朱保利, 李强, 邹俊伟, 陈光盛. 扑翼微型飞行器风洞动态试验[J]. 南昌航空大学学报(自然科学版), 2011, 25(1): 18-21.
引用本文: 朱保利, 李强, 邹俊伟, 陈光盛. 扑翼微型飞行器风洞动态试验[J]. 南昌航空大学学报(自然科学版), 2011, 25(1): 18-21.
shu
ZHU Bao-li, LI Qiang, ZOU Jun-wei, CHEN Guang-sheng. Wind Tunnel Dynamic Experiments of Flapping-wing MAV[J]. Journal of nanchang hangkong university(Natural science edition), 2011, 25(1): 18-21.
Citation: ZHU Bao-li, LI Qiang, ZOU Jun-wei, CHEN Guang-sheng. Wind Tunnel Dynamic Experiments of Flapping-wing MAV[J]. Journal of nanchang hangkong university(Natural science edition), 2011, 25(1): 18-21.
shu

扑翼微型飞行器风洞动态试验

Wind Tunnel Dynamic Experiments of Flapping-wing MAV

    摘要
  • 摘要: 文章在低速风洞中进行了多自由度扑翼微型飞行器的吹风试验,实测了扑翼机的升力、阻力随扑动频率、迎角和来流速度等参数的不同而导致的变化情况,测量的扑动参数对扑翼微型飞行器的气动力特性均有较大的影响.

     

    Abstract: In order to investigate the MAV's aerodynamic characteristics,using multi-DOF flapping-wing MAV,the load measurement experiment was done in low-speed wind tunnel.The lift and drag were measured with different flapping frequency,attack angle and free-stream velocity.The influence of the flapping parameters on the MAV's aerodynamic characteristics was reported.The results could be helpful for the design of multi-DOF flapping-wing MAV.

     

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