首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于Transition SST模型的高雷诺数圆柱绕流数值研究
引用本文:雷娟棉,谭朝明.基于Transition SST模型的高雷诺数圆柱绕流数值研究[J].北京航空航天大学学报,2017,43(2):207-217.
作者姓名:雷娟棉  谭朝明
作者单位:北京理工大学宇航学院,北京,100081;北京理工大学宇航学院,北京,100081
基金项目:国家自然科学基金(11372040)National Natural Science Foundation of China
摘    要:为了研究高雷诺数下圆柱绕流边界层的转捩现象和圆柱尾迹近壁区的流动特征,首先通过在典型雷诺数下采用Transition SST四方程转捩模型模拟圆柱绕流得到的结果与实验结果及采用SST k-ω两方程湍流模型模拟结果的对比分析,验证了Transition SST模型在模拟高雷诺数下圆柱绕流的优越性,并较为准确地预测出了圆柱绕流边界层的转捩现象及尾迹近壁区的流动特征。然后分别对亚临界区、临界区、超临界区和过临界区的圆柱绕流问题进行了数值模拟,分析了不同雷诺数下圆柱绕流的流场结构及圆柱表面压力系数、摩擦力系数的变化规律,研究了圆柱绕流近壁区的流动特征、边界层转捩的流动机理、转捩位置及其随雷诺数的变化规律。结果表明,亚临界区二维圆柱绕流边界层发生层流分离,无分离泡和转捩现象;临界区和超临界区二维圆柱绕流边界层先产生了分离泡现象,之后流动发生了转捩并在转捩后发生湍流分离;过临界区二维圆柱绕流边界层流动在转捩之后发生湍流分离,无分离泡现象;在临界区、超临界区和过临界区,二维圆柱绕流边界层转捩位置随雷诺数增大向前驻点移动。

关 键 词:圆柱绕流  Transition  SST模型  流动特征  转捩现象  气动特性
收稿时间:2016-01-26

Numerical simulation for flow around circular cylinder at high Reynolds number based on Transition SST model
LEI Juanmian,TAN Zhaoming.Numerical simulation for flow around circular cylinder at high Reynolds number based on Transition SST model[J].Journal of Beijing University of Aeronautics and Astronautics,2017,43(2):207-217.
Authors:LEI Juanmian  TAN Zhaoming
Abstract:In order to study the boundary layer transition phenomenon and the flow characteristics of flow around circular cylinder at high Reynolds number, the experimental results and the results that are obtained by using the Transition SST model and the SST k-ω model were firstly analyzed at typical Reynolds number, and the advantages of the Transition SST model was verified at high Reynolds number. Meanwhile, the boundary layer transition phenomenon and the flow characteristics were more accurately predicted. Then, the numerical simulations were performed in subcritical, critical, supercritical and over critical regions. The variation of flow field structure and the friction coefficient curve was analyzed under the different Reynolds number. The flow characteristics, flow mechanism of boundary layer transition, and variation of transition positions were studied. Results show that the boundary layer separates laminarly, and the flow does not form a separation bubble and transition phenomenon in subcritical region; in critical and supercritical region, the flow forms a separation bubble, and ultimately turbulent separation happens after transition occurs with the flow; in over critical region, the boundary layer separates turbulently after transition occurs with the flow, and the flow does not form a separation bubble; the more the Reynolds number is, the closer the transition position is to the front stagnation point of cylinder in critical, supercritical and over critical region.
Keywords:flow around circular cylinder  Transition SST model  flow characteristics  transition phenomenon  aerodynamic characteristics
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号