Unsteady aerodynamics of a morphing tandem-wing unmanned aerial vehicle
The effects of unsteady aerodynamics for a tandem-wing unmanned aerial vehicle (UAV) prototype during the morphing stage have been investigated numerically at low Reynolds numbers (Re<10^6). The morphing stage consists of two stages. The first stage involves the unfolding of the canards and wings...
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| Main Authors: | , |
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| 其他作者: | |
| 格式: | Article |
| 語言: | English |
| 出版: |
2013
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| 在線閱讀: | https://hdl.handle.net/10356/85676 http://hdl.handle.net/10220/11677 |
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| 機構: | Nanyang Technological University |
| 語言: | English |