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Implementation and Validation of the Chien k-epsilon Turbulence Model in the Wind Navier-Stokes CodeThe two equation k-epsilon turbulence model of Chien has been implemented in the WIND Navier-Stokes flow solver. Details of the numerical solution algorithm, initialization procedure, and stability enhancements are described. Results obtained with this version of the model are compared with those from the Chien k-epsilon model in the NPARC Navier-Stokes code and from the WIND SST model for three validation cases: the incompressible flow over a smooth flat plate, the incompressible flow over a backward facing step, and the shock-induced flow separation inside a transonic diffuser. The k-epsilon model results indicate that the WIND model functions very similarly to that in NPARC, though the WIND code appears to he slightly more accurate in the treatment of the near-wall region. Comparisons of the k-epsilon model results with those from the SST model were less definitive, as each model exhibited strengths and weaknesses for each particular case.
Document ID
19990047464
Acquisition Source
Glenn Research Center
Document Type
Reprint (Version printed in journal)
Authors
Yoder, Dennis A.
(NASA Glenn Research Center Cleveland, OH United States)
Georgiadis, Nicholas J.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1999
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA/TM-1999-209080
E-11662
AIAA Paper 99-0745
NAS 1.15:209080
Report Number: NASA/TM-1999-209080
Report Number: E-11662
Report Number: AIAA Paper 99-0745
Report Number: NAS 1.15:209080
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 11, 1999
End Date: January 14, 1999
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 537-05-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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