Airfoil: SD7037 (B) Builder: D. Thompson Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 60300 Number of angles of attack: 49 alpha / Cl / Cm -5.98 -0.321 -0.0800 -4.49 -0.216 -0.0800 -3.67 -0.161 -0.0800 -2.42 -0.058 -0.0800 -1.49 0.005 -0.0800 -0.59 0.095 -0.0800 0.59 0.223 -0.0800 1.50 0.360 -0.0800 2.73 0.537 -0.0800 3.66 0.629 -0.0800 4.61 0.707 -0.0800 5.85 0.809 -0.0800 6.82 0.889 -0.0800 7.80 0.963 -0.0800 8.76 1.019 -0.0800 9.71 1.076 -0.0800 10.89 1.143 -0.0800 11.79 1.181 -0.0800 12.94 1.199 -0.0800 13.77 0.930 -0.0800 14.72 0.978 -0.0800 15.77 0.957 -0.0800 16.78 0.971 -0.0800 17.78 0.962 -0.0800 18.75 0.955 -0.0800 17.25 0.933 -0.0800 16.28 1.005 -0.0800 15.25 0.967 -0.0800 14.29 0.942 -0.0800 13.30 0.943 -0.0800 12.25 0.970 -0.0800 11.32 1.174 -0.0800 10.37 1.130 -0.0800 9.23 1.056 -0.0800 8.26 1.000 -0.0800 7.25 0.934 -0.0800 6.26 0.854 -0.0800 5.26 0.769 -0.0800 4.26 0.691 -0.0800 3.13 0.587 -0.0800 2.16 0.461 -0.0800 0.99 0.283 -0.0800 0.01 0.144 -0.0800 -0.98 0.058 -0.0800 -1.96 -0.024 -0.0800 -2.94 -0.097 -0.0800 -4.08 -0.191 -0.0800 -5.05 -0.256 -0.0800 -6.01 -0.325 -0.0800 Tabulated from data in file CL00797.DAT & reduced using program Q02.00L Average Reynolds #: 100200 Number of angles of attack: 49 alpha / Cl / Cm -5.95 -0.352 -0.0800 -4.64 -0.225 -0.0800 -3.42 -0.125 -0.0800 -2.52 -0.044 -0.0800 -1.39 0.070 -0.0800 -0.28 0.212 -0.0800 0.63 0.348 -0.0800 1.56 0.465 -0.0800 2.78 0.581 -0.0800 3.73 0.664 -0.0800 4.67 0.748 -0.0800 5.65 0.832 -0.0800 6.92 0.943 -0.0800 7.63 1.008 -0.0800 8.84 1.088 -0.0800 9.79 1.144 -0.0800 10.96 1.206 -0.0800 11.88 1.232 -0.0800 12.78 1.242 -0.0800 13.88 1.219 -0.0800 14.80 0.974 -0.0800 15.89 1.000 -0.0800 16.90 1.020 -0.0800 17.75 0.985 -0.0800 18.74 0.980 -0.0800 17.12 1.005 -0.0800 16.31 1.015 -0.0800 15.26 1.002 -0.0800 14.34 0.996 -0.0800 13.34 0.990 -0.0800 12.19 1.225 -0.0800 11.40 1.207 -0.0800 10.25 1.155 -0.0800 9.30 1.100 -0.0800 8.29 1.039 -0.0800 7.27 0.955 -0.0800 6.23 0.868 -0.0800 5.21 0.779 -0.0800 4.19 0.690 -0.0800 3.18 0.600 -0.0800 2.20 0.511 -0.0800 1.03 0.393 -0.0800 0.01 0.245 -0.0800 -1.01 0.105 -0.0800 -2.04 -0.013 -0.0800 -3.06 -0.102 -0.0800 -4.01 -0.181 -0.0800 -5.01 -0.260 -0.0800 -6.14 -0.367 -0.0800 Tabulated from data in file CL00799.DAT & reduced using program