Table 2 Thrust and airspeed MAPE results for all four loading conditions
From: Experimental and numerical study of novel Coanda-based unmanned aerial vehicle
Mean absolute percentage error (%) | ||||
|---|---|---|---|---|
Propeller | Without Coanda surface | Overall | Isolated propeller | |
Thrust | 4.3% | 6.7% | 5.4% | 7.8% |
Airspeed | 3.3% | 7.9% | 6.1% | 4.1% |