Development of deployable wing glider
This report will explore the development of a deployable wing mechanism for use in gliders of wingspan 1-1.5 metres. The wing will be stowed along the fuselage prior to launch and will be deployed to its desired location in flight. The objective of wing stowage is to achieve a higher height attainme...
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| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2013
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/53541 |
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| 機構: | Nanyang Technological University |
| 語言: | English |