Algebraic closures for the turbulent scalar fluxes were evaluated for a discrete hole film cooling geometry using the results from a high-fidelity large eddy simulation (LES). Several models for the turbulent scalar fluxes exist, including the widely used gradient diffusion hypothesis (GDH), the generalized GDH (GGDH), and the higher-order GDH (HOGGDH). By analyzing the results from the LES, it was possible to isolate the error due to these turbulent mixing models. Distributions of the turbulent diffusivity, turbulent viscosity, and turbulent Prandtl number were extracted from the LES results. It was shown that the turbulent Prandtl number varies significantly spatially, undermining the applicability of the Reynolds analogy for this flow. The LES velocity field and Reynolds stresses were fed into a Reynolds-averaged Navier–Stokes (RANS) solver to calculate the fluid temperature distribution. This analysis revealed in which regions of the flow various modeling assumptions were invalid and what effect those assumptions had on the predicted temperature distribution.
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January 2016
Research-Article
Analysis of Turbulent Scalar Flux Models for a Discrete Hole Film Cooling Flow
Kevin J. Ryan,
Kevin J. Ryan
Mechanical Engineering Department,
Stanford University,
Stanford, CA 94305
Stanford University,
Stanford, CA 94305
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Julien Bodart,
Julien Bodart
ISAE,
University of Toulouse,
Toulouse 31400, France
University of Toulouse,
Toulouse 31400, France
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John K. Eaton
John K. Eaton
Mechanical Engineering Department,
Stanford University,
Stanford, CA 94305
Stanford University,
Stanford, CA 94305
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Julia Ling
Kevin J. Ryan
Mechanical Engineering Department,
Stanford University,
Stanford, CA 94305
Stanford University,
Stanford, CA 94305
Julien Bodart
ISAE,
University of Toulouse,
Toulouse 31400, France
University of Toulouse,
Toulouse 31400, France
John K. Eaton
Mechanical Engineering Department,
Stanford University,
Stanford, CA 94305
Stanford University,
Stanford, CA 94305
1J. Ling is currently at Sandia National Labs.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received August 20, 2015; final manuscript received September 8, 2015; published online October 21, 2015. Editor: Kenneth C. Hall.
J. Turbomach. Jan 2016, 138(1): 011006 (7 pages)
Published Online: October 21, 2015
Article history
Received:
August 20, 2015
Revised:
September 8, 2015
Citation
Ling, J., Ryan, K. J., Bodart, J., and Eaton, J. K. (October 21, 2015). "Analysis of Turbulent Scalar Flux Models for a Discrete Hole Film Cooling Flow." ASME. J. Turbomach. January 2016; 138(1): 011006. https://doi.org/10.1115/1.4031698
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