微型扑翼飞行器风洞试验初步研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2007, Vol. 28 ›› Issue (2): 275-280.

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Experimental Investigation of Flapping wing MAV in Wind Tunnel

SHAO Li-min，SONG Bi-feng，XIONG Chao，YANG Shu-li

School of Aeronautics, Northwestern Polytechnical University

Received:2005-12-21 Revised:2006-12-04 Online:2007-03-10 Published:2007-03-10
Contact: SONG Bifeng

Abstract

Abstract:

In order to quantificationally investigate the aerodynamics of flapping-wing MAV(Micro Air Vehicle)， the wind tunnel test of flapping-wing MAV is performed in special micro air vehicle wind tunnel of NPU(Northwestern Polytechnical University).The effects of flapping frequency， wind velocity， angle of attack， plane shape of wing and cambered aerofoil are investigated.In this experiment the producing rules of lift and thrust are found.The result of experiment can guide the conceptual design and aerodynamic design of the flapping-wing MAV.

Key words: flappingwing , micro , air , vehicle, , wing&rsquo, s , aerodynamic , characteristics, , wind , tunnel , test

CLC Number:

V211.7

SHAO Li-min;SONG Bi-feng;XIONG Chao;YANG Shu-li. Experimental Investigation of Flapping wing MAV in Wind Tunnel[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2007, 28(2): 275-280.

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Experimental Investigation of Flapping wing MAV in Wind Tunnel

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