A Parametric Design Method for Hybrid Airfoils for Icing Wind Tunnel Test

Table 2

Test parameters for Cp.

Case	Airfoil	AoA (°)	Flow speed (m/s)	Temperature (°C)	Atmosphere (kPa)
Case 1	Hy00	0	30	8.0	98.60
	NACA0012	0	30	11.6	97.68
Case 2	Hy02	2	30	4.5	98.94
	NACA0012	2	30	11.6	97.68
Case 3	Hy04	4	30	3.0	98.57
	NACA0012	4	30	11.6	97.68
Case 4	Hy06	6	30	3.5	98.67
	NACA0012	6	30	11.6	97.68
Case 5	Hy08	8	30	8.5	98.87
	NACA0012	8	30	11.6	97.68
Case 6	Hy010	10	30	8.0	98.91
	NACA0012	10	30	11.6	97.68
Case 7	Hy20	0	30	15.8	96.97
	NACA2412	0	30	28.7	95.40
Case 8	Hy22	2	30	13.0	98.19
	NACA2412	2	30	28.7	95.40
Case 9	Hy24	4	30	11.4	98.67
	NACA2412	4	30	28.7	95.40
Case 10	Hy26	6	30	11.8	97.95
	NACA2412	6	30	28.7	95.40