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TECHNICAL PAPERS: Gas Turbines: Heat Transfer

The Two-Flux Model Applied to Radiative Transfer and Forced Convection in the Laminar Boundary Layer on a Flat Plate

[+] Author and Article Information
F. Malpica

Departamento de Termodinámica y, Fenómenos de Transferencia, Universidad Simón Bolivar, Caracas AP 89000, Venezuela

N. Moreno, A. Tremante

Departamento de Conversión y Transporte de Energia, Universidad Simón Bolivar, Caracas AP 89000, Venezuela

J. Eng. Gas Turbines Power 125(3), 734-741 (Aug 15, 2003) (8 pages) doi:10.1115/1.1496775 History: Received August 01, 2000; Revised April 01, 2001; Online August 15, 2003
Copyright © 2003 by ASME
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References

Figures

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Geometry of the physical model and the coordinate system
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Temperature profiles over flat-plate forced convection comparison with optically thin approximation. A=3,θ=0.5,Wo=0.0,Pr=1.0,N=0.1,εw=1.0.
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Temperature profiles over flat-plate forced convection, two-flux method (A=3) compared with thick limit. θ=0.5,Wo=0.0,Pr=1.0,N=0.1,εw=1.0.
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Temperature profiles over flat-plate forced convection. Effect of scattering, Wo=0.5,Pr=1.0,N=0.1,εw=1.0,A=3.
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(a) Temperature gradients across the boundary layer. Effect of ξ. Pr=1.0,εw=1.0,θ=0.5,E=0.0,Wo=0.0,A=3. (b) Temperature gradients across the boundary layer. Effect of parameter ξ. Pr=1.0,εw=1.0,θ=0.5,E=0.0,Wo=0.0,A=3. (c) Temperature gradients across the boundary layer. Effect of ξ. Pr=1.0,εw=1.0,θ=0.5,E=0.0,Wo=0.0,A=3.
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(a) Effect of parameter ξ on radiative heat flux across the boundary layer. Pr=1.0,εw=1.0,θ=0.5,E=0.0,Wo=0.0,A=3. (b) Effect of parameter ξ on radiative heat flux across the boundary layer. Pr=1.0,εw=1.0,θ=0.5,E=0.0,Wo=0.0,A=3. (c) Effect of parameter ξ on radiative heat flux across the boundary layer. Pr=1.0,εw=1.0,θ=0.5,E=0.0,Wo=0.0,A=3.
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Total heat flux coefficient (convection+radiation)Pr=1.0,εw=1.0,E=0.0,Wo=0.0,A=3

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