Flow Characterization of Bluff Bodies: A Two-Dimensional Transformation From Square to Triangular Cylinder

IF 1.8 3区 工程技术 Q3 ENGINEERING, MECHANICAL Journal of Fluids Engineering-Transactions of the Asme Pub Date : 2021-05-31 DOI:10.1115/1.4051310
R. Borah, Siddhant Jain, Dyuman V. Joshi, U. Saha
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引用次数: 1

Abstract

In the present study, two-dimensional unsteady, incompressible flow around a square body that is being transformed into a vertex oriented towards the flow configuration of a triangular body is numerically investigated at Re =100 using ANSYS FLUENT 19.0 software. The purpose is to explore the effect of this transformation on the wake characteristics of a square body with l/d = 1 to a triangular body with l/d = 0; where l is the length of lateral and front surface, and d is the body height. The effect on the flow behavior caused by the leading-edge transformation from the prospect of wake width, recirculation length and stagnation pressure difference is discussed. It is seen that as the l/d ratio decreases, the vortex strength increases which is attributed to the higher stagnation pressure difference value resulting in more intense rolling of the shedding vortex and a smaller wake width. For lower l/d, the fluid traverses a longer distance along the lateral surfaces resulting in greater loss of momentum and hence the lower vortex formation length. The mean drag coefficient is found to be minimum for l/d = 0.75 with stagnation pressure difference and recirculation length being the more dominating factor on this variation. The flow in all the cases separates at the rear surface and the general trend of decrease in drag coefficient with decrease in wake width is not followed. However, such modification leads to better aerodynamic outcome by weakening the periodic drag and lift forces.
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钝体的流动特性:从正方形到三角形圆柱体的二维变换
本文利用ANSYS FLUENT 19.0软件,在Re =100时,数值研究了二维非定常不可压缩绕方形体的流动,并将其转化为面向三角形体流动构型的顶点。目的是探讨这种变换对l/d = 1的正方形体到l/d = 0的三角形体的尾迹特性的影响;式中,l为侧前表面长度,d为车身高度。从尾迹宽度、再循环长度和滞止压差的角度讨论了前缘变换对流动特性的影响。可以看出,随着l/d比的减小,涡强度增大,这是由于滞止压差值越高,导致脱落涡的滚动越剧烈,尾迹宽度越小。当l/d较低时,流体沿侧向表面移动的距离较长,导致动量损失较大,因此涡流形成长度较短。平均阻力系数在l/d = 0.75时最小,滞止压力差和再循环长度是影响阻力系数变化的主要因素。所有情况下的气流均在后表面分离,阻力系数随尾迹宽度的减小而减小的总体趋势不一致。然而,这种修改通过削弱周期性阻力和升力导致更好的空气动力学结果。
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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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