Research Article
A Parametric Design Method for Hybrid Airfoils for Icing Wind Tunnel Test
| 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 |
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