TY - GEN
T1 - Computation of turbulent flow in a lid-driven 2D cavity and a 3D box using a number of turbulence models
AU - Nagapetyan, Hakop J.
AU - Wray, Timothy J.
AU - Agarwal, Ramesh K.
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - In this paper, various turbulence models are used for simulating internal turbulent flow with large recirculation by considering the flow in a 2-D lid-driven square cavity and a 3-D lid driven cubic box. The accuracy of the newly developed Wray-Agarwal (WA) one equation turbulence model is compared against the two well-known industry standard turbulence models - the Spalart-Allmaras (SA) model and the Shear-Stress-Transport (SST) k-ω model. The simulations are performed by numerically solving the Reynolds-Averaged Navier-Stokes (RANS) equations in conjunction with WA, SA and SST k-ω models and comparing the results with the available experimental data and Large Eddy Simulation (LES) results. 2-D numerical solutions are obtained at Reynolds numbers of 10,000, 20,000, 50,000, and 100,000. 3-D numerical solutions are obtained at Reynolds numbers of 3200 and 10,000. All numerical calculation are compared with other numerical results available in the literature. The open-source CFD code OpenFOAM is used to compute the flow field. Computational results clearly demonstrate that the Wray-Agarwal model outperforms in accuracy both the Spalart-Allmaras and Shear-Stress-Transport k-ω models at all Reynolds numbers considered.
AB - In this paper, various turbulence models are used for simulating internal turbulent flow with large recirculation by considering the flow in a 2-D lid-driven square cavity and a 3-D lid driven cubic box. The accuracy of the newly developed Wray-Agarwal (WA) one equation turbulence model is compared against the two well-known industry standard turbulence models - the Spalart-Allmaras (SA) model and the Shear-Stress-Transport (SST) k-ω model. The simulations are performed by numerically solving the Reynolds-Averaged Navier-Stokes (RANS) equations in conjunction with WA, SA and SST k-ω models and comparing the results with the available experimental data and Large Eddy Simulation (LES) results. 2-D numerical solutions are obtained at Reynolds numbers of 10,000, 20,000, 50,000, and 100,000. 3-D numerical solutions are obtained at Reynolds numbers of 3200 and 10,000. All numerical calculation are compared with other numerical results available in the literature. The open-source CFD code OpenFOAM is used to compute the flow field. Computational results clearly demonstrate that the Wray-Agarwal model outperforms in accuracy both the Spalart-Allmaras and Shear-Stress-Transport k-ω models at all Reynolds numbers considered.
UR - https://www.scopus.com/pages/publications/85007559153
U2 - 10.2514/6.2016-1114
DO - 10.2514/6.2016-1114
M3 - Conference contribution
AN - SCOPUS:85007559153
SN - 9781624103933
T3 - 54th AIAA Aerospace Sciences Meeting
BT - 54th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 54th AIAA Aerospace Sciences Meeting, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -