Vibration control of the straight bladed vertical axis wind turbine structure using the leading-edge protuberanced blades

被引:6
作者
Vel, E. Karthik [1 ]
Pillai, S. Nadaraja [1 ]
机构
[1] SASTRA Deemed Univ, Turbulence & Flow Control Lab, Thanjavur 613401, Tamil Nadu, India
关键词
Vibration control; VAWT; Leading edge protuberance; Dynamic stall; Passive flow control; Experimental study; Aerodynamic damping; AERODYNAMIC CHARACTERISTICS; PERFORMANCE; TUBERCLES; MODEL;
D O I
10.1016/j.engstruct.2024.118806
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This study investigates the impact of structural responses resulting from alterations in aerodynamic characteristics caused by incorporating leading-edge protuberance (LEP) blades in vertical-axis wind turbines (VAWTs) under various wind speeds. The current experimental investigation was conducted on a scaled-down straightblade VAWT with multiple wind speeds at a fixed pitch angle and uniform blade configuration. The unsteady structural excitation caused by the decay of vortices due to the different aerodynamic loads and its effect on the VAWT structure is examined in great detail. The presence of counter-rotating vortices from the LEP profile, however, enhances the aerodynamics of the blades at higher angles of attack. It is crucial to understand the structural characteristics resulting from changes in aerodynamics. The paper presents the effects of the LEP on the structural excitation of the VAWT by analyzing the acceleration and displacement data obtained from the static structure of VAWT for various operational wind speeds. The results showed decreased acceleration and displacement amplitudes for the VAWT with LEP at medium and higher wind speeds. Significant aerodynamic and structural damping was observed in the VAWT with LEP blades. The results obtained were in close agreement with the time and frequency domains of the measured displacement and acceleration from the structure. The bidirectional vibration control was observed for the VAWT with LEP, which was found to have a reduction ratio of 70 %.
引用
收藏
页数:18
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