TY - GEN
T1 - Turbulence model conditioning for vortex dominated flows based on experimental results
AU - Moioli, Matteo
AU - Breitsamter, Christian
AU - Sørensen, Kaare A.
N1 - Publisher Copyright:
© 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. All rights reserved.
PY - 2018
Y1 - 2018
N2 - Focusing on vortex dominated flows, related to delta wings, Reynolds Averaged Navier-Stokes numerical simulation with eddy viscosity models is an appropriate tool with respect to the computational effort. Nevertheless, higher accuracy is required to improve the prediction of the vortex flow development and characteristics. More complex turbulence models like Reynolds Stress Models introduce stability issues and increase the computational costs, not always improving the flow solution; Detached Eddy Simulation and Large Eddy Simulation models are not always a viable option due to computational resources. The idea introduced is to enhance the Spalart-Allmaras one-equation eddy viscosity model with additional destruction terms, exclusively active in the vortex region, optimized with experimental data as reference. The vortex topology is adjusted by correcting the distribution of eddy viscosity. The level of improvement in data accuracy, the range of improvements for the considered test cases and the flexibility of the model variation are investigated to understand the potential of the approach.
AB - Focusing on vortex dominated flows, related to delta wings, Reynolds Averaged Navier-Stokes numerical simulation with eddy viscosity models is an appropriate tool with respect to the computational effort. Nevertheless, higher accuracy is required to improve the prediction of the vortex flow development and characteristics. More complex turbulence models like Reynolds Stress Models introduce stability issues and increase the computational costs, not always improving the flow solution; Detached Eddy Simulation and Large Eddy Simulation models are not always a viable option due to computational resources. The idea introduced is to enhance the Spalart-Allmaras one-equation eddy viscosity model with additional destruction terms, exclusively active in the vortex region, optimized with experimental data as reference. The vortex topology is adjusted by correcting the distribution of eddy viscosity. The level of improvement in data accuracy, the range of improvements for the considered test cases and the flexibility of the model variation are investigated to understand the potential of the approach.
KW - Computational Fluid Dynamics
KW - Delta wing
KW - Turbulence modeling
KW - Vortex flow
UR - http://www.scopus.com/inward/record.url?scp=85060484955&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85060484955
T3 - 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
BT - 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
PB - International Council of the Aeronautical Sciences
T2 - 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
Y2 - 9 September 2018 through 14 September 2018
ER -