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...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Journal Article |
| Language: | English |
| Published: |
2013
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| Online Access: | https://hdl.handle.net/10356/85676 http://hdl.handle.net/10220/11677 |