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Experimental Investigations on the Effect of Overlap Ratio and Blade Edge Conditions on the Performance of Conventional Savonius Rotor

机译:重叠比和叶片边缘条件对常规Savonius转子性能影响的实验研究

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The torque of a conventional Savonius rotor is studied experimentally for overlap ratio from 0.10 to 0.70, blade edge condition (flat and round) and the change in Reynolds number. The results indicate that the coefficient of static torque improves marginally for round edged rotors for rotor angles up to 45°. The coefficient of static torque decreases as the overlap ratio is increased to 0.70 from 0.50 and is independent of the Reynolds numbers studied in the range between 120000 to 200000. Wind tunnel blockage ratio is studied. The power coefficient increases with the increase in the Reynolds number, whereas the coefficient of static torque is independent of the Reynolds number in the range studied. The coefficient of power, torque coefficient and coefficient static torque are independent of blockage ratios at a given Reynolds number.
机译:实验研究了传统Savonius转子的转矩,其重叠比为0.10至0.70,叶片边缘条件(平坦和圆形)以及雷诺数的变化。结果表明,对于最大角度为45°的圆边转子,静转矩系数略有提高。静转矩系数随着重叠比从0.50增加到0.70而减小,并且与研究的雷诺数在120000到200000之间的范围无关。研究风洞阻塞率。功率系数随雷诺数的增加而增加,而静态转矩系数与所研究范围内的雷诺数无关。在给定的雷诺数下,功率系数,扭矩系数和静态扭矩系数与阻塞比无关。

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