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

Table 8

Validation of the NASA SC(2)-0714 rotor.

S. no.	Velocity	Exp lift force	CFD lift force	% of error
1	10	1680.599	1980	15.12
2	14	2957.085	3384	12.61
3	19	3701.167	4251	12.93
4	25	5061.041	5754	12.04
5	30	6844.272	7600	9.94
6	35	8326.021	9051	8.01