Evaluation of turbulence models in the PARC code for transonic diffuser flows

Author:

Georgiadis N.1,Drummond J.2,Leonard B.2

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. Akron Univ., OH

Publisher

American Institute of Aeronautics and Astronautics

Reference31 articles.

1. Pulliam,T.H. "EulerandThinLayerNavier-Stokes Codes: ARC2D,ARC3D."NotesforComuutational FluidDvnamicsUser'sWorkshop,TheUniversity of TennesseeSpaceInstitute,Tullahoma,Tennessee, (UTSIPublicationE02-4005-023-84),1984,pp.15.1-15.85.

2. Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow

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1. Evaluación de Modelos de Turbulencia para el Flujo de Aire en un Difusor Transónico;Revista Politécnica;2020-04-16

2. A Compressible Pressure-based Solution Algorithm for Gas Turbine Combustion Chambers Using the PDF/FGM Model;Flow, Turbulence and Combustion;2013-03-08

3. Wind-US Unstructured Flow Solutions for a Transonic Diffuser;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

4. HPC CHSSI CFD-7 - Scalable WIND from the NPARC Alliance;30th Plasmadynamic and Lasers Conference;1999-06-28

5. The NPARC Alliance - A progress report;33rd Joint Propulsion Conference and Exhibit;1997-07-06

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