Table 3 CFD force distribution across different surfaces of novel design from 4000 RPM to 8000 RPM
From: Experimental and numerical study of novel Coanda-based unmanned aerial vehicle
Rotation speed (RPM) | Propeller (N) | Baseplate (N) | Coanda surfaces (N) | Overall thrust (N) |
|---|---|---|---|---|
4000 | 0.62 | 0.96 | 0.52 | 0.18 |
6000 | 1.52 | 1.98 | 1.21 | 0.75 |
8000 | 2.88 | 3.55 | 2.28 | 1.61 |