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Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
A18 (original) 7.33 30 3.939 45 1.1 0.0069
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AG 10 10 15.999 6.443 32.1 1.798 0.015
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AG 27 6.11 22.1565 2.666 44.2161 1.066 0.0073
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AG 34 9.28 27.7194 2.485 36.863 1.236 0.0103
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AG 35 8.72 27.8827 2.341 35.6838 1.124 0.0099
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