Effect of activation energy on mass transfer features of Powell-Eyring nanofluid via shrinking disk: Dual solutions and stability analysis

IF 6.7 2区 工程技术 Q1 ENGINEERING, AEROSPACE
Propulsion and Power Research Pub Date : 2026-06-01 Epub Date: 2026-04-28 DOI:10.1016/j.jppr.2026.02.009
Mudassar Qamar, Masood Khan, Syed Modassir Hussain
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引用次数: 0

Abstract

This study's main goal is to investigate the Darcy-Forchheimer model of Eyring-Powell nanofluid's mass and thermal transport mechanisms across a shrinking disk. Joule heating, magnetic field, thermophoresis, viscous dissipation, non-uniform energy sink/source, activation energy, and Brownian motion with convective constraint are all taken into account in the physical model. The non-linear ODEs model is tackled numerically and graphically with the help of the bvp4c approach. The key finding shows that a dual solution was performed in the region (χ>χci) for shrinking disk with varying values of distinct factors, while no solution occurs in the sector (χ<χci). It also found that the critical point (χci) stay constant at (−0.4277), despite variation of Rd(=0.3,0.4,0.5) and Ec(=2,2.5,3) against heat transportation rate. The heat transportation coefficient increases with the rising factor of the Powell fluid for the first solution. Furthermore, the mass curve shows a rising trend for both solutions with a positive variation in the value of energy activation. To identify which solution is stable or unstable, stability analysis is carried out.
活化能对Powell-Eyring纳米流体缩盘传质特性的影响:双溶液和稳定性分析
这项研究的主要目标是研究Eyring-Powell纳米流体的质量和热输运机制的Darcy-Forchheimer模型。物理模型考虑了焦耳加热、磁场、热激流、粘性耗散、非均匀能量汇/源、活化能和对流约束下的布朗运动。利用bvp4c方法对非线性ode模型进行了数值和图形化处理。关键发现表明,对于具有不同因子值的收缩盘,在区域(χ>χci)中执行了双重解决,而在扇区中没有解决(χ<χci)。研究还发现,尽管Rd(=0.3,0.4,0.5)和Ec(=2,2.5,3)随热传递率的变化而变化,但临界点(χci)保持不变,为(- 0.4277)。对于第一种溶液,传热系数随鲍威尔流体体积的增大而增大。此外,两种解的质量曲线均呈上升趋势,能量活化值呈正变化。为了确定哪个溶液是稳定的或不稳定的,进行稳定性分析。
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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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