Design and aerodynamic analysis of a flapping-wing micro aerial vehicle

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Title:	Design and aerodynamic analysis of a flapping-wing micro aerial vehicle
Authors:	蔡博章 Tsai, Bor-Jang
Contributors:	機械工程學系 Mechanical Engineering
Keywords:	平板薄膜翼;振翅翼;微飛機 Planar membrane wing;Flapping wing;MAV
Date:	2009
Issue Date:	2014-06-27 03:08:53 (UTC+8)
Abstract:	本研究之目的針對平板薄膜翼之氣動性能做一個探討，並以模擬結果之平均升力值做為振翅翼微飛機之重量依據(重量必須低於8.78克)，設計製造一台振翅翼微飛機。本研究將從兩個方向來做探討，第一是針對平板薄膜翼型做三維氣動力數值計算與流場狀態模擬，分析不同振翅頻率及不同攻角下，壓力分佈、翼尖渦流及上洗氣流之情形。第二是以模擬結果之平均升力值8.78克，做為設計微飛機之重量限制，設計製造一架總重量8克、翼展15公分、弦長5公分之振翅翼微飛機。藉由對四連桿機構的概念，設計完整的拍翅機構來模擬鳥類的動作，並可以控制向上及 This paper presents the design and aerodynamic performance of a planar membrane wing as shape airfoil for the micro aerial vehicle. This simulation calculates the average lift force, L as the criteria weight of the flapping wing (weight must be lower than
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