Investigation of Aerodynamic Characteristics of Closed Wing Applied on High-Altitude, Long-Endurance Solar UAV
碩士 === 國立虎尾科技大學 === 飛機工程系航空與電子科技碩士班 === 106 === Closed wing has the advantage including low weight, high stiffness, low induced drag and good stability, and has great potential for development of HALE Solar UAV. This study focuses on reducing the structure weight as well as enhancing stability of ma...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2018
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| Online Access: | http://ndltd.ncl.edu.tw/handle/7hns68 |