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| DC 欄位 | 值 | 語言 |
|---|---|---|
| dc.contributor.advisor | 楊鏡堂(Jing-Tang Yang) | |
| dc.contributor.author | Yu-Chen Tsai | en |
| dc.contributor.author | 蔡語誠 | zh_TW |
| dc.date.accessioned | 2021-05-15T17:55:33Z | - |
| dc.date.available | 2014-07-15 | |
| dc.date.available | 2021-05-15T17:55:33Z | - |
| dc.date.copyright | 2014-07-15 | |
| dc.date.issued | 2014 | |
| dc.date.submitted | 2014-07-10 | |
| dc.identifier.citation | Alexander, D. E. (1986), ”Wind tunnel studies of turns by flying dragonflies,” The Journal of Experimental Biology, 122, pp. 81-98.
Azuma, Akira and Watanabe, Tadaaki (1988), “Flight performance of a dragonfly,” The Journal of Experimental Biology, 137, pp. 221-252 Chung, H. C., Lal Kummari, K., Croucher, S. J., Lawson, N. J., Guo, S. J. and Huang, Z. (2008), “Coupled piezoelectric fans with two degree of freedom motion for the application of flapping wing micro aerial vehicles,” Sensors and Actuators A, 147, pp. 607–612. Dickinson, M. H. (1994), “The effects of wing rotation on unsteady aerodynamic performance at low Reynolds numbers,” The Journal of Experimental Biology, 192, pp. 179–206. Dickinson, M. H. (1999), “Wing rotation and the aerodynamic basis of insect flight,” Science, 284, pp. 1954-1960 Fry, S. N., Sayaman, R. and Dickinson, M. H. (2003), “The aerodynamics of free-flight maneuvers in Drosophila,” Science, 300, pp. 495-498 Fry, S. N., Sayaman, R. and Dickinson, M. H. (2005), “The aerodynamics of hovering flight in drosophila,” The Journal of Experimental Biology, 208, pp. 2303-2318 Hsieh, C. T., Kung, C. F., Chang, C. C. and Chu, C. C. (2010), “Unsteady aerodynamics of dragonfly using a simple wing–wing model from the perspective of a force decomposition,” Journal of Fluid Mechanics, vol. 663, pp. 233-252 Jardin, T., David, L. and Farcy, A. (2009), “Characterization of vortical structures and loads based on time-resolved PIV for asymmetric hovering flapping flight,” Experiments in Fluids, 46, pp. 847–857 Marden, J. H., (1987), “Maximum lift production during takeoff in flying animals,” The Journal of Experimental Biology,130, pp.235-258 Norberg, R. A. (1975), “Hovering flight of the dragonfly aeschna juncea l., kinematics and aerodynamics,” Swimming and Flying in Nature,” vol.2, pp. 763-781 Pines, DarryII J. and Bohorquez, F. (2006), “Challenges facing future micro-air-vehicle development,” Journal of Aircraft, vol. 43, No.2, pp. 290-305 Ristroph, L., Ristroph, G., Morozova, S., Bergou, A. J., Chang, S., Guckenheimer, J., Wang, Z. J. and Cohen, I. (2013), “Active and passive stabilization of body pitch in insect flight,” Journal of the Royal Society Interface, 10, 20130237 Rudolph, R. (1976), “Preflight behaviour and the initiation of flight in tethered and unrestrained dragonfly, Calopteryx splendens (Harris) (Zygoptera: Calopterygidae),” Odonatologica, 5, p.p. 59-64 Sato, Machiko and Azuma, Akira (1997), “The flight performance of a damselfly ceriagrion melanurum selys,” The Journal of Experimental Biology, 200, pp. 1765–1779 Sane, S. P. (2003), “The aerodynamics of insect flight,” The Journal of Experimental Biology, 206, pp. 4191-4208 Shyy, W., Berg, M. and Ljungqvist, D. (1999), “Flapping and flexible