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研究生:侯詞軒
研究生(外文):Tzu-Hsuan Hou
論文名稱:蝴蝶翼展尺寸效應及飛行動態策略
論文名稱(外文):Scale Effect of Wing Span and Flight Kinematic Strategies in Free-Flying Butterflies
指導教授:楊鏡堂楊鏡堂引用關係
口試日期:2017-07-18
學位類別:碩士
校院名稱:國立臺灣大學
系所名稱:機械工程學研究所
學門:工程學門
學類:機械工程學類
論文種類:學術論文
論文出版年:2017
畢業學年度:105
語文別:中文
論文頁數:74
中文關鍵詞:蝴蝶尺寸差異數值分析動作分析翼面負重空氣作用力
外文關鍵詞:size effectnumerical analysismotion analysiswing loadingaerodynamics force
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本文透過生物實驗與數值模擬方式分析蝴蝶尺寸對於飛行表現及飛行動態之影響,並從中提出小型蝶類提升翅膀負重與速度調控之機制與策略。實驗首先透過高速攝影機拍攝翼展差異明顯之四種蝴蝶(介於136-44 mm)於實驗箱中進行自由飛行,並篩選蝴蝶於前飛模式下之動態,藉由影像處理軟體對其動作分析。然而,由於實驗中過多參數之影響,造成部分趨勢不明顯,因此本文進一步透過數值模擬方式控制變因,定量分析尺寸差異對於飛行之影響,並比較實驗與模擬所呈現之結果。
實驗量測結果顯示蝴蝶翼面負重與翼展尺寸有正相關的趨勢,相較於數值計算之結果,在飛行動態固定之情況下,蝴蝶平飛時計算之翼面負重會隨翼展迅速下降,數值模擬預測小型蝶類所能承受之翅膀負重相較於真實蝶類不理想;在飛行動態方面,真實小型蝶類之拍撲頻率和身體俯仰振幅有高於大型蝶類之趨勢,因此推測小型蝶類可能透過動態差異提升翼面負重達到更好之飛行表現,因此本文進一步探討提升拍撲頻率和身體俯仰振幅動態對小型蝶類空氣作用力與功率產生之影響。透過數值模擬之方式,分析提升頻率與身體俯仰動態對於蝴蝶飛行之影響,研究結果發現兩者皆能有效提升蝴蝶翼面負重使達成穩定飛行,而前者對於蝴蝶能達到較高之飛行速度,但需要較多之空氣動力功率;而後者所能達到之飛行速度較低,但相對較節能,透過此兩動態之調配可進行飛行速度與飛行功率之調整。
本研究提供蝴蝶尺寸與翼面負重、功率與飛行速度等之關係,其可做為未來仿蝴蝶飛行器在尺寸、重量與馬達設計及材料選擇上重要之參考準則;此外,透過實驗與數值模擬結果之差異,本文提出運用飛行動態達到微飛行器飛行速度與功率之調控策略。
The scale of butterflies largely variate among species, and might affect their flight performance intrinsically. In this work, we carry out experimental observations and numerical analysis to investigate how flight performances and flight motions of butterflies correlate with their sizes, and a flight strategy to enhance wing loading of small size butterflies is proposed accordingly.
Four different species of Taiwan butterflies with significant differences on wingspan (variating from 44-136 mm) were selected to study experimentally. The motions of butterflies were recorded with high-speed cameras when they were freely flying in an experimental chamber. The images of flight that close to forward flight were selected and analyze with the image processing software (Image J). The experimental results indicate that the wing loading of butterflies positively correlate to their wingspan, and the irregularity of the flight trajectory is not as evident as the previous research (Dudley, 1990). In addition, the flapping frequency and body angle amplitude of the small butterflies are found to be higher than that of large butterflies in our experiments.
Numerical models of butterflies in different scales are further created to analyze the size effect quantitatively since various parameters in experiments are combined and are unable to control separately. The butterfly in the simulation translate freely along the vertical and horizontal directions; the flight speeds determined by calculating the aerodynamic force and gravity force. The shape and flight motions of butterflies are considered as the same in each cases, and the mass is manually controlled to find the maximum wing loading of butterflies in specific size. The simulations results show that the wing loading decreases with the wingspan sharply while the shapes and the flight motions are considered as the same. The decreasing rate is more rapid than the trend recorded from experiments, which implies that small butterflies may adjust their flight motions, flapping frequency and body angle amplitude in our observation, to enhance their wing loading in nature. To clarify the effects of these two motions, we further adjust the flapping frequency and rotation amplitude in the simulation model. The results show that both ways effectively improve the wing loading of the butterflies as excepted; moreover, the butterflies are able to achieve higher forward speed with the former motion and are more energy-efficient with the latter motion. Butterflies may alter the flapping frequency or rotation amplitude.
Our results provide relations between the size of butterflies and the flight parameters. In an engineering perspective, these relations are especially important for the designing of flight vehicles; for example, determining the total weight of vehicles and power required of the motor. In addition, by comparing the difference between the experimental and simulation results, we proposed a motion control strategy to adjust the flight speed and power consumption of micro aircraft vehicles.
目錄
符號說明 vi
目錄 viii
圖表目錄 x
第一章 前言 1
第二章 文獻回顧 3
2.1 微型飛行器之發展 3
2.2 飛行之背景知識 4
2.2-1 名詞介紹 4
2.2-2 升力和阻力 5
2.2-3 壓力中心、空氣動力中心和失速 6
2.2-4 渦度與環流量 6
2.2-5 Kutta-Joukowski定理 7
2.2-6 華格納效應 (Wagner effect) 7
2.3 昆蟲飛行之物理機制 9
2.3-1 名詞介紹 9
2.3-2 翼前緣渦漩貼附(leading edge vortex attachment) 11
2.3-3 翼尖渦漩 (wing tip vortex) 13
2.3-4 夾翼與拋翼 (clap and fling) 15
2.3-5 尾流捕捉效應(wake capture) 15
2.3-6 翅膀旋轉(wing rotation) 16
2.3-7 翅膀撓性 (wing flexibility) 17
2.4 蝴蝶相關研究 19
2.4-1 蝴蝶之構造 19
2.4-2 蝴蝶身體動態之研究 20
2.4-3 生物尺寸大小與飛行關係之相關研究 22
2.4-4 預期貢獻 24
第三章 研究方法 25
3.1 研究對象 26
3.2 因次分析 28
3.3 實驗分析 30
3.3-1 實驗設備架設 30
3.3-2 動作分析 31
3.3-3 數據分析 32
3.4 數值模擬 35
3.4-1 統御方程式 35
3.4-2 軟體介紹 35
3.4-3 網格介紹 35
3.3-4 動態網格 36
3.3-5 物理建模 37
3.3-6 動作參數和數值運算 39
第四章 結果與討論 41
4.1 實驗觀察 42
4.1-1生物特徵記錄 42
4-4.2飛行表現與尺寸趨勢與回歸 48
4.2 數值模擬 55
4.2-1 尺寸定量分析 55
4.2-2 自由飛行模擬動態分析 57
4.2-3 飛行動態分析 60
第五章 結論與未來展望 64
5.1 結論 64
5.2 未來展望 65
第六章 附錄 66
第七章 參考文獻 72
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