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Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
CLARK W 11.21 30 3.684 40 1.643 0.0075
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CLARK Y 11.73 30.87 3.528 43.47 1.595 0.006
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CLARK YH 11.9 30 2.45 30 1.392 0.0095
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CLARK YS 11.7 30 2.353 30 1.274 0.0055
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DAE51 9.38 30.94 3.465 46.07 1.186 0.0078
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