關鍵字查詢 | 類別:期刊論文 | | 關鍵字:A flapping MAV with PVDF-parylene composite skin

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1 96/1 機電系 楊龍杰 教授 期刊論文 發佈 A flapping MAV with PVDF-parylene composite skin , [96-1] :A flapping MAV with PVDF-parylene composite skin期刊論文A flapping MAV with PVDF-parylene composite skin楊龍杰; Yang, L. J.; Hsu C.-K.; Feng, C.-K.; Ho, J.-Y.; Feng, G.-H.; Shih H.-M.淡江大學機械與機電工程學系Journal of the Aeronautics and Astronautics-Series A 39(3), pp.195-201The research of micro aerial vehicles (MAVs) is a new field of low-Reynolds-number flow, which attracts much attention in the advanced aeronautical area. The flapping wing, proved by many natural flyers, is the most appropriate way of flying objects which sizes are less than 6 inches. However, there is still plenty of room for people to investigate the unsteady aerodynamic characteristic of flapping wings. In this paper, the flapping wing of lightweight and high strength is composed of the titanium-alloy frame and the parylene skin. Such an integration of fabrication needs the help of MEMS processing technique. In the wind-tunnel test of the flapping MAV, the signals from load cell and PVDF film are used to detect the on-site
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