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Heat Transfer on a Flat Plate with Uniform and Step Temperature DistributionsHeat transfer associated with turbulent flow on a step-heated or cooled section of a flat plate at zero angle of attack with an insulated starting section was computationally modeled using the GASP Navier-Stokes code. The algebraic eddy viscosity model of Baldwin-Lomax and the turbulent two-equation models, the K- model and the Shear Stress Turbulent model (SST), were employed. The variations from uniformity of the imposed experimental temperature profile were incorporated in the computations. The computations yielded satisfactory agreement with the experimental results for all three models. The Baldwin- Lomax model showed the closest agreement in heat transfer, whereas the SST model was higher and the K-omega model was yet higher than the experiments. In addition to the step temperature distribution case, computations were also carried out for a uniformly heated or cooled plate. The SST model showed the closest agreement with the Von Karman analogy, whereas the K-omega model was higher and the Baldwin-Lomax was lower.
Document ID
20050186543
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Bahrami, Parviz A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
May 16, 2005
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2005-212841
A-0513611
Report Number: NASA/TM-2005-212841
Report Number: A-0513611
Funding Number(s)
OTHER: 376-70-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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