[Retracted] Wind Tunnel Testing and Validation of Helicopter Rotor Blades Using Additive Manufacturing

Table 9

Validation of HH02 rotor.

S. no.	Velocity	Exp lift force	CFD lift force	% of error
1	10	1417.605	1684	15.81
2	14	2103.956	2450	14.12
3	19	3245.737	3751	13.47
4	25	4502.979	5152	12.59
5	30	6061.703	6742	10.09
6	35	7440.82	8201	9.27