The present research investigates boundary layer heat transfer with very high freestream turbulence, a problem of primary interest in the gas turbine industry where existing boundary layer correlations and codes underpredict local heat transfer rates on first-stage turbine blades and vanes by as much as a factor of three for some engine designs. The problem was studied experimentally by placing a constant-temperature heat transfer surface at various locations in the margin of a turbulent free jet and measuring both the surface heat transfer rate and the turbulence in the free stream. In this experiment, free-stream turbulent fluctuations 20 to 60 percent relative to the mean velocity augment heat transfer 1.8 to 4 times that which would be predicted locally using accepted correlations for turbulent boundary layers at the same Reynolds number.
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Heat Transfer With Very High Free-Stream Turbulence: Part I—Experimental Data
P. K. Maciejewski,
P. K. Maciejewski
Mechanical Engineering Department, University of Pittsburgh, Pittsburgh, PA 15261
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R. J. Moffat
R. J. Moffat
Department of Mechanical Engineering, Stanford University, Stanford, CA 94305
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P. K. Maciejewski
Mechanical Engineering Department, University of Pittsburgh, Pittsburgh, PA 15261
R. J. Moffat
Department of Mechanical Engineering, Stanford University, Stanford, CA 94305
J. Heat Transfer. Nov 1992, 114(4): 827-833 (7 pages)
Published Online: November 1, 1992
Article history
Received:
April 1, 1991
Revised:
April 1, 1992
Online:
May 23, 2008
Citation
Maciejewski, P. K., and Moffat, R. J. (November 1, 1992). "Heat Transfer With Very High Free-Stream Turbulence: Part I—Experimental Data." ASME. J. Heat Transfer. November 1992; 114(4): 827–833. https://doi.org/10.1115/1.2911889
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