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 simulat...
| 出版年: | Aerospace |
|---|---|
| 主要な著者: | , |
| フォーマット: | 論文 |
| 言語: | 英語 |
| 出版事項: |
MDPI AG
2025-04-01
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| 主題: | |
| オンライン･アクセス: | https://www.mdpi.com/2226-4310/12/4/317 |