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TECHNICAL PAPERS

Toward Improved Prediction of Heat Transfer on Turbine Blades

[+] Author and Article Information
G. Medic, P. A. Durbin

Mechanical Engineering Department, Stanford University, Stanford, CA 94305-3030

J. Turbomach 124(2), 187-192 (Apr 09, 2002) (6 pages) doi:10.1115/1.1458020 History: Received March 20, 2001; Revised October 15, 2001; Online April 09, 2002
Copyright © 2002 by ASME
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References

Figures

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Isentropic Mach number, Mis
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Heat transfer coefficient ht (W/m2 K)—(a) k−ε models, (b) k−ω models
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Turbulence intensity, k−ε model
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Turbulence intensity, k−ω model
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Turbulence intensity, Kato-Launder k−ε model
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T/Tlimk−ε model, higher inflow value of ε, lε=Cμ3/4k3/2/ε=0.001 m model is used in any particular application
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T/Tlim,k−ε model, lower inflow value of ε, lε=Cμ3/4k3/2/ε=0.01 m
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Turbulence intensity, v2−f model
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Turbulence intensity, T bound with k−ω model
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Turbulence intensity, T bound with k−ε model

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