Open Access
Table 2
Geometric characteristics.
| Airfoil | Max thickness | Max camber |
|---|---|---|
| NACA 0015 | 15% | 0% |
| S1210 | 12% | 6.7% |
| S8037 | 16% | 1.9% |
| SG6040 | 16% | 2.3% |
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