Research Article
A New Aerodynamic Optimization Method with the Consideration of Dynamic Stability
Table 2
Aerodynamic parameters after conventional optimization.
| Parameters | Original airfoil | Conventional optimization |
| | 0.406184 | 0.6082 | | 0.01240452 | 0.012 | Lift-to-drag ratio | 32.74 | 50.68 | | 12% | 12.6% | | ā2.11 | 16.32 |
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