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Please use this identifier to cite or link to this item: http://hdl.handle.net/11133/2848

Title: 羽ばたき飛行機の羽ばたき時の流体力計測
Other Titles: ハバタキ ヒコウキ ノ ハバタキ ジノ リュウタイリョク ケイソク
"Measurement of aerodynamic forces for flapping Micro air vehicle"
Authors: 北川, 一敬
野村, 達也
鳥居, 祐太
KITAGAWA, Kazutaka
NOMURA, Tatsuya
TORII, Yuuta
Issue Date: 30-Sep-2014
Publisher: 愛知工業大学
Abstract: "Unmanned micro aerial vehicles(UMAV) have carried out unmanned missions the natural disaster and a forest fire on airborne survey, and direct sowing on farmland. Development of automatic and radio controlled pilot flight system of MAV have focused on an aerodynamic behavior of low Reynolds number effect for biofluid in unsteady regime. The motivation of present study is to design the beetle-like flapping micro air vehicle for disaster investigating and planetary exploring. To explain the outline of flapping mechanism, the results of the visualization of the flap motion and the experiment on little aerodynamic force measurement using the cantilever system."
URI: http://hdl.handle.net/11133/2848
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