Effect of Groove Size on Aerodynamic Performance of a Low Reynolds Number UAV Propeller (Part II)
Following on from the author's previous work on grooved propellers, numerical investigations are carried out on Applied Precision Composites Slow Flyer 10×7 propeller. Computational Fluid Dynamics is used to analyze the novel design. The grooved sections considered have a rectangular geometry m...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2022-12-01
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| Series: | INCAS Bulletin |
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| Online Access: | https://bulletin.incas.ro/files/seeni__vol_14_iss_4.pdf |