inner cylinders are fixed. The appropriate governing equations for the flow are rendered dimensionless and transformed using suitable techniques, the Laplace transform technique is further used to transform the partial differential equations into the total differential equation. The solution of the ODE is later transformed to the time domain using the well-known Riemann-sum approximation approach. To validate the accuracy of the numerical scheme deployed in this research, numerical comparison of the steady-state solution, and the values generated using the implicit finite difference on the transient state model is presented. Generally, higher dominance of clear fluid and fluid injection at the inner cylinder is found to enhance the fluid velocity at the fluid interface. It is also good to note that injection of fluid at the inner cylinder pose a decreasing influence on the flow with minimum or no effect near the point R = 1.7.

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多孔壁部分填充多孔材料的复合环形管道中的瞬态Dean流
本文提出了多孔壁部分填充多孔材料的复合环形管道中瞬态迪安流动的半解析解。流动是由于施加在方位(θ)方向上的压力梯度而形成的,而内外圆柱体都是固定的。将适当的流场控制方程进行无因次化和变换,利用拉普拉斯变换技术将偏微分方程转化为全微分方程。ODE的解随后用著名的黎曼和近似方法转换到时域。为了验证本研究中采用的数值格式的准确性,对稳态解和瞬态模型上使用隐式有限差分生成的值进行了数值比较。通常情况下,较高的清液优势和内缸的流体注入可以提高流体界面处的流体速度。同样值得注意的是,内气缸处注入的流体对流量的影响逐渐减小,在R = 1.7点附近影响最小或没有影响。
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
7.50
自引率
5.70%
发文量
30
期刊介绍: Propulsion and Power Research is a peer reviewed scientific journal in English established in 2012. The Journals publishes high quality original research articles and general reviews in fundamental research aspects of aeronautics/astronautics propulsion and power engineering, including, but not limited to, system, fluid mechanics, heat transfer, combustion, vibration and acoustics, solid mechanics and dynamics, control and so on. The journal serves as a platform for academic exchange by experts, scholars and researchers in these fields.
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