wings for biological and micro air vehicles,” Progress in Aerospace Sciences, 35, pp.455-505 Sun, Mao and Lan, Shi-Long (2004), “A computational study of the aerodynamic forces and power requirements of dragonfly (Aeschna juncea) hovering,” The Journal of Experimental Biology, 207, pp.1887-1901 Taylor, G. K. (2001), “Mechanics and aerodynamics of insect flight control,” Biological Reviews, 76, pp. 449-471 Taylor G. K., Nudds, R. L. and Thomas, A. L. R. (2003), “Flying and swimming animals cruise at a Strouhal number tuned for high power efficiency,” Nature, 425, p.p. 707-711 Thomas, A. L. R., Taylor, G. K., Srygley, R. B., Nudds, R. L. and Bomphrey, R. J. (2004), “Dragonfly flight: free-flight and tethered flow visualizations reveal a diverse array of unsteady lift-generating mechanisms, controlled primarily via angle of attack,” The Journal of Experimental Biology, 207, pp. 4299-4323 Wakeling, J. M. and Ellington, C. P. (1997), “Dragonfly flight II. velocities, accelerations and kinematics of flapping flight,” The Journal of Experimental Biology, 200, pp. 557-582 Wakeling, J. M. and Ellington, C. P. (1997), “Dragonfly flight III. lift and power requirements,” The Journal of Experimental Biology, 200, pp. 583–600 Wagner, H. (1925). “The production of dynamic lift on wings,” Journal of Applied Mathematics and Mechanics, 5. Wang, H., Zeng, L., Liu, H., and Yin, C. (2003), “Measuring wing kinematics, flight trajectory and body attitude during forward flight and turning maneuvers in dragonflies,” The Journal of Experimental Biology, 206, pp. 745-757 Weis-Fogh, T. (1973), “Quick estimates of flight fitness in hovering animals, including novel mechanisms for lift production,” The Journal of Experimental Biology, 59, pp.169-230 | |
| dc.identifier.uri | http://tdr.lib.ntu.edu.tw/jspui/handle/123456789/5306 | - |
| dc.description.abstract | 本文選用台灣常見的豆娘中華珈璁以及細胸珈璁作為實驗物種,將其放入特製之狹長型透明壓克力觀測箱中,觀測豆娘在其中試圖迴避四周壁面而由原本向前飛行轉換至向後飛行的急遽變化。實驗分析使用高速攝影機捕捉豆娘迴旋時的拍翅動作以及身體俯仰動作,並利用二維PIV技術將流場可視化,找出影響轉彎的關鍵運動學參數及限制,並藉由比較拍翅運動學和流場渦旋互動歸納出豆娘特殊的轉彎策略。
結果顯示豆娘在不同雷諾數(Reynolds number)區間下會採用兩種不同的迴旋模式,分別是低雷諾數(50~300)的往復式急迴旋以及中高雷諾數(200~700)的旋轉式急迴旋。頭部加速度與飛行雷諾數成正相關。低雷諾數下(Re < 300)豆娘以增加拍翅頻率(+26%)獲得頭部加速度的大幅提升(+100~120%),高雷諾數(Re > 200)下豆娘則普遍藉由降低拍翅平面角度改變阻力作用點,使身體旋轉以大幅增加頭部加速度(+70~75%)。並且隨著雷諾數提高,豆娘之史卓荷數(Strouhal number)會趨近約0.2,以Taylor (2003) 之觀點可視為迴旋飛行操控之最佳能量效率操作點。 流場分析顯示在穩定前飛期間,豆娘前翅翼前緣渦旋(leading edge vortex, LEV)逸散緩慢,上下拍轉換期間會停留在前翅後方與後翅上方之狹窄區間,並與後翅翼前緣渦旋融合,強度提升至最高160 1/s並持續維持約半周期;此現象說明豆娘能夠以低於蜻蜓一半的拍翅頻率飛行,並在急迴旋期間之懸停階段藉由相似機制提供足夠升力之原因。 研究中之豆娘運動學參數可被使用於更具有操控潛能之微飛行器利用,並期望能改善能源使用效率之目的。 | zh_TW |
| dc.description.abstract | The turning mechanics of damselfly species Psolodesmus mandarinus and Mnais tenuis is investigated. When free-flying in highly-confined acrylic chambers, damselflies are observed to decelerate from forward fly status and perform special turning maneuver in order to avoid impact. High speed camera (fps>1000) is used to capture transient flapping trajectories and body posture while two dimensional PIV technique reveals the transient flow field and vortices patterns. The study focuses on finding the key kinematic parameters influencing the turning ability and deducing the turning strategies by combining flapping kinematics and vortices interaction.
