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An investigation into the numerical prediction of boundary layer transition using the K.Y. Chien turbulence modelAssessments were made of the simulation capabilities of transition models developed at the University of Minnesota, as applied to the Launder-Sharma and Lam-Bremhorst two-equation turbulence models, and at The University of Texas at Austin, as applied to the K. Y. Chien two-equation turbulence model. A major shortcoming in the use of the basic K. Y. Chien turbulence model for low-Reynolds number flows was identified. The problem with the Chien model involved premature start of natural transition and a damped response as the simulation moved to fully turbulent flow at the end of transition. This is in contrast to the other two-equation turbulence models at comparable freestream turbulence conditions. The damping of the transition response of the Chien turbulence model leads to an inaccurate estimate of the start and end of transition for freestream turbulence levels greater than 1.0 percent and to difficulty in calculating proper model constants for the transition model.
Document ID
19900016953
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stephens, Craig A.
(Texas Univ. Austin, TX, United States)
Crawford, Michael E.
(Texas Univ. Austin, TX, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-185252
NAS 1.26:185252
REPT-89-3
Report Number: NASA-CR-185252
Report Number: NAS 1.26:185252
Report Number: REPT-89-3
Accession Number
90N26269
Funding Number(s)
CONTRACT_GRANT: NAG3-864
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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