The Role of the Turbulent Prandtl Number in Turbine Blade Heat Transfer Prediction
Author(s) -
Kevin Whitaker
Publication year - 1990
Publication title -
sae technical papers on cd-rom/sae technical paper series
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.295
H-Index - 107
eISSN - 1083-4958
pISSN - 0148-7191
DOI - 10.4271/901810
Subject(s) - turbulent prandtl number , prandtl number , turbine blade , turbulence , heat transfer , mechanics , blade (archaeology) , magnetic prandtl number , turbine , gas turbines , environmental science , mechanical engineering , physics , thermodynamics , materials science , aerospace engineering , engineering , nusselt number , reynolds number
Improvement of the prediction of external (gas-to-blade) heat transfer coefficients in gas turbine engines was undertaken. The effects of improved eddy diffusivity of heat modeling in the turbulence model was specifically investigated. A two-dimensional boundary STAN5, was selected and modified by incorporating several different turbulent Prandtl number models. Results indicated that slight effects were attributable to the modified turbulence model. Boundary layer character appeared to be much more significant.
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