TY - GEN
T1 - One-Equation, Two-Equation and Full Reynolds Stress Turbulence Modeling of the BeVERLI Hill Configuration
AU - Wadhai, Vishal
AU - Nair, Shyam
AU - Yang, Xiang
AU - Kunz, Robert
N1 - Publisher Copyright:
© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2024
Y1 - 2024
N2 - The BeVERLI Hill configuration has been studied using steady RANS at several tunnel orientations and Reynolds numbers. We report results using a sequence of (supplied) meshes, and five different RANS turbulence models: the standard Spalart-Allmaras one-equation model, a data-augmented Spalart-Allmaras model, the Menter κ - ω SST two-equation model, the Chien κ - ε two-equation model, the seven-equation SSG-LRR Full Reynolds Stress Model (FRSM). Results for the 30° orientation BeVERLI Hill bump are presented at two Reynolds numbers ReH =250000 and 650000 per the “blind" model comparison call for this series of papers, using the data templates provided by Virginia Tech. There is in general good agreements among the two SA models, the SST κ - ω model and the FRSM, with Chien κ - ε model yielding somewhat different results.
AB - The BeVERLI Hill configuration has been studied using steady RANS at several tunnel orientations and Reynolds numbers. We report results using a sequence of (supplied) meshes, and five different RANS turbulence models: the standard Spalart-Allmaras one-equation model, a data-augmented Spalart-Allmaras model, the Menter κ - ω SST two-equation model, the Chien κ - ε two-equation model, the seven-equation SSG-LRR Full Reynolds Stress Model (FRSM). Results for the 30° orientation BeVERLI Hill bump are presented at two Reynolds numbers ReH =250000 and 650000 per the “blind" model comparison call for this series of papers, using the data templates provided by Virginia Tech. There is in general good agreements among the two SA models, the SST κ - ω model and the FRSM, with Chien κ - ε model yielding somewhat different results.
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U2 - 10.2514/6.2024-4437
DO - 10.2514/6.2024-4437
M3 - Conference contribution
AN - SCOPUS:85204202766
SN - 9781624107160
T3 - AIAA Aviation Forum and ASCEND, 2024
BT - AIAA Aviation Forum and ASCEND, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation Forum and ASCEND, 2024
Y2 - 29 July 2024 through 2 August 2024
ER -