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Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
AG 36 8.17 27.883 2.203 35.6838 1.076 0.0101
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AG03 (flat aft bottom) 6.24 25.6511 2.013 31.8857 0.981 0.0076
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AG04 6.42 21.8852 1.703 39.3636 0.931 0.0077
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AG08 5.83 14.2151 1.934 26.7002 0.907 0.007
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AG09 4.86 15.9674 1.795 33.2344 0.886 0.0096
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