首页> 外文期刊>Frontiers in Heat and Mass Transfer >NEW SIMILARITY SOLUTION OF MICROPOLAR FLUID FLOW PROBLEM OVER AN UHSPR IN THE PRESENCE OF QUARTIC KIND OF AUTOCATALYTIC CHEMICAL REACTION
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NEW SIMILARITY SOLUTION OF MICROPOLAR FLUID FLOW PROBLEM OVER AN UHSPR IN THE PRESENCE OF QUARTIC KIND OF AUTOCATALYTIC CHEMICAL REACTION

机译:存在自催化化学反应的第四类超微粒子上超微流体流动问题的新的相似解

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The motion of air (i.e fluid) in which tiny particle rotates past a pointed surface of a rocket (as in space science), over a bonnet of a car and past a pointed surface of an aircraft is of important to experts in all these fields. Geometrically, all the domains of fluid flow in all these cases can be referred to as upper horizontal surface of a paraboloid of revolution (uhspr). Meanwhile, the solution of the corresponding partial differential equation is an open question due to unavailability of suitable similarity variable to non-dimensionalize the angular momentum equation. This article unravels the nature of skin friction coefficient, heat transfer rate, velocity, temperature, concentration of homogeneous bulk fluid and heterogeneous catalyst which exists on a stretchable surface which is neither a perfect horizontal/vertical nor inclined/cone. Theory of similarity solution was adopted to obtain the similarity variable suitable to scale the proposed angular momentum equation. These equations along with the boundary conditions are solved numerically using Runge-Kutta technique along with shooting method. The similarity variable successfully non-dimensionalized and parameterized the angular momentum for boundary layer flow past uhspr. Temperature dependent dynamic viscosity parameter increases vertical velocity near a free stream but reduces micro-rotation near uhspr. Effect of thermal radiation parameter on temperature profile and heat transfer rate can be greatly influenced by thickness parameter. Full Text: PDF DOI: http://dx.doi.org/10.5098/hmt.8.26 ISSN: 2151-8629 About Us | Contact Us | Terms of Use | Privacy Policy | Disclaimer
机译:对于所有这些领域的专家而言,微小颗粒在其中旋转的空气(即流体)运动经过火箭的尖端表面(如在太空科学中),经过汽车的引擎盖并经过飞机的尖端表面都是非常重要的。 。在几何学上,在所有这些情况下,流体流动的所有区域都可以称为旋转抛物面(uhspr)的上水平表面。同时,由于无法使用合适的相似变量来对角动量方程进行无量纲化,因此相应的偏微分方程的解是一个悬而未决的问题。本文揭示了存在于可拉伸表面上的皮肤摩擦系数,传热速率,速度,温度,均相本体流体和非均相催化剂浓度的性质,该表面既不是完美的水平/垂直也不是倾斜/圆锥形的。采用相似性解的理论来获得适合于缩放所提出的角动量方程的相似性变量。这些方程与边界条件一起使用Runge-Kutta技术和射击方法进行了数值求解。相似变量成功地对边界层流经过uhspr的角动量进行了无量纲化和参数化。温度相关的动态粘度参数会增加自由流附近的垂直速度,但会降低超高速附近的微旋转。厚度参数会极大地影响热辐射参数对温度分布和传热速率的影响。全文:PDF DOI:http://dx.doi.org/10.5098/hmt.8.26 ISSN:2151-8629关于我们|联系我们|使用条款|隐私政策|免责声明

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