| The micro aerial vehicle (MAV) with flapping wings | |
|---|---|
| 學年 | 93 |
| 學期 | 2 |
| 發表日期 | 2005-07-10 |
| 作品名稱 | The micro aerial vehicle (MAV) with flapping wings |
| 作品名稱（其他語言） | |
| 著者 | 楊龍杰; Yang, Lung-jieh; Hsu, Cheng-kuei; Ho, Jen-yang; Wang, Hsin-hsiung; Feng, Gwo-hwa |
| 作品所屬單位 | 淡江大學機械與機電工程學系 |
| 出版者 | N.Y.: IEEE (Institute of Electrical and Electronic Engineers) |
| 會議名稱 | |
| 會議地點 | Taipei, Taiwan |
| 摘要 | The research of micro aerial vehicles (MAVs) is a new field of low-Reynolds-number flow, which attracts much attention in the advanced aeronautical area. The flapping wing, proved by many natural flyers, is the most appropriate way of flying objects which sizes are less than 6 inches. However, there is still plenty of room for studying on the unsteady aerodynamic characteristics of flapping wings. The flapping wing, which is light weighted and high strengthened, is originally composed of the titanium-alloy frame and the parylene skin. Such an integration of fabrication needs the help of MEMS processing. Additionally, the flapping test after the wing fabrication and the corresponding signal analysis from the smart wing skin concluded this project and set the bases for the wind-tunnel verification/correction in the very near future. |
| 關鍵字 | |
| 語言 | en |
| 收錄於 | |
| 會議性質 | 國內 |
| 校內研討會地點 | |
| 研討會時間 | 20050710~20050712 |
| 通訊作者 | |
| 國別 | TWN |
| 公開徵稿 | |
| 出版型式 | |
| 出處 | ICM '05. IEEE International Conference on Mechatronics, Taipei, pp.811-815 |
| 相關連結 |
機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/38040 ) |
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