宇航总体技术2024,Vol.8Issue(1) :68-75.

高雷诺数下交叉圆柱涡激振动的数值分析

Numerical Analysis of Vortex-Induced Vibration of a Crossed Circular Cylinder at High Reynolds Numbers

金叶青 张俊涛 秦岩 崔景芝 孙海亮
宇航总体技术2024,Vol.8Issue(1) :68-75.

高雷诺数下交叉圆柱涡激振动的数值分析

Numerical Analysis of Vortex-Induced Vibration of a Crossed Circular Cylinder at High Reynolds Numbers

金叶青 1张俊涛 2秦岩 1崔景芝 3孙海亮3
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作者信息

  • 1. 哈尔滨工程大学烟台哈尔滨工程大学研究院,烟台 265503
  • 2. 哈尔滨工程大学烟台哈尔滨工程大学研究院,烟台 265503;哈尔滨工程大学船舶工程学院,哈尔滨 150001
  • 3. 北京宇航系统工程研究所,北京 100076
  • 折叠

摘要

基于能量捕获应用场景,利用数值仿真的方法研究了高雷诺数下交叉圆柱的涡激振动(Vortex Induced Vibration,ⅥⅤ)现象.首先建立了三维ⅥⅤ数值模型,通过与已有文献试验数据对比验证了该数值模型的准确性.进而在该模型的基础上,对交叉圆柱的ⅥⅤ进行了仿真研究,并与普通圆柱做了对比分析.研究发现,受竖圆柱的影响,交叉圆柱在中低流速的涡强度有所减小,使低流速下的柱体振幅减小,启动流速变大;在中流速范围,涡脱落位置的改变,使得振幅增加;在高流速范围涡强度和涡脱落位置变化并不明显,振幅也与普通圆柱相近.

Abstract

Based on the energy capture application scenario,this paper studies the ⅥⅤphenomenon of crossed cylinders at high Reynolds numbers by numerical simulation.A three-di-mensional ⅥⅤ numerical model was established,and the accuracy of the numerical model was verified by comparing with the experimental data in the existing paper.On the basis of the model,the ⅥⅤ of the crossed cylinder is simulated and compared with that of the ordinary cylinder.It is found that due to the influence of the vertical cylinder,the vortex intensity of the crossed cylinder at low and medium flow rates decreases,which reduces the amplitude of the cylinder at low flow rates and increases the starting flow rate.In the middle flow rate range,the amplitude increases due to the change of the vortex shedding position.In the high velocity range,the vortex intensity and vortex shedding position do not change significantly,and the amplitude is also similar to that of the ordinary cylinder.

关键词

涡激振动/交叉圆柱/高雷诺数/数值仿真

Key words

Vortex induced vibrations/Crossed cylinder/High-Reynolds numbers/Numerical simulation

引用本文复制引用

基金项目

山东省重点研发计划重大创新工程项目(2022CXGC020509)

火箭创新基金(ZH2022009)

中央高校基本科研业务费(3072022QBZ2701)

中央高校基本科研业务费(3072022QBZ2702)

中央高校基本科研业务费(3072022JC2701)

烟台新旧动能转换研究院暨烟台科技成果转移转化示范基地项目(YTDNY20220425-01)

出版年

2024
宇航总体技术

宇航总体技术

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参考文献量14
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