TY - GEN
T1 - Comparison of DES turbulence models with the flow around circular cylinder at ReD=3900
AU - Tang, Hu
AU - Chang, Shinan
AU - Cheng, Zhu
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - Based on the requirements of simulating the flow around spray bar installed in ground based icing test facilities, the accuracy of three Detached Eddy Simulation (DES) turbulence models, including Spalart-Allmaras DES, Realizable k-ε DES, and Shear Stress Transport k-ω DES, were examined through the comparison and analysis of instantaneous flow characteristics and flow statistic parameters obtained from a three-dimensional subcritical flow around circular cylinder at ReD=3900. It is found that: (a) from the point of instantaneous flow characterization, the k-ω RANS (Reynolds Averaged Navier-Stokes) branch also has remarkable influence on the accuracy of SST k-ω DES except k-ε RANS branch, (b) from the point of error range of flow statistic parameters, the size of recirculation region Lrec and mimimum streamwise velocity umin are the key parameters which can reflect the accuracy of numerical simulation on flow around circular cylinder to some extend, (c) compared comprehensively, the predicted values from SST k-ω DES among three DES models give a relatively closer agreement with experimental data, which indicate that it has the potential of applying to the calculation of wake turbulence generated from spray bar system installed in ground based icing test facilities.
AB - Based on the requirements of simulating the flow around spray bar installed in ground based icing test facilities, the accuracy of three Detached Eddy Simulation (DES) turbulence models, including Spalart-Allmaras DES, Realizable k-ε DES, and Shear Stress Transport k-ω DES, were examined through the comparison and analysis of instantaneous flow characteristics and flow statistic parameters obtained from a three-dimensional subcritical flow around circular cylinder at ReD=3900. It is found that: (a) from the point of instantaneous flow characterization, the k-ω RANS (Reynolds Averaged Navier-Stokes) branch also has remarkable influence on the accuracy of SST k-ω DES except k-ε RANS branch, (b) from the point of error range of flow statistic parameters, the size of recirculation region Lrec and mimimum streamwise velocity umin are the key parameters which can reflect the accuracy of numerical simulation on flow around circular cylinder to some extend, (c) compared comprehensively, the predicted values from SST k-ω DES among three DES models give a relatively closer agreement with experimental data, which indicate that it has the potential of applying to the calculation of wake turbulence generated from spray bar system installed in ground based icing test facilities.
UR - https://www.scopus.com/pages/publications/85088061899
U2 - 10.2514/6.2017-4285
DO - 10.2514/6.2017-4285
M3 - 会议稿件
AN - SCOPUS:85088061899
SN - 9781624105067
T3 - 23rd AIAA Computational Fluid Dynamics Conference, 2017
BT - 23rd AIAA Computational Fluid Dynamics Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 23rd AIAA Computational Fluid Dynamics Conference, 2017
Y2 - 5 June 2017 through 9 June 2017
ER -