Numerical Analysis of Boundary Layer Flow and Heat Transfer over a Stretching and Non-Stretching Bullet-Shaped Object

M. Ali, M. A. Alim
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Abstract

The two-dimensional axisymmetric magnetohydrodynamic boundary layer flow with heat transfer of Newtonian fluid over a stretching and non-stretching bullet-shaped object has been investigated. Therefore, fluid flow and heat transfer have been investigated in two types of flow geometries such as the thicker surface and the thinner surface of the bullet-shaped object. The present analysis also focuses on the physical relevance and accurate trends of the boundary layer profiles which are adequate in the laminar boundary layer flow. The novelty of this current work is to discuss the effect of shape and size (surface thickness parameter s) and the stretching factor of the bullet-shaped object on the fluid velocity and temperature profiles within the boundary layer region also develop the relationship between the dependent and independent parameters by the correlation coefficient. The partial differential equations of momentum and energy have been reduced to a system of non-linear ordinary differential equations along with the transformed boundary conditions by applying the local similarity transformations. These coupled non‐linear ordinary differential equations’ governing the flow field has been solved by the Spectral Quasi-Linearization Method (SQLM). The numerical analysis of the SQLM has been carried out with MATLAB for investigating the effect of various controlling parameters on the flow fields. The residual error infinity norms have been analyzed to determine the speed of convergence and accuracy of the method. The numerical results have been displayed graphically and in tabular form and the physical behavior of the problem also discussed. The investigation shows that in the case of a thicker bullet-shaped object the velocity profile does not approach the ambient condition asymptotically but intersects the axis with a steep angle and the boundary layer structure has no definite shape whereas in the case of a thinner bullet-shaped object the velocity profile converge the ambient condition asymptotically and the boundary layer structure has a definite shape. It is also noticed that thinner bullet-shaped object acts as good cooling conductor compared to thicker bullet-shaped object and the wall friction can be reduced much when thinner bullet-shaped object is used rather than the thicker bullet-shaped object in both types of non-stretching or stretching bullet-shaped object . Keywords: forced convection, correlation coefficient, multiple regression, MHD, stretching
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拉伸与非拉伸弹形物体边界层流动与传热的数值分析
研究了牛顿流体在拉伸和非拉伸弹形物体上的二维轴对称磁流体动力学边界层流动及其传热问题。因此,已经在两种类型的流动几何形状中研究了流体流动和传热,例如子弹形物体的较厚表面和较薄表面。本分析还侧重于边界层剖面的物理相关性和精确趋势,这在层流边界层流动中是足够的。目前这项工作的新颖之处在于讨论了子弹状物体的形状和尺寸(表面厚度参数s)以及拉伸因子对边界层区域内流体速度和温度分布的影响,并通过相关系数建立了相关参数和独立参数之间的关系。通过应用局部相似变换,动量和能量的偏微分方程与变换后的边界条件一起被简化为非线性常微分方程组。这些控制流场的耦合非线性常微分方程已通过谱拟线性化方法(SQLM)求解。利用MATLAB对SQLM进行了数值分析,研究了各种控制参数对流场的影响。分析了残差无穷大范数,以确定该方法的收敛速度和精度。数值结果以图表和表格的形式显示,并讨论了问题的物理行为。研究表明,在较厚的子弹形物体的情况下,速度剖面不会渐近地接近环境条件,而是以一个陡峭的角度与轴相交,并且边界层结构没有确定的形状,而在较薄的子弹形对象的情况下速度剖面渐近地收敛于环境条件,边界层这个结构有一个确定的形状。还注意到,与较厚的子弹形物体相比,较薄的子弹形对象起到了良好的冷却导体的作用,并且在两种类型的非拉伸或拉伸子弹形对象中,当使用较薄的弹头形对象而不是较厚的弹形对象时,壁摩擦可以大大降低。关键词:强迫对流,相关系数,多元回归,MHD,拉伸
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