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Measurement of high solidity vertical axis wind turbine aerodynamic loads under high vibration response conditions

机译:高振动响应条件下高强度垂直轴风力涡轮机空气动力载荷的测量

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A series of full-scale experimental wind tunnel tests were performed to determine the aerodynamic loading behaviour on the airfoils of a high solidity, H-type, vertical axis wind turbine. During the course of this investigation, high amplitude vibration of the turbine was observed over a wide range of test conditions. The primary vibration excitation mechanism was resonance of the dominant whirling mode of the turbine with the operating blade pass frequency. In addition, for a significant number of test cases, resonance of the airfoil support struts at higher frequencies was also observed. This large vibration response resulted in conditions that made it difficult or impossible to measure the underlying aerodynamic loading. As a result, in order to gain a greater understanding of the aerodynamic loading, a vibration isolation methodology was developed to remove the effect of vibration from the measured aerodynamic forces on the blades. This included tests with two different support shaft end conditions over a range of flow velocities from 8 to 11 m/s, and the use of band-stop filtering to remove residual small amplitude vibrations. In this way, an accurate and complete measurement of the aerodynamic loading on the turbine blades could be obtained to better understand the effects of dynamic stall and validate the results of numerical model predictions.
机译:进行了一系列全面的试验性风洞试验,以确定高强度H型垂直轴风力涡轮机机翼的空气动力学载荷行为。在此研究过程中,在各种测试条件下都观察到了涡轮机的高振幅振动。主要的振动激励机制是涡轮机的主导回旋模式与工作叶片通过频率的共振。此外,对于大量测试案例,还观察到了机翼支撑支柱在较高频率下的共振。这种大的振动响应导致条件难以或不可能测量潜在的空气动力学负荷。结果,为了更好地了解空气动力学负荷,开发了一种隔振方法,以从叶片上测得的空气动力学力中消除振动的影响。这包括在8到11 m / s的流速范围内使用两种不同的支撑轴端部条件进行的测试,以及使用带阻滤波器消除残留的小振幅振动。以此方式,可以获得涡轮叶片上的空气动力学负载的准确且完整的测量结果,以更好地理解动态失速的影响并验证数值模型预测的结果。

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