Q02.00L Average Reynolds #: 200600 Number of angles of attack: 49 alpha / Cl / Cm -6.05 -0.299 -0.0800 -4.56 -0.144 -0.0800 -3.54 -0.038 -0.0800 -2.39 0.079 -0.0800 -1.53 0.168 -0.0800 -0.40 0.270 -0.0800 0.71 0.370 -0.0800 1.71 0.467 -0.0800 2.55 0.552 -0.0800 3.66 0.661 -0.0800 4.66 0.771 -0.0800 5.66 0.864 -0.0800 6.78 0.962 -0.0800 7.64 1.034 -0.0800 8.70 1.110 -0.0800 9.76 1.179 -0.0800 10.81 1.234 -0.0800 11.83 1.269 -0.0800 12.81 1.273 -0.0800 13.73 1.251 -0.0800 14.79 1.228 -0.0800 15.58 1.003 -0.0800 16.67 1.018 -0.0800 17.65 1.049 -0.0800 18.61 1.036 -0.0800 17.15 1.017 -0.0800 16.27 1.026 -0.0800 15.23 1.038 -0.0800 14.31 1.049 -0.0800 13.30 1.262 -0.0800 12.43 1.276 -0.0800 11.34 1.250 -0.0800 10.44 1.211 -0.0800 9.41 1.149 -0.0800 8.32 1.073 -0.0800 7.24 0.992 -0.0800 6.31 0.909 -0.0800 5.32 0.817 -0.0800 4.25 0.714 -0.0800 3.09 0.588 -0.0800 2.08 0.487 -0.0800 1.09 0.389 -0.0800 0.04 0.289 -0.0800 -0.94 0.207 -0.0800 -1.90 0.115 -0.0800 -3.14 -0.017 -0.0800 -3.99 -0.104 -0.0800 -4.99 -0.203 -0.0800 -6.06 -0.320 -0.0800 Tabulated from data in file CL00801.DAT & reduced using program Q02.00L Average Reynolds #: 300900 Number of angles of attack: 49 alpha / Cl / Cm -6.03 -0.269 -0.0800 -4.29 -0.096 -0.0800 -3.40 -0.013 -0.0800 -2.59 0.065 -0.0800 -1.28 0.177 -0.0800 -0.37 0.263 -0.0800 0.82 0.391 -0.0800 1.48 0.457 -0.0800 2.61 0.573 -0.0800 3.64 0.676 -0.0800 4.75 0.785 -0.0800 5.81 0.885 -0.0800 6.65 0.957 -0.0800 7.78 1.050 -0.0800 8.63 1.115 -0.0800 9.68 1.191 -0.0800 10.69 1.254 -0.0800 11.85 1.296 -0.0800 12.79 1.299 -0.0800 13.68 1.280 -0.0800 14.70 1.251 -0.0800 15.37 1.123 -0.0800 16.68 1.091 -0.0800 17.60 1.082 -0.0800 18.77 1.046 -0.0800 17.20 1.103 -0.0800 16.18 1.083 -0.0800 15.18 1.087 -0.0800 14.71 1.252 -0.0800 13.30 1.287 -0.0800 12.42 1.300 -0.0800 11.35 1.278 -0.0800 10.37 1.231 -0.0800 9.22 1.157 -0.0800 8.22 1.081 -0.0800 7.14 0.997 -0.0800 6.24 0.918 -0.0800 5.16 0.819 -0.0800 4.08 0.715 -0.0800 2.97 0.604 -0.0800 2.06 0.511 -0.0800 1.00 0.402 -0.0800 -0.03 0.287 -0.0800 -1.05 0.196 -0.0800 -2.16 0.100 -0.0800 -3.16 0.005 -0.0800 -4.18 -0.091 -0.0800 -5.08 -0.176 -0.0800 -6.10 -0.278 -0.0800 Tabulated from data in file CL00803.DAT & reduced using program Q02.00L File 7037b.lft created on 09-12-1997 at 13:46:18 using program FORMAT