Research Article
Computational Acoustic Beamforming for Noise Source Identification for Small Wind Turbines
Table 1
Lift and drag coefficients comparison for the NACA 0012 airfoil at zero degree angle-of-attack.
| | | Experiment [23, 24] | Simulation (time-averaged) |
| | 0 | 0.0105 | | (0.0062, 0.0082) | 0.0065 |
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