李羽, 柳灿, 连波, 竺晓程. 基于强迫振动和自由振动的风力机翼型涡激振动数值研究[J]. 动力工程学报, 2024, 44(2): 270-276. DOI: 10.19805/j.cnki.jcspe.2024.230074
引用本文: 李羽, 柳灿, 连波, 竺晓程. 基于强迫振动和自由振动的风力机翼型涡激振动数值研究[J]. 动力工程学报, 2024, 44(2): 270-276. DOI: 10.19805/j.cnki.jcspe.2024.230074
LI Yu, LIU Can, LIAN Bo, ZHU Xiaocheng. Numerical Study on Vortex-induced Vibration of Wind Turbine Airfoil via Prescribed Vibration and Free Vibration[J]. Journal of Chinese Society of Power Engineering, 2024, 44(2): 270-276. DOI: 10.19805/j.cnki.jcspe.2024.230074
Citation: LI Yu, LIU Can, LIAN Bo, ZHU Xiaocheng. Numerical Study on Vortex-induced Vibration of Wind Turbine Airfoil via Prescribed Vibration and Free Vibration[J]. Journal of Chinese Society of Power Engineering, 2024, 44(2): 270-276. DOI: 10.19805/j.cnki.jcspe.2024.230074

基于强迫振动和自由振动的风力机翼型涡激振动数值研究

Numerical Study on Vortex-induced Vibration of Wind Turbine Airfoil via Prescribed Vibration and Free Vibration

  • 摘要: 基于动网格技术,分别采用强迫振动和自由振动方法对90°攻角下风力机翼型的涡激振动现象进行了数值研究。通过强迫振动计算方法,确定了Du96-W-180风力机翼型在不同振幅下的涡振区间,并比较了改变来流速度和改变结构刚度对涡振区间的影响;通过自由振动计算方法,获得了不同来流速度下的翼型涡振区间,对比了频率比r=0.93和r=1.11时不同结构阻尼对翼型振动响应的影响,分析了翼型涡振的发展和演化过程。结果表明:改变来流速度和改变结构刚度时不同频率比下的涡振区间基本一致;自由振动数值计算验证了强迫振动的涡振区间;不同频率比下6%结构阻尼比时翼型振动出现涡激振动和强迫振动2种形式。

     

    Abstract: Based on the dynamic mesh technique, the vortex-induced vibration of wind turbine airfoil at 90° angle of attack was numerically studied by using the prescribed vibration method and the free vibration method respectively. Through the prescribed vibration calculation method, the vortex-induced vibration range of Du96-W-180 wind turbine airfoil at different amplitudes was determined, and the effects of changing the incoming flow velocity and changing the structural stiffness on the vortex-induced vibration range were compared. Through the free vibration calculation method, the vortex-induced vibration range of the airfoil at different inflow speeds was obtained. The influence of different structural damping on the vibration response of the airfoil at the frequency ratio r=0.93 and r=1.11 was compared, and the development and evolution process of the vortex-induced vibration of the airfoil were analyzed. Results show that vortex-induced vibration range at different frequency ratios is basically the same while changing incoming flow velocity and changing the structural stiffness. The free vibration numerical simulation verifies the vortex-vibration range of the forced vibration. When 6% structural damping is applied at different frequency ratios, the vibration of the airfoil exhibits two forms: vortex-induced vibration and forced vibration.

     

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