Abstract
A estimation model was built to predict the aerodynamic characteristics of airfoils through ±180° angle of attack. The lift coefficients, drag coefficients, moment coefficients of full range section were estimated for NACA0012 airfoil, NACA0015 airfoil and DU96-W-180 airfoil. Comparisons between the model predictions and experiment data showed that the estimation model is reasonable.
Original language | English |
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Pages (from-to) | 717-722 |
Number of pages | 6 |
Journal | Taiyangneng Xuebao/Acta Energiae Solaris Sinica |
Volume | 33 |
Issue number | 5 |
State | Published - May 2012 |
Keywords
- Aerodynamic characteristic
- Airfoil
- Estimate
- Full range section
- Wind turbine