Toward Improved Prediction of Heat Transfer on Turbine Blades-Reference-Cited by-同舟云学术

Toward Improved Prediction of Heat Transfer on Turbine Blades

Published:2002-04-01 Issue:2 Volume:124 Page:187-192
ISSN:0889-504X
Container-title:Journal of Turbomachinery
language:en
Short-container-title:

Author:

Medic G.¹,Durbin P. A.²

Affiliation:

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

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

Abstract

Abstract Reynolds averaged computations of turbulent flow in a transonic turbine passage are presented to illustrate a manner in which widely used turbulence models sometimes provide poor heat transfer predictions. It is shown that simple, physically and mathematically based constraints can substantially improve those predictions.

Publisher

ASME International

Subject

Mechanical Engineering

Link

https://asmedigitalcollection.asme.org/turbomachinery/article-pdf/124/2/187/6838112/187_1.pdf

Reference14 articles.

1. Prakash, C., 1995, “Some Experiences With the Standard k−ε, RNG and Chen Turbulence Models,” National Turbulent Combustion Model Meeting, NASA Lewis, July 27–28.

2. Durbin, P. A. , 1996, “On the k−ε Stagnation Point Anomaly,” Int. J. Heat Fluid Flow, 17, pp. 89–90.

3. Behnia, M., Parneix, S., Shabany, Y., and Durbin, P. A., 1999, “Numerical Study of Turbulent Heat Transfer in Confined and Unconfined Impinging Jets,” Int. J. Heat Fluid Flow, 20, pp. 1–9.

4. Kato, M., and Launder, B. E., 1993, “Modelling Flow-Induced Oscillations in Turbulent Flow Around a Square Cylinder,” ASME FED 157, pp. 189–199.

5. Camci, C., and Arts, T., 1985, “Short Duration Measurements and Numerical Simulation of Heat Transfer Along the Suction Side of a Film-Cooled Gas Turbine Blade,” ASME J. Eng. Power, 107, pp. 991–997.

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