Results show that damselflies mainly use two different kinds of turning modes according to their forward fly Reynolds number and the head acceleration increases with increasing Reynolds number. When the Reynolds number is lower than 300, damselflies perform “reciprocating turn” while they shift to “rotational turn” when the Reynolds number is greater than 200. During reciprocating turn, damselflies increase their flapping frequency to increase their head acceleration up to 120% compared to counterparts with same Reynolds number. In rotational turn, damselflies adjust their stroke plane angle to change the location of the drag force. A net moment is thus created to rotate the body, enhancing the head acceleration up to 75% compared to counterparts with same Reynolds number. Additionally, as Reynolds number increases, the operating Strouhal number for damselflies is shown to approach a constant of 0.2, which agrees with Taylor (2003) that flapping insects operate at certain Strouhal numbers in order to achieve high energy efficiency. The study also discovers that during both forward fly and turning maneuver, the slowly-shed fore wing LEVs interact with hind wing LEVs between the gaps of two wings, forming sustaining vortices with vorticity up to 160 1/s. The vortices interaction mechanism strengthens the facts that under same flying speed a damselfly can operate with half the flapping frequency compared to a dragonfly and, during hovering stage in turning maneuver, the lift is sufficient to provide body support. Flapping kinematics obtained in the study can be used to design and fabric more agile and energy-saving micro air vehicles capable of challenging tasks. | en |
| dc.description.provenance | Made available in DSpace on 2021-05-15T17:55:33Z (GMT). No. of bitstreams: 1 ntu-103-R01522107-1.pdf: 4581532 bytes, checksum: 6c0aa01d83e7d261dadbd55376624a7b (MD5) Previous issue date: 2014 | en |
| dc.description.tableofcontents | 口試委員會審定書 ii
誌謝 iii 中文摘要 iv 英文摘要 v 目錄 vii 圖目錄 ix 表目錄 xi 符號說明 xii 第一章 前言 - 1 - 1-1 研究背景與動機 - 1 - 1-2 研究目的 - 2 - 第二章 文獻回顧 - 3 - 2-1 名詞解釋 - 3 - 2-2 微飛行器 - 5 - 2-2.1 起源與形式 - 5 - 2-2.2 飛行器的種類 - 6 - 2-2.3 微型飛行器的發展困境 - 7 - 2-3 拍撲翼飛行機制 - 7 - 2-3.1 渦度與環流量 - 7 - 2-3.2 Kutta-Joukowski 定理 - 8 - 2-3.3 翼前緣渦旋與延遲失速現象 - 8 - 2-3.4 尾流捕捉 - 9 - 2-3.5 拍翼與拋翼 - 9 - 2-4 豆娘 - 10 - 2-4.1 豆娘構造簡介 - 10 - 2-4.2 豆娘振翅結構 - 10 - 2-5 蜻蜓與豆娘的飛行 - 11 - 2-5.1 穩定前飛研究 - 11 - 2-5.2 操控性飛行研究 - 12 - 第三章 研究方法 - 15 - 3-1 實驗參數與因次分析 - 16 - 3-2 實驗對象 - 18 - 3-3 動作分析 - 19 - 3-3.1 觀測平台與高速攝影機 - 19 - 3-3.2 分析方法 - 20 - 3-4 流場分析 - 21 - 3-4.1 粒子影像測速法原理 - 21 - 3-4.2 實驗架設 - 22 - 3-5 機構實作 - 24 - 第四章 結果與討論 - 27 - 4-1動作與運動學參數分析 - 27 - 4-1.1迴旋動作和參數定義 - 27 - 4-1.2急迴旋運動學參數總覽 - 29 - 4-1.3前飛和迴轉動作比較 - 32 - 4-1.4頻率調控機制 - 34 - 4-1.5拍翅平面角度調控機制 - 35 - 4-1.6 攻角 - 36 - 4-1.7身體俯仰角調控機制與轉彎策略 - 37 - 4-2 流場分析 - 38 - 4-2.1穩定前飛 - 38 - 4-2.2 急迴旋 - 39 – 4-3 中華珈璁與細胸珈璁力學特性比較- 47 - 第五章 結論與展望 - 49 - 甘梯圖 - 50 - 參考文獻 - 51 - | |
| dc.language.iso | zh-TW | |
| dc.subject | 翼前緣渦旋 | zh_TW |
| dc.subject | 渦旋互動 | zh_TW |
| dc.subject | 豆娘 | zh_TW |
| dc.subject | 操控性飛行 | zh_TW |
| dc.subject | 轉彎 | zh_TW |
| dc.subject | 身體俯仰角 | zh_TW |
| dc.subject | leading edge vortex | en |
| dc.subject | damselfly | en |
| dc.subject | maneuvering flight | en |
| dc.subject | turning | en |
| dc.subject | body pitch angle | en |
| dc.subject | vortices interaction | en |
| dc.title | 豆娘穩定前飛與急停迴旋之力學機制探討 | zh_TW |
| dc.title | Investigation of steady forward flight and sharp turning mechanism of damselfly | en |
| dc.type | Thesis | |
| dc.date.schoolyear | 102-2 | |
| dc.description.degree | 碩士 | |
| dc.contributor.oralexamcommittee | 紀凱容,楊瑞珍,吳宗信 | |
| dc.subject.keyword | 豆娘,操控性飛行,轉彎,身體俯仰角,翼前緣渦旋,渦旋互動, | zh_TW |
| dc.subject.keyword | damselfly,maneuvering flight,turning,body pitch angle,leading edge vortex,vortices interaction, | en |
| dc.relation.page | 53 | |
| dc.rights.note | 同意授權(全球公開) | |
| dc.date.accepted | 2014-07-10 | |
| dc.contributor.author-college | 工學院 | zh_TW |
| dc.contributor.author-dept | 機械工程學研究所 | zh_TW |
| 顯示於系所單位: | 機械工程學系 | |
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