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Low-Reynolds-number k-epsilon model for unsteady turbulent boundary-layer flowsAn assessment of the near-wall and low-Reynolds-number functions used in low-Reynolds-number k-epsilon models suggests that they are not suitable for the near-wall region of unsteady turbulent boundary layers, where the flow is characterized by rapid changes in phase. An improved low-Reynolds-number k-epsilon model is developed in this paper. The near-wall and low-Reynolds-number functions in this model are formulated as functions of the local turbulent Reynolds numbers instead of the inner variable y(+). The present model also has the correct asymptotic behavior in the near-wall region. The turbulence model has been incorporated in an unsteady boundary-layer code and validated for unsteady turbulent boundary layers with and without adverse pressure gradients. The predictions agree well with the experimental data and the theoretical analysis. For the cases tested, the present model correctly predicts the unsteady near-wall flow and the unsteady shin friction at various frequencies.
Document ID
19930069211
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Fan, Sixin
(NASA Lewis Research Center Cleveland, OH, United States)
Lakshminarayana, Budugur
(Pennsylvania State Univ. University Park, United States)
Barnett, Mark
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
August 16, 2013
Publication Date
October 1, 1993
Publication Information
Publication: AIAA Journal
Volume: 31
Issue: 10
ISSN: 0001-1452
Subject Category
Aerodynamics
Accession Number
93A53208
Funding Number(s)
CONTRACT_GRANT: NAG3-1168
Distribution Limits
Public
Copyright
Other

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