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Calculation of Turbulent Subsonic Diffuser Flows Using the NPARC Navier-Stokes CodeAxisymmetric subsonic diffuser flows were calculated with the NPARC Navier-Stokes code in order to determine the effects various code features have on the flow solutions. The code features examined in this work were turbulence models and boundary conditions. Four turbulence models available in NPARC were used: the Baldwin-Lomax algebraic model, the Baldwin-Barth one-equation model, and the Chien kappa-epsilon and Wilcox kappa-omega two-equation models. The three boundary conditions examined were the free boundary, the mass flux boundary and the subsonic outflow with variable static pressure. In addition to boundary condition type, the geometry downstream of the diffuser was varied to see if upstream influences were present. The NPARC results are compared with experimental data and recommendations are given for using NPARC to compute similar flows.
Document ID
19960016641
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dudek, J. C.
(NASA Lewis Research Center Cleveland, OH United States)
Georgiadis, N. J.
(NASA Lewis Research Center Cleveland, OH United States)
Yoder, D. A.
(Cincinnati Univ. OH United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1996
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 96-0497
NASA-TM-107177
NAS 1.15:107177
E-10139
Report Number: AIAA Paper 96-0497
Report Number: NASA-TM-107177
Report Number: NAS 1.15:107177
Report Number: E-10139
Meeting Information
Meeting: 34th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 15, 1996
End Date: January 18, 1996
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
96N22270
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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