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A convergence study of solutions using two two-equation RANS turbulence models on a finite volume solver for structured grids
Jatinder Pal Singh Sandhu,
Published in American Institute of Aeronautics and Astronautics Inc, AIAA
2018
Abstract
In this paper, we present a new, modular, explicit time marching based, three-dimensional finite volume solver for compressible flows on structured grids: FEST3D (Finite volume Explicit STructured 3 Dimensional solver). We provide details of the solver along with the verification performed to test the implementation of the code. Also, we present a study on the convergence of RANS solutions for two different, two equation turbulence models: k − ω/k − ɛ (Menter, F. R., “Two-equation eddy-viscosity turbulence models for engineering applications,” AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598–1605.) and k − kL (Abdol-Hamid, K. S., Carlson, J.-R., and Rumsey, C. L., “Verification and Validation of the k-kL Turbulence Model in FUN3D and CFL3D Codes,” 46th AIAA Fluid Dynamics Conference, 2016.). Our study shows that for subsonic flow, which do not have discontinuities, using a limiter for higher order state reconstruction only for turbulence variables improves the overall convergence of the solution. © 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
About the journal
JournalData powered by Typeset2018 Fluid Dynamics Conference
PublisherData powered by TypesetAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISSN0001-1452
Impact Factor1.868
Open AccessNo
Citation Styleunsrt
Sherpa RoMEO Archiving PolicyGreen
Concepts (11)
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    Aviation
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    Navier stokes equations
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    3-DIMENSIONAL
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    EDDY VISCOSITY TURBULENCE MODEL
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    Engineering applications
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    Rans turbulence models
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    STRUCTURED GRID
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    TIME MARCHING
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    Two-equation turbulence models
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    VERIFICATION-AND-VALIDATION
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    Turbulence models