Generaleristics of unsteady MHD temperature boundary layer

2015 ◽  
Vol 73 ◽  
pp. 75-84 ◽  
Author(s):  
Dragiša Nikodijević ◽  
Živojin Stamenković
2019 ◽  
Vol 213 ◽  
pp. 02002
Author(s):  
Pavel Antoš ◽  
Sergei Kuznetsov

Boundary layer on a uniformly heated flat plate was studied experimentally. Both, the velocity boundary layer and the temperature boundary layer, was investigated by means of hot-wire anemometry. A probe with parallel wires was used for velocity-temperature measurement. Experiment was performed in the closed-circuit wind tunnel with several levels of heat flux at the wall. The wall temperature was set up in the interval from 20 ºC to 200 ºC.


1978 ◽  
Vol 15 (3) ◽  
pp. 289-300 ◽  
Author(s):  
Th. Foken ◽  
S. A. Kitajgorodskij ◽  
O. A. Kuznecov

Author(s):  
Leizhi Wang ◽  
Yongjun Zhou ◽  
Zhaobo Chen

AbstractThe heat transfer of a reactor with improved Intermig impellers was numerically investigated by the finite element method (FEM) simulation software Fluent (V.19). A turbulence model utilized the standard k-ε model, and the turbulent flows in two large vortexes between vertical tubes were collided to form a strong convection. The influence of heat and mass transfer developing from the impeller diameters, the distance between the two impellers (C1), the rotational speed and the installation height of the bottom impeller (C2) were studied. The reactor was equipped with special structure vertical tubes to increase the heat exchange areas. The rate of heat transfer, including criteria such as the convective heat transfer coefficient, the Nusselt number of outside vertical tubes, and the temperature boundary layer thickness, assured the accurate control of the heat exchange mixing state. The experimental testing platform was designed to validate the simulated results, which revealed the influence order of related factors. The Nusselt number Nu was affected by various related factors, resulting in the rotation and diameter of impellers extending far beyond the distance between the two impellers (C1) and the installation height of the impeller (C2). The average temperature boundary layer thicknesses of the symmetrical and middle sections were 3.24 mm and 3.48 mm, respectively. Adjusting the appropriate parameters can accurately control the heat exchange process in such a reactor, and the conclusions provide a significant reference for engineering applications.


1977 ◽  
Vol 44 (3) ◽  
pp. 396-400 ◽  
Author(s):  
D. B. Ingham

The thermal boundary layer over a semi-infinite flat plate is investigated. For time t < 0 there is the Blasius boundary layer and no thermal boundary layer. At t = 0, a temperature boundary layer is initiated without altering the velocity and the subsequent temperature boundary layer is studied for all time. The resulting linear, singular parabolic partial differential equation is solved using an efficient numerical method. Numerical results for several values of the Prandtl number are compared with analytical and numerical results obtained by previous authors. Because of the large interest shown recently in impulsive problems which result in the solution of singular parabolic equations the method is extended to study some of these problems. In two of the examples considered the governing equations are nonlinear.


2003 ◽  
pp. 247-264 ◽  
Author(s):  
Mira Miric-Milosavljevic ◽  
Milos Pavlovic

In the paper the universal governing equations of incompressible laminar temperature boundary layer on the sphere are obtained using the improved method of general similarity for the case of adiabatic boundary conditions. Universal solutions in one parametric approximation for Pr=1 and Pr=0.72 are obtained by numerical integration. Calculated universal functions for temperature boundary layer are presented graphically. As an example eigen-temperature of the sphere are calculated and discussed.


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