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Similarity solution and Runge Kutta method to a thermal boundary layer model at the entrance region of a circular tube: the Leveque approximation)

Wan Omar, Wan Zaidi and Belhocine, Ali (2018) Similarity solution and Runge Kutta method to a thermal boundary layer model at the entrance region of a circular tube: the Leveque approximation). Revista Cientifica Semana Academica, 31 (1). pp. 6-18. ISSN 0124-2253

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Abstract

In the thermal entrance region, a thermal boundary layer develops and also reaches the circular tube center. The fully developed region is the zone in which the flow is both hydrodynamically and thermally developed. The heat flux will be higher near the inlet because the heat transfer coefficient is highest at the tube inlet where the thickness of the thermal boundary layer is zero, and decreases gradually to the fully developed value. In this paper, the assumptions implicit in Leveque's approximation are re-examined, and the analytical solution of the problem with additional boundary conditions, for the temperature field and the boundary layer thickness through the long tube is presented. By defining a similarity variable, the governing equations are reduced to a dimensionless equation with an analytic solution in the entrance region. This report gives justification for the similarity variable via scaling analysis, details the process of converting to a similarity form, and presents a similarity solution. The analytical solutions are then checked against numerical solution programming by Fortran code obtained via using Runge-Kutta fourth order (RK4) method. Finally, others important thermal results obtained from this analysis, such as; approximate Nusselt number in the thermal entrance region was discussed in detail.

Item Type:Article
Uncontrolled Keywords:thermal boundary layer, dimensionless variables
Subjects:T Technology > TJ Mechanical engineering and machinery
Divisions:Mechanical Engineering
ID Code:82328
Deposited By: Siti Nor Hashidah Zakaria
Deposited On:30 Sep 2019 09:00
Last Modified:25 Nov 2019 07:15

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