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研究生: 李秉樺
Lee, Ping-Hua
論文名稱: 蝴蝶之翼形與撲翼模式對飛行之影響研究
The effects of flapping-wing patterns and the wing-shape of butterflies on flight
指導教授: 葉孟考
Yeh, Meng-Kao
楊鏡堂
Yang, Jing-Tang
口試委員:
學位類別: 碩士
Master
系所名稱: 工學院 - 動力機械工程學系
Department of Power Mechanical Engineering
論文出版年: 2009
畢業學年度: 97
語文別: 中文
論文頁數: 85
中文關鍵詞: 蝴蝶流場可視化翼形拍撲機構
外文關鍵詞: butterfly, flow visualization, wing-shape, flapping mechanism
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  • 大自然界的各種飛行生物,昆蟲、鳥類、哺乳類等,均選擇了撲翼的方式來飛行,這些飛行生物為了產生更大的推進力量與更好的操控性,共同特點是具有低雷諾數、高的表面積/體積比以及飛行動作複雜,而撲翼飛行比起傳統固定翼飛行更能適合這種飛行方式。本研究的主旨在於深入瞭解蝴蝶之飛行動作,歸納蝴蝶在不同飛行模式下的撲翼動作,對自然飛行(free flight)作更深入的分析,希望可以證實創新的升力/推進力理論。歸納出撲翼攻角(angle of attack)、撲翼頻率(wing beat frequency)、撲翼幅度(wing beat amplitude)等相關參數與升力及推進力之間的關係,同時也探討其動作與飛行操控性之關係,分析蝴蝶飛行動作以及飛行時產生的流場。透過仿生拍撲機構的實驗,進一步討論展弦比(aspect ratio)、雷諾數(Re)、史卓赫數(St)、尾凸(tail)、翼縫(wing gap)對於飛行的影響,得到往復雷諾數與轉動雷諾數有正比的關係,展弦比對轉動雷諾數沒有太大影響;史卓赫數接近最佳效率時均為小展弦比,證實小展弦比的蝴蝶適合拍撲飛行,大展弦比的蝴蝶適合滑翔;發現蝴蝶在飛行時也使用間隙效應的高升力機制,利用自行設計的機構加以驗證;在翼片加入尾突結構會使轉動雷諾數增大,原因為尾突可以影響翼片所打出的渦流環中心射流的角度,增加有效推進力。


    摘 要 i Abstract ii 目 錄 iv 圖表目錄 vii 第一章 前 言 1 第二章 文獻回顧與分析 4 2-1無人飛行器(unmanned aerials vehicles, UAVs) 5 2-2微小化飛行器(Micro aerials vehicles, MAVs) 5 2-3目前MAVs發展時所遇到的問題 6 2-3.1飛行時處於低雷諾數,不適用傳統空氣動力學理論 6 2-3.2 提供的升力不足 6 2-3.3推進系統的設計困難 7 2-4昆蟲與鳥之比較 7 2-5名詞介紹 8 2-6昆蟲撲翼特性 10 2-7 反向卡門渦串 (Reversed von Karman vortex) 11 2-8渦度與環流量 12 2-9 史卓荷數 (Strouhal number) 13 2-10昆蟲撲翼飛行產生升力的物理機制: 13 2-10.1 Clap and fling mechanism 13 2-10.2 翼前緣渦流 (leading edge vortex) 14 2-10.3 Wake capture 14 2-10.4 Wing rotation 15 2-10.5 Added mass 15 2-11昆蟲介紹 15 2-11.1昆蟲胸部結構 15 2-11.2昆蟲振翅機制 16 2-11.2昆蟲翅膀結構 17 2-11.3蝴蝶 18 2-11.4蝴蝶翅膀顏色 19 2-11.4昆蟲飛行研究 20 2-12翼形狀影響 22 2-13 間隙效應(Gap effect) 23 2-14人為模擬昆蟲撲翼 24 第三章 研究方法 25 3-1實驗參數 26 3-2無因次分析 27 3-4飼養蝴蝶 30 3-5自由與束縛飛行 32 3-6觀測平台之架設 32 3-7實驗設備 33 3-9粒子影像測速儀 (particle image velocimetry,PIV)原理 41 3-9 生物統計 43 3-10 實驗方法 44 第四章 結果與討論 47 4-1實體蝴蝶分析 48 4-1.1蝴蝶飛行動作 48 4-1.2似平衡分析 51 4-1.3渦流環分析 52 4-2 仿生拍撲機構分析 55 4-2.1翼片參數與實驗概述 55 4-2.2翼片參數對流場之影響 57 4-2.3 翼縫 63 4-2.4 尾突 69 第五章 結論與未來展望 78 5-1 結論 78 5-2未來展望 80 第六章 參考文獻 81

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