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Prediction of Turbulent Diffusing Flows Using FUN3DThe FUN3D code was used to perform Reynolds-averaged Navier-Stokes (RANS) simulations to compute subsonic flow in an S-duct diffuser and transonic flow in a two-dimensional diffuser using the Speziale-Sarkar-Gatski/Launder-Rodi-Reece (SSG/LRR) Reynolds stress model (RSM). For comparison purposes, additional simulations were run with the one-equation Spalart-Allmaras (SA) and the two-equation Menter Shear-Stress Transport (SST) turbulence models. Each model was run with and without the quadratic constitutive relation (QCR) for computing the turbulent stresses. It was shown that the simulations that utilized the RSM had better overall predictions of the diffusive flow fields compared to the simulations that utilized the one and two equation turbulence models.
Document ID
20210024218
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
David Friedlander
(Glenn Research Center Cleveland, Ohio, United States)
Julianne Dudek
(Glenn Research Center Cleveland, Ohio, United States)
May-Fun Liou
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
November 10, 2021
Subject Category
Aerodynamics
Meeting Information
Meeting: AIAA SciTech Forum
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.03.09.01.04
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Inlet Distortion
CFD
Computational Fluid Dynamics
Diffuser Flows
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