Discussion on “Higher Order Chemical Reaction and Radiation Effects on Magnetohydrodynamic Flow of a Maxwell Nanofluid With Cattaneo–Christov Heat Flux Model Over a Stretching Sheet in a Porous Medium” (Reddy Vinodkumar, M. and Lakshminarayana, P., 2022, ASME J. Fluids Eng., 144(4), p. 041204)

IF 1.8 3区 工程技术 Q3 ENGINEERING, MECHANICAL
Asterios Pantokratoras
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引用次数: 0

Abstract

The most important development in Fluid Mechanics during the 20th century was the concept of boundary layer flow introduced by Prandtl in Ref. [1]. A boundary layer is that layer of fluid which forms in the vicinity of a surface bounding the fluid. Every time a fluid moves along a surface a boundary layer near the surface appears. Therefore, boundary layers exist in the interior of water pipes, in sewer pipes, in irrigation channels, near the earth's surface, and around buildings due to winds, near airplane wings, around a moving car, at the river bottom, inside the blood vessels and so on. Therefore, it is a popular field in Fluid Mechanics for engineers, physicists, and mathematicians. Hundreds of papers are published each year in this field. However, errors appear in many papers. Four usual errors made in investigation of boundary layer flows have been analyzed by Pantokratoras in Ref. [2]. The most usual error is that concerning the truncation of velocity and temperature profiles, and this kind of errors exist in Ref. [3]. The analysis of errors in Ref. [3] follows.In Ref. [3] the boundary conditions (11) are as follows: (1)f′=0,θ=0,ϕ=0 asη→∞where f′ is the nondimensional fluid velocity, θ is the nondimensional temperature, and ϕ is the nondimensional concentration. In Eq. (1), η→∞ means a very long η.In Fig. 1 of the present work, the dimensionless temperature profile taken from Fig. 11 of Ref. [3] is shown. It is seen that the temperature profile from Ref. [3] does not approach the ambient condition asymptotically but intersects the horizontal axis with a steep angle (the profile by Ref. [3] is a straight line). At the same figure, it is shown a correct profile (sketch), proposed by the present author, which extends to high values of transverse component η and approaches smoothly the ambient condition. In Fig. 11 of Ref. [3], the calculations have been restricted to a maximum η equal to 5. It is obvious that this calculation domain is insufficient to capture the real shape of profile and a higher value of η is needed.According to above analysis, most of the curves in Figs. 3, 5, 6, 8–16, 18–21 in Ref. [3] are incorrect.The temperature gradient θ′(0)=∂θ(0)∂η at point A, which lies at the sheet, is quite different in the work presented in Ref. [3] and the corrected profile. This means that ALL −θ′(0) values in Tables 1–4 in Ref. [3] are wrong. More information on the truncation error is given by Pantokratoras in Ref. [4]. Recently a similar paper with truncated profiles has been retracted [5].From Fig. 1 of Ref. [3], it is clear that the x axis is horizontal, and the y axis is vertical. The horizontal momentum equation (2) in Ref. [3] is as follows: (2)u∂u∂x+v∂u∂y=υ∂2u∂y2−λ1(u2∂2u∂x2+2uv∂2u∂x∂y+v2∂2u∂y2)−υku−σB02uρ+g(βT(T−T∞)+βC(C−C∞)It is well known that gravity acts in the vertical direction. Therefore, the gravity term g(βT(T−T∞)+βC(C−C∞) in Eq. (2) must be zero. For the same reason, the gravity terms Grθ and Gcϕ in the transformed equation (8) in Ref. [3] must be zero.
“基于Cattaneo-Christov热流模型的麦克斯韦纳米流体在多孔介质中拉伸薄片上的高阶化学反应和辐射效应”的讨论(Reddy Vinodkumar, M.和Lakshminarayana, P., 2022, ASME J.流体工程。, 144(4), p. 041204)
20世纪流体力学最重要的发展是Prandtl在文献[1]中引入的边界层流动概念。边界层是在流体边界表面附近形成的流体层。每当流体沿着表面移动时,表面附近就会出现一个边界层。因此,边界层存在于水管内部、下水管道、灌溉渠、地表附近、建筑物周围、飞机机翼附近、移动的汽车周围、河底、血管内部等。因此,它是流体力学中工程师、物理学家和数学家的热门领域。这一领域每年发表数百篇论文。然而,错误出现在许多论文中。Pantokratoras在文献[2]中分析了边界层流动研究中常见的四种错误。最常见的误差是关于速度和温度剖面的截断,这类误差在文献[3]中存在。参考文献[3]中的误差分析如下。在文献[3]中,边界条件(11)如下:(1)f ' =0,θ=0,ϕ=0, η→∞,其中f '为无因次流体速度,θ为无因次温度,ϕ为无因次浓度。在式(1)中,η→∞表示一个很长的η。在本工作的图1中,显示了参考文献[3]的图11的无因次温度分布。可以看出,文献[3]中的温度廓线并不是渐近地接近环境条件,而是与水平轴以陡角相交(文献[3]中的温度廓线是一条直线)。在同一图中,显示了由作者提出的正确的轮廓(草图),该轮廓延伸到高的横向分量η值,并平滑地接近环境条件。在文献[3]的图11中,计算被限制为最大η等于5。显然,该计算域不足以反映实际的轮廓形状,需要更高的η值。根据以上分析,文献[3]中的图3、图5、图6、图8-16、图18-21中的大部分曲线是不正确的。在A点处的温度梯度θ′(0)=∂θ(0)∂η,位于薄片上,在文献[3]和修正后的剖面中有很大的不同。这意味着Ref.[3]中表1-4中的ALL−θ′(0)值是错误的。关于截断误差的更多信息由Pantokratoras在参考文献[4]中给出。最近,一篇类似的论文被删节了[5]。从文献[3]的图1可以看出,x轴是水平的,y轴是垂直的。参考[3]中的水平动量方程(2)如下:(2)u∂u∂x+v∂u∂y=υ∂2u∂y2−λ1(u2∂2u∂x2+2uv∂2u∂x∂y+v2∂2u∂y2)−ku−σB02uρ+g(βT(T−T∞)+βC(C−C∞)众所周知,重力在垂直方向上起作用。因此,Eq.(2)中的重力项g(βT(T−T∞)+βC(C−C∞)必须为零。出于同样的原因,文献[3]中变换后的方程(8)中的重力项Grθ和Gcϕ必须为零。
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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