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A kappa-epsilon calculation of transitional boundary layersA recently proposed kappa-epsilon model for low Reynolds number turbulent flows was modified by introducing a new damping function f(sub mu). The modified model is used to calculate the transitional boundary layer over a flat plate with different freestream turbulence levels. It is found that the model could mimic the transitional flow. However, the predicted transition is found to be sensitive to the initial conditions.
Document ID
19920013155
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Yang, Z.
(NASA Lewis Research Center Cleveland, OH, United States)
Shih, T. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
CMOTT-92-05
NASA-TM-105604
NAS 1.15:105604
E-6939
ICOMP-92-08
Report Number: CMOTT-92-05
Report Number: NASA-TM-105604
Report Number: NAS 1.15:105604
Report Number: E-6939
Report Number: ICOMP-92-08
Accession Number
92N22398
Funding Number(s)
CONTRACT_GRANT: NASA ORDER C-99066-G
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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