2011•Journal of Nanchang Hangkong UniversityRequires access

Wind Tunnel Dynamic Experiments of Flapping-wing MAV

Guang-Sheng Chen

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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Available abstract

Key concepts: Flapping, Aerodynamics, Aerospace engineering, Wind tunnel, Wing, Angle of attack, Lift-to-drag ratio, Lift (data mining)