Aerodynamic Analysis of a Hexacopter with an Inner Tilted-Rotor Configuration During Hovering
The present work is aimed at investigating the arrangement design of an inner tilted-rotor hexacopter to optimize aerodynamic performance with different rotor spacing ratios (<i>s</i>/<i>D</i>) and dihedral angles (<i>β</i>). Both experiments and numerical simulations were applied for different roto...
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| Hlavní autoři: | , |
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| Médium: | Artigo |
| Jazyk: | Inglês |
| Vydáno: |
MDPI AG
2025-04-01
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| Edice: | Aerospace |
| Témata: | |
| On-line přístup: | https://www.mdpi.com/2226-4310/12/4/317 |
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