Static Performance Results of Propellers Used on Nano, Micro, and Mini Quadrotors
Static Performance Results of Propellers Used on Nano, Micro, and Mini Quadrotors
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纳米、微型和迷你四旋翼飞行器上使用的螺旋桨的静态性能结果
DOI：
10.2514/6.2018-4122
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发表时间：
2018
期刊：
影响因子：
--
通讯作者：
M. Selig
中科院分区：
文献类型：
--
作者：
Robert W. Deters;Or D. Dantsker;Stefan Kleinke;Narcrisha S. Norman;M. Selig
随着小型四旋翼机数量的增加，人们对这些飞机所使用的螺旋桨的性能数据产生了兴趣。由于飞机尺寸小于5英寸，螺旋桨直径小于3英寸，这些四旋翼通常被爱好者和制造商称为迷你，微型或纳米。在这些飞行器上使用的螺旋桨的尺寸在低雷诺数下操作，对于直径高达3英寸，该低雷诺数通常小于50，000，并且对于直径高达2英寸，该低雷诺数通常小于20，000。完成了11个小型四旋翼螺旋桨的静态性能试验。对于直径小于1.4英寸的螺旋桨，产生的扭矩太小，无法精确测量。
An increase in the number of small quadrotors has created the interest in having performance data on the propellers used by these aircraft. With an aircraft size less than 5 in and propellers diameters less than 3 in, these quadrotors are typically referred to mini, micro, or nano by hobbyists and manufacturers. The size of the propellers used on these aircraft operate at low Reynolds numbers that are typically less than 50,000 for diameters up to 3 in and less than 20,000 for diameters up to 2 in. Static performance testing of the propellers used on 11 small quadrotors was completed. For propellers with diameters less than 1.4 in, the torque produced was too small to accurately measure.