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首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >A comparison of wake measurements in motor-driven and flow-driven turbine experiments
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A comparison of wake measurements in motor-driven and flow-driven turbine experiments

机译:电机驱动和流量驱动涡轮实验中的尾流测量结果比较

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We present experimental data to compare and contrast the wake characteristics of a turbine whose rotation is either driven by the oncoming flow or prescribed by a motor. Velocity measurements are collected using two-dimensional particle image velocimetry in the near-wake region of a lift-based, vertical-axis turbine. The wake of this turbine is characterized by a spanwise asymmetric velocity profile which is found to be strongly dependent on the turbine tip speed ratio (TSR), while only weakly dependent on Reynolds number (Re). For a given Re, the TSR is controlled either passively by a mechanical brake or actively by a DC motor. We find that there exists a finite region in TSR versus Re space where the wakes of the motor-driven turbine and flow-driven turbine are indistinguishable to within experimental precision. Outside of this region, the sign of the net circulation in the wake changes as TSR is increased by the motor. Shaft torque measurements show a corresponding sign change above this TSR threshold set by circulation, indicating a transition from net torque due to lift to net torque due to drag produced by the turbine blades, the latter of which can give wake measurements that are inconsistent with a flow-driven turbine. The results support the claim that the turbine kinematics and aerodynamic properties are the sole factors that govern the dynamics of its wake, irrespective of the means to move the turbine blades. This has significance for both experimental and computational studies where it may be necessary, or perhaps more economical, to prescribe the turbine kinematics in order to analyze its aerodynamic characteristics.
机译:我们提供了实验数据,以比较和对比涡轮的尾流特性,该涡轮的旋转要么由来流驱动,要么由电动机规定。使用二维粒子图像测速仪在基于升力的垂直轴涡轮机的近尾流区域中收集速度测量值。该涡轮机的尾流特征在于翼展方向的非对称速度曲线,发现该曲线强烈依赖于涡轮叶尖速比(TSR),而仅弱依赖于雷诺数(Re)。对于给定的Re,TSR要么通过机械制动被动控制,要么通过DC电动机主动控制。我们发现在TSR与Re空间中存在一个有限区域,在该区域内,电动机驱动的涡轮机和流动驱动的涡轮机的尾流在实验精度内是无法区分的。在该区域之外,尾流中净循环的符号会随着电机增加TSR而改变。轴扭矩测量结果显示,相应的符号变化高于循环设定的TSR阈值,表明从升力产生的净扭矩过渡到涡轮叶片产生的阻力引起的净扭矩,后者的尾流测量值与涡轮叶片不一致。流动驱动涡轮。结果证明了涡轮的运动学和空气动力学特性是控制其尾流动力学的唯一因素,而与移动涡轮叶片的方式无关。这对于实验和计算研究都具有重要意义,因为在这些研究中可能有必要或更经济地规定涡轮运动学以分析其空气动力学特性。

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