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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
20220001759
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
David J Friedlander
(Glenn Research Center Cleveland, Ohio, United States)
Julianne C Dudek
(Glenn Research Center Cleveland, Ohio, United States)
May-fun Liou
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
January 31, 2022
Publication Date
February 25, 2022
Subject Category
Aerodynamics
Report/Patent Number
E-20017
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
Diffuser Flows
Computational Fluid Dynamics
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