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Comparison of DES turbulence models with the flow around circular cylinder at ReD=3900

  • Beihang University
  • China Aircraft Strength Research Institute

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

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.

源语言英语
主期刊名23rd AIAA Computational Fluid Dynamics Conference, 2017
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624105067
DOI
出版状态已出版 - 2017
活动23rd AIAA Computational Fluid Dynamics Conference, 2017 - Denver, 美国
期限: 5 6月 20179 6月 2017

出版系列

姓名23rd AIAA Computational Fluid Dynamics Conference, 2017

会议

会议23rd AIAA Computational Fluid Dynamics Conference, 2017
国家/地区美国
Denver
时期5/06/179/06/17

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