A SIMULATION OF COMPRESSIBLE BOUNDARY-LAYER FLOW WITH HEAT TRANSFER AND PRESSURE GRADIENT

Author(s):  
Mohammad Reza Mohaghegh
2020 ◽  
Author(s):  
James Sucec

Abstract Stanton number, St, calculations as a function of position, x, are made for turbulent, external boundary layer flow over aerodynamically rough surfaces and also for a fully developed duct flow with rough top and bottom surfaces. This is accomplished with three different forms of generalized Reynolds analogies from the literature and also with a new data correlation developed with the aid of the thermal inner and outer layers. Comparison of these predicted values of St with experimental data, from the literature, is made for several favorable equilibrium, one non-equilibrium, and a zero pressure gradient as well as a duct flow over “real” roughness patterns. Predictions compare reasonably well with the data for some of the generalized Reynolds analogies.


2014 ◽  
Vol 6 (3) ◽  
pp. 1216-1226
Author(s):  
Sathyanarayana. S. B

The aim of this work is to obtain exact analytical solution to the two dimensional laminar compressible boundary layer flow with an adverse pressure gradient in the presence of heat and mass transfer with MHD. The method applied is homotopy analysis method. It is shown that this solution agrees very well with numerical solution which is obtained by Runge-Kutta Merson method and results are shown graphically for different magnetic parameters.


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