合成射流对串列双圆柱涡致振动的控制效果OA
Control effects of synthetic jets on the Vortex Induced Vibration of two tandem circular cylinders
采用数值模拟的方法研究了合成射流对串列双圆柱涡致振动的影响.分析了折减速度和控制合成射流的动量系数对下游圆柱漩涡脱落过程、位移幅值、升阻力的影响.研究中,来流雷诺数Re=150,合成射流的位置角度α=45°,间距比为4.数值结果表明,水平合成射流能有效抑制下游圆柱的横流向振动,最高可使振幅降低80.48%.在水平合成射流控制下,下游圆柱脱落的两排尾涡间宽度明显减小.动量系数Cu由2增大到4后,抑制效果更为明显.
The effect of synthetic jets on the Vortex Induced Vibration(VIV)of two tandem circular cylinders was studied by numerical simulation.The effects of reduced velocity and the momentum co-efficient of the resultant jet on the shedding process,displacement amplitude and lift resistance of the downstream cylinder vortex were analyzed.In the study,the incoming Reynolds number Re=150,the position angle α=45°,and the spacing ratio is 4.The numerical results show that the horizontal synthetic jet can effectively suppress the vibration of the downstream cylinder and reduce the oscilla-tion amplitudes up to 80.48%.Under the control of the horizontal synthetic jet,the width between the two rows of trailing vortices shed by the downstream cylinder is obviously reduced.When the mo-mentum coefficient Cu increases from 2 to 4,the inhibition effect becomes more obvious.
张品源;王海博;胡小龙;于海龙
常州大学 石油与天然气工程学院,江苏 常州 213164常州大学 石油与天然气工程学院,江苏 常州 213164常州大学 石油与天然气工程学院,江苏 常州 213164常州大学 石油与天然气工程学院,江苏 常州 213164
航空航天
涡致振动合成射流串列双圆柱尾涡结构
Vortex Induced Vibrationsynthetic jetstwo tandem circular cylinderswake structure
《常州大学学报(自然科学版)》 2026 (2)
83-92,10
常州大学科研启动基金资助项目(ZMF21020384).
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