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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/38040

    Title: The micro aerial vehicle (MAV) with flapping wings
    Authors: 楊龍杰;Yang, Lung-jieh;Hsu, Cheng-kuei;Ho, Jen-yang;Wang, Hsin-hsiung;Feng, Gwo-hwa
    Contributors: 淡江大學機械與機電工程學系
    Date: 2005-07-10
    Issue Date: 2010-04-15 10:32:04 (UTC+8)
    Publisher: N.Y.: IEEE (Institute of Electrical and Electronic Engineers)
    Abstract: The 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 studying on the unsteady aerodynamic characteristics of flapping wings. The flapping wing, which is light weighted and high strengthened, is originally composed of the titanium-alloy frame and the parylene skin. Such an integration of fabrication needs the help of MEMS processing. Additionally, the flapping test after the wing fabrication and the corresponding signal analysis from the smart wing skin concluded this project and set the bases for the wind-tunnel verification/correction in the very near future.
    Relation: ICM '05. IEEE International Conference on Mechatronics, Taipei, pp.811-815
    DOI: 10.1109/ICMECH.2005.1529366
    Appears in Collections:[機械與機電工程學系暨研究所] 會議論文

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