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.
Toward Improved Prediction of Heat Transfer on Turbine Blades
Contributed by the International Gas Turbine Institute for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received by the IGTI, March 20, 2001; revised manuscript received October 15, 2001. Associate Editor: R. Bunker.
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Medic, G., and Durbin, P. A. (April 9, 2002). "Toward Improved Prediction of Heat Transfer on Turbine Blades ." ASME. J. Turbomach. April 2002; 124(2): 187–192. https://doi.org/10.1115/1.1458020
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