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流向强迫振荡圆柱绕流的涡脱落模态分析
引用本文:张宇飞,肖志祥,符松.流向强迫振荡圆柱绕流的涡脱落模态分析[J].力学学报,2007,39(3):408-416.
作者姓名:张宇飞  肖志祥  符松
作者单位:清华大学航天航空学院,100084 清华大学航天航空学院 清华大学航天航空学院, 100084
基金项目:国家自然科学基金,高等学校博士学科点专项科研项目
摘    要:通过求解采用ALE方法描述的运动坐标系Navier-Stokes方程组,分析均匀来流下雷诺 数为150的静止和流向振荡的圆柱绕流. 主要研究了强迫振荡频率和较大振幅比 (A/D=0.3-1.2)对圆柱升力、阻力变化特性以及涡脱落模态的影响. 研究表 明,流向振荡圆柱绕流存在多种涡脱落模态,如对称S以及反对称A-I, A-III, A-IV等多种形式;比较研究结果,拓展了各模态下对应的锁定区域,并将其分为5个 子区;A-I模态中圆柱受力较以前所知更复杂;通过分析计算结果,发现最大加速度 比Af_{c}^{2}/Df_{s0}^{2}可能是涡脱落模态(尤其是对称S模态)最有效的控制参数.

关 键 词:圆柱绕流  ALE方法  流向振荡  涡脱落模态  最大加速度比
文章编号:0459-1879(2007)03-0408-09
收稿时间:2005-10-17
修稿时间:2006-12-20

ANALYSIS OF VORTEX SHEDDING MODES OF AN IN-LINE OSCILLATING CIRCULAR CYLINDER IN A UNIFORM FLOW
Zhang Yufei,Xiao Zhixiang,Fu Song.ANALYSIS OF VORTEX SHEDDING MODES OF AN IN-LINE OSCILLATING CIRCULAR CYLINDER IN A UNIFORM FLOW[J].chinese journal of theoretical and applied mechanics,2007,39(3):408-416.
Authors:Zhang Yufei  Xiao Zhixiang  Fu Song
Institution:School of Aerospace, Tsinghua University, Beijing 100084, China
Abstract:Flows around stationary and in-line oscillating circular cylinder in uniform flow at Reynolds number of 150 is studied by solving Navier-Stokes equations on a moving grid system which described by Arbitrary Largangian-Eulerian (ALE) method. The main objective is to investigate the lift and drag features and vortex shedding modes through different reduced oscillating frequencies and a little strong amplitudes, where the ratio of amplitude and diameter A/D is from 0.3 to 1.2. Present numerical results show that there are several modes of vortex shedding such as symmetrical S and anti-symmetrical A-I, A-III and A-IV modes. Through analysis of previous and present results, the region of lock-on is extended, which is divided into five sub-regions. Especially, the force on the circular cylinder at anti-symmetrical A-I mode shows more complex characters than the original mode. Based on the experimental and numerical results, we suggest that the radio of maximum acceleration Af_{c}^{2}/Df_{s0}^{2} should be an important parameter for vortex shedding modes, especially for the symmetrical S mode.
Keywords:flow around circular cylinder  ALE method  in-line oscillating  vortex shedding  ratio of maximum acceleration
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