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Guo W.,Northwestern Polytechnical University | Song W.,Northwestern Polytechnical University | Hou Y.,The First Aircraft Institute of AVIC 1
Taiyangneng Xuebao/Acta Energiae Solaris Sinica | Year: 2012

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. Source

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