Aerodynamic Analysis of a Logistics UAV with Foldable Bi-wing Configuration
Herein, a twin-boom, inverted V-tailed unmanned aerial vehicle (UAV) featuring a foldable bi-wing configuration is proposed for logistics and transportation applications. We employed the Navier–Stokes solver to numerically simulate steady, incompressible flow conditions. By examining the effects of...
Saved in:
| Main Authors: | Xiaolu Wang, Wenlong Lu, Weiwei Liu, Changning Chen, Liangyu Zhao |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2023-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2023/3304048 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Design and Prototype Testing of a Smart SMA Actuator for UAV Foldable Tail Wings
by: Yan Cheng, et al.
Published: (2024-12-01) -
Design and Mechanical Analysis of Bionic Foldable Beetle Wings
by: Caidong Wang, et al.
Published: (2018-01-01) -
Wing Design for Class I Mini Unmanned Aerial Vehicles—Special Considerations for Foldable Wing Configuration at Low Reynolds Numbers
by: Eleftherios Karatzas, et al.
Published: (2025-04-01) -
Aerodynamic Analysis and Application of the Channel Wing Configuration Based on the Actuator Disk Model
by: Mingzhi Cao, et al.
Published: (2025-06-01) -
Aerodynamic Analysis and Simulation for a Z-Shaped Folding Wing UAV
by: Jin-Gang Wang, et al.
Published: (2024-09-01)