Aerodynamics Optimization of a Ducted Coaxial Rotor in Forward Flight Using Orthogonal Test Design

Table 3

Hovering thrust and trimmed torque versus mesh quantity based on MFR model at 6000 rpm.

6000 rpm					Expt.
(kg)	30.588	32.682	33.991	34.636	37.318
N·m	0.111	0.108	0.106	0.105	0.103