contributor author | Ling, Julia | |
contributor author | Ryan, Kevin J. | |
contributor author | Bodart, Julien | |
contributor author | Eaton, John K. | |
date accessioned | 2017-05-09T01:33:59Z | |
date available | 2017-05-09T01:33:59Z | |
date issued | 2016 | |
identifier issn | 0889-504X | |
identifier other | turbo_138_01_011006.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/162730 | |
description abstract | Algebraic closures for the turbulent scalar fluxes were evaluated for a discrete hole film cooling geometry using the results from a highfidelity 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 higherorder 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 Reynoldsaveraged 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Analysis of Turbulent Scalar Flux Models for a Discrete Hole Film Cooling Flow | |
type | Journal Paper | |
journal volume | 138 | |
journal issue | 1 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4031698 | |
journal fristpage | 11006 | |
journal lastpage | 11006 | |
identifier eissn | 1528-8900 | |
tree | Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 001 | |
contenttype | Fulltext | |