# XFOIL data with adjustments for AR effects and clmax overprediction, wing profile drag only -90 0 -75 -.54 -65 -.8 -55 -1 -45 -.9 -35 -.7 -20 -.82 -10. -.6 7.0000000e+00 1.1245520e+00 9.0000000e+00 1.2525040e+00 1.1000000e+01 1.3198240e+00 1.3000000e+01 1.3647040e+00 1.7000000e+01 1.3429680e+00 2.0000000e+01 1.2785520e+00 25 1.085 35 1.08 40 1.1 45 1.1 55 1 65 .8 75 .54 90 0