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...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2025-04-01
|
| Series: | Aerospace |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/12/4/317 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|