计算物理 ›› 2019, Vol. 36 ›› Issue (1): 53-59.DOI: 10.19596/j.cnki.1001-246x.7815

• • 上一篇    下一篇

基于有限差分法刚性圆柱体涡激振动响应特性数值研究

高云1,2, 邹丽3,4, 宗智3   

  1. 1. 西南石油大学 油气藏地质及开发工程国家重点实验室, 四川 成都 610500;
    2. 东京大学 机械工程学院, 东京 日本 113-8656;
    3. 大连理工大学 工业装备结构分析国家重点实验室, 辽宁 大连 116024;
    4. 高技术船舶与深海开发装备协同创新中心, 上海 200240
  • 收稿日期:2017-12-18 修回日期:2018-01-20 出版日期:2019-01-25 发布日期:2019-01-25
  • 作者简介:高云,男,副教授,硕士生导师,主要研究方向为海洋工程水动力学,E-mail:dutgaoyun@163.com
  • 基金资助:
    国家自然科学基金(51609206,51522902,51579040),国家留学基金(201608515007),青岛海洋科学与技术国家实验室开放基金(QNLM2016OPR0402)及中央高校基本科研业务费专项资金项目(DUT17ZD233)资助

Numerical Study of Response Performance of Vortex-Induced Vibration on a Rigid Cylinder Based on Finite Difference Method

GAO Yun1,2, ZOU Li3,4, ZONG Zhi3   

  1. 1. State Key Laboratory of Oil and Gas Reservoir Geology and Exploration, Southwest Petroleum University, Chengdu 610500, China;
    2. School of Mechanical Engineering, The University of Tokyo, Tokyo 113-8656, Japan;
    3. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, China;
    4. Collaborative Innovation Center for Advanced Ship and Deep-Sea Exploration, Shanghai, 200240, China
  • Received:2017-12-18 Revised:2018-01-20 Online:2019-01-25 Published:2019-01-25

摘要: 基于尾流振子模型对刚性圆柱体涡激振动响应特性进行数值研究.建立圆柱体结构振子及尾流振子之间的耦合方程,基于二阶精度中心差分格式对耦合模型先离散后迭代进行求解.对不同质量比及不同阻尼比圆柱体涡激振动响应的无量纲位移、无量纲升力、频率比及锁定区间等参数进行分析.结果表明数值方法可以很好地模拟刚性圆柱体的涡激振动响应特性.随着质量比的增加,锁定开始点逐渐延后,锁定结束点逐渐提前,锁定区间宽度逐渐变窄.

关键词: 涡激振动, 尾流振子模型, 锁定区间, 有限差分法

Abstract: Numerical study based on a wake oscillator model is conducted to determine response performance of vortex-induced vibration (VIV) on a rigid cylinder. A coupled model of structural oscillator of a rigid cylinder and wake oscillator is established, and then the model is discretized and solved based on a standard central finite difference method of the second order. VIV response characteristics including dimensionless displacement, dimensionless lift, and frequency ratio and lock-in region varied with mass ratios and damping ratios are compared. It can be found that the numerical method simulates response performances of vortex-induced vibration on a rigid cylinder very well. As dimensionless mass ratio increases, onset of lock-in region occurs later, lock-out point occurs earlier, and so the lock-in region becomes smaller.

Key words: vortex-induced vibration, wake oscillator model, lock-in region, finite difference method

中图分类号: