Development and control of vortices over a very low aspect-ratio wing
The vortical structures over a thin rectangular wing with a very low aspect ratio (AR) of 0.277 are investigated in a wind tunnel at an effective Reynolds number of 3 × 106 . The maximum lift of this thin wing is found at an angle of attack of 42◦ . The flow separates at the leading-edge and reattac...
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| Format: | Thesis (University of Nottingham only) |
| Language: | English |
| Published: |
2022
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| Online Access: | https://eprints.nottingham.ac.uk/71606/ |