Aerodynamic experimental investigation for mechanism of lift and thrust of flexible flapping-wing MAV
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Aerodynamic experimental investigation for mechanism of lift and thrust of flexible flapping-wing MAV
Vol. 22, Issue 11, (2007)
作者机构:
南京航空航天大学 微型飞行器研究中心,南京,210016
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Published:2007
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ANG Hai-song, ZENG Rui, DUAN Wen-bo, et al. Aerodynamic experimental investigation for mechanism of lift and thrust of flexible flapping-wing MAV[J]. 2007, 22(11).
DOI:
ANG Hai-song, ZENG Rui, DUAN Wen-bo, et al. Aerodynamic experimental investigation for mechanism of lift and thrust of flexible flapping-wing MAV[J]. 2007, 22(11).DOI:
Aerodynamic experimental investigation for mechanism of lift and thrust of flexible flapping-wing MAV
Anew flapping-wing model of MAV(Micro Air Vehicle) with flexible structure was developed in order to explore mechanism of lift and thrust generation in flexible flapping-wing MAV.Wind tunnel test demonstrated the downstroke of the flapping-wing by utilizing laser instrument.Variation of the lift and thrust of flexible flapping-wing under conditions of different flap parameters such as flap frequency
angle of attach
flow speed and so on was investigated and compared with computed results.The research provides reference for design of flapping-wing MAV.The flight tests of the Flexible Flapping-wing MAVconducted in Research Center of MAVof NUAAwere also successfully completed.