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Advanced k-epsilon modeling of heat transferThis report describes two approaches to low Reynolds-number k-epsilon turbulence modeling which formulate the eddy viscosity on the wall-normal component of turbulence and a length scale. The wall-normal component of turbulence is computed via integration of the energy spectrum based on the local dissipation rate and is bounded by the isotropic condition. The models account for the anisotropy of the dissipation and the reduced mixing length due to the high strain rates present in the near-wall region. The turbulent kinetic energy and its dissipation rate were computed from the k and epsilon transport equations of Durbin. The models were tested for a wide range of turbulent flows and proved to be superior to other k-epsilon models, especially for nonequilibrium anisotropic flows. For the prediction of airfoil heat transfer, the models included a set of empirical correlations for predicting laminar-turbulent transition and laminar heat transfer augmentation due to the presence of freestream turbulence. The predictions of surface heat transfer were generally satisfactory.
Document ID
19950025002
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kwon, Okey
(Allison Engine Co. Indianapolis, IN, United States)
Ames, Forrest E.
(Allison Engine Co. Indianapolis, IN, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-9748
NAS 1.26:4679
NASA-CR-4679
Report Number: E-9748
Report Number: NAS 1.26:4679
Report Number: NASA-CR-4679
Accession Number
95N31423
Funding Number(s)
CONTRACT_GRANT: NAS3-25950
PROJECT: RTOP 505-62-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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