[Retracted] Streamline Effect Improvement of Additive Manufactured Airfoil Utilizing Dynamic Stream Control Procedure

Table 4

C_l and C_d values of at various AOA.

α (°)	Basic aerofoil		With 1^st module open		With 2^nd module open		With 3^rd module open
	Cl	Cd	Cl	Cd	Cl	Cd	Cl	Cd
0	0.11	0.07	0.15	0.07	0.11	0.05	0.18	0.06
5	0.78	0.02	0.87	0.02	0.71	0.02	0.73	0.02
10	1.02	0.02	1.19	0.02	0.96	0.03	1.01	0.02
15	1.02	0.05	1.11	0.05	0.97	0.05	0.91	0.04
20	0.66	0.06	0.54	0.08	0.63	0.07	0.66	0.05