Airfoil: WASP Builder: M. Fox Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 61100 Number of angles of attack: 33 alpha / Cl / Cm -5.89 -0.302 -0.0740 -4.26 -0.189 -0.0740 -2.66 -0.065 -0.0740 -1.05 0.081 -0.0740 0.33 0.281 -0.0740 1.95 0.515 -0.0740 3.38 0.640 -0.0740 4.97 0.778 -0.0740 6.62 0.915 -0.0740 8.12 1.029 -0.0740 9.60 1.140 -0.0740 11.21 1.214 -0.0740 12.58 1.227 -0.0740 14.05 1.037 -0.0740 15.68 1.003 -0.0740 17.15 1.023 -0.0740 18.56 1.025 -0.0740 16.87 1.035 -0.0740 15.47 1.093 -0.0740 13.98 1.071 -0.0740 12.56 1.254 -0.0740 10.98 1.229 -0.0740 9.50 1.153 -0.0740 7.91 1.037 -0.0740 6.41 0.919 -0.0740 4.79 0.790 -0.0740 3.37 0.668 -0.0740 1.76 0.520 -0.0740 0.32 0.300 -0.0740 -1.30 0.077 -0.0740 -2.80 -0.053 -0.0740 -4.35 -0.170 -0.0740 -5.84 -0.283 -0.0740 Tabulated from data in file AB00228.DAT & reduced using program Q01.00L Average Reynolds #: 101900 Number of angles of attack: 33 alpha / Cl / Cm -5.92 -0.339 -0.0740 -4.18 -0.199 -0.0740 -2.44 -0.052 -0.0740 -0.86 0.154 -0.0740 0.32 0.345 -0.0740 2.04 0.516 -0.0740 3.65 0.662 -0.0740 5.26 0.815 -0.0740 7.06 0.972 -0.0740 8.27 1.077 -0.0740 9.91 1.194 -0.0740 11.52 1.239 -0.0740 12.59 1.243 -0.0740 14.15 1.219 -0.0740 15.50 1.042 -0.0740 17.21 0.987 -0.0740 19.03 1.019 -0.0740 16.19 1.007 -0.0740 15.16 0.984 -0.0740 13.92 1.204 -0.0740 12.33 1.221 -0.0740 10.67 1.208 -0.0740 9.36 1.144 -0.0740 7.78 1.016 -0.0740 6.49 0.903 -0.0740 4.72 0.738 -0.0740 3.27 0.603 -0.0740 1.53 0.447 -0.0740 0.07 0.279 -0.0740 -1.26 0.074 -0.0740 -3.10 -0.132 -0.0740 -4.40 -0.228 -0.0740 -6.21 -0.380 -0.0740 Tabulated from data in file AB00143.DAT & reduced using program Q01.00L Average Reynolds #: 203200 Number of angles of attack: 33 alpha / Cl / Cm -5.90 -0.350 -0.0740 -4.10 -0.175 -0.0740 -2.62 0.018 -0.0740 -0.85 0.222 -0.0740 0.37 0.349 -0.0740 2.17 0.534 -0.0740 3.48 0.661 -0.0740 5.16 0.827 -0.0740 6.60 0.961 -0.0740 8.24 1.100 -0.0740 9.76 1.197 -0.0740 11.06 1.229 -0.0740 12.51 1.223 -0.0740 14.27 1.206 -0.0740 15.43 1.101 -0.0740 17.19 0.943 -0.0740 18.80 0.938 -0.0740 16.77 0.961 -0.0740 15.15 1.140 -0.0740 14.00 1.194 -0.0740 12.50 1.219 -0.0740 11.05 1.226 -0.0740 9.51 1.178 -0.0740 7.98 1.070 -0.0740 6.38 0.930 -0.0740 4.77 0.779 -0.0740 3.21 0.623 -0.0740 1.82 0.484 -0.0740 0.19 0.317 -0.0740 -1.45 0.152 -0.0740 -2.98 -0.042 -0.0740 -4.57 -0.237 -0.0740 -5.98 -0.370 -0.0740 Tabulated from data in file AB00230.DAT & reduced using program Q01.00L Average Reynolds #: 304100 Number of angles of attack: 33 alpha / Cl / Cm -5.97 -0.352 -0.0740 -4.26 -0.164 -0.0740 -2.55 0.042 -0.0740 -1.09 0.187 -0.0740 0.82 0.386 -0.0740 2.13 0.520 -0.0740 3.48 0.658 -0.0740 5.11 0.817 -0.0740 6.56 0.953 -0.0740 8.17 1.091 -0.0740 9.57 1.186 -0.0740 11.30 1.235 -0.0740 12.61 1.228 -0.0740 14.19 1.214 -0.0740 15.64 1.170 -0.0740 16.90 0.979 -0.0740 18.39 0.988 -0.0740 16.91 1.003 -0.0740 15.40 1.203 -0.0740 13.97 1.214 -0.0740 12.51 1.227 -0.0740 11.02 1.231 -0.0740 9.42 1.179 -0.0740 7.93 1.072 -0.0740 6.30 0.929 -0.0740 4.75 0.776 -0.0740 3.23 0.626 -0.0740 1.66 0.465 -0.0740 -0.16 0.280 -0.0740 -1.51 0.141 -0.0740 -3.18 -0.027 -0.0740 -4.75 -0.224 -0.0740 -6.18 -0.382 -0.0740 Tabulated from data in file AB00232.DAT & reduced using program Q01.00L File wasp.lft created on 12-05-1997 at 15:25:53 using program FORMAT