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Atmospheric Testing of Wind Turbine Trailing Edge Aerodynamic Brakes

机译:风力涡轮机后缘空气动力学制动器的大气测试

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An experimental investigation was conducted using an instrumented horizontal-axis wind turbine that incorporated variable span trailing-edge aerodynamic brakes. A primary goal was to directly compare study results with (infinite-span) wind tunnel data and to provide information on how to account for device span effects during turbine design or analysis. Comprehensive measurements were utilized to define effective hcanges in the aerodynamic coefficients, as a function of angle of attack and control deflection, for three device spans and configurations. Differentces in the lift and drag behavior are most pronounced near stall and for device spans of less thant 15
机译:使用装有可变跨度后缘空气动力学制动器的仪器化水平轴风力涡轮机进行了实验研究。主要目标是将研究结果与(无限跨度)风洞数据直接进行比较,并提供有关如何在涡轮机设计或分析过程中考虑设备跨度影响的信息。综合测量用于定义三种装置跨度和配置的空气动力学系数的有效变化,该变化是迎角和控制偏斜的函数。在失速附近以及小于15的设备跨度中,举升和拖动行为的差异最为明显

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