Airfoil: S7012 (B) Builder: M. Lachowski Comment: clean Number of Reynolds #'s: 5 Average Reynolds #: 61100 Number of angles of attack: 33 alpha / Cl / Cm -5.84 -0.411 -0.0400 -4.31 -0.292 -0.0400 -2.74 -0.151 -0.0400 -1.25 -0.043 -0.0400 0.14 0.114 -0.0400 1.74 0.376 -0.0400 3.49 0.561 -0.0400 4.86 0.684 -0.0400 6.37 0.813 -0.0400 7.89 0.942 -0.0400 9.55 1.034 -0.0400 10.98 1.084 -0.0400 12.60 1.097 -0.0400 13.84 1.036 -0.0400 15.53 0.990 -0.0400 16.91 0.953 -0.0400 18.44 0.997 -0.0400 17.05 0.994 -0.0400 15.60 0.997 -0.0400 14.10 1.032 -0.0400 12.66 1.096 -0.0400 11.06 1.089 -0.0400 9.64 1.047 -0.0400 8.01 0.953 -0.0400 6.60 0.841 -0.0400 4.99 0.698 -0.0400 3.54 0.570 -0.0400 1.88 0.404 -0.0400 0.35 0.142 -0.0400 -1.25 -0.043 -0.0400 -2.61 -0.132 -0.0400 -4.20 -0.276 -0.0400 -5.84 -0.410 -0.0400 Tabulated from data in file AB00093.DAT & reduced using program Q01.00L Average Reynolds #: 102000 Number of angles of attack: 33 alpha / Cl / Cm -5.88 -0.459 -0.0400 -4.40 -0.329 -0.0400 -2.88 -0.192 -0.0400 -1.30 -0.057 -0.0400 0.27 0.177 -0.0400 1.79 0.355 -0.0400 3.32 0.504 -0.0400 4.80 0.651 -0.0400 6.42 0.813 -0.0400 7.97 0.939 -0.0400 9.54 1.030 -0.0400 10.99 1.078 -0.0400 12.54 1.051 -0.0400 13.86 0.973 -0.0400 15.46 0.948 -0.0400 16.92 0.929 -0.0400 18.47 0.929 -0.0400 17.15 0.927 -0.0400 15.57 0.928 -0.0400 14.18 0.968 -0.0400 12.53 1.017 -0.0400 11.09 1.083 -0.0400 9.66 1.031 -0.0400 8.02 0.933 -0.0400 6.55 0.820 -0.0400 5.03 0.664 -0.0400 3.53 0.517 -0.0400 1.92 0.361 -0.0400 0.44 0.198 -0.0400 -1.13 -0.060 -0.0400 -2.68 -0.174 -0.0400 -4.31 -0.320 -0.0400 -5.83 -0.456 -0.0400 Tabulated from data in file AB00091.DAT & reduced using program Q01.00L Average Reynolds #: 152600 Number of angles of attack: 33 alpha / Cl / Cm -5.94 -0.423 -0.0400 -4.16 -0.258 -0.0400 -2.60 -0.117 -0.0400 -1.10 0.040 -0.0400 0.51 0.233 -0.0400 1.96 0.380 -0.0400 3.43 0.537 -0.0400 5.12 0.713 -0.0400 6.67 0.862 -0.0400 8.10 0.969 -0.0400 9.67 1.060 -0.0400 11.18 1.107 -0.0400 12.68 1.062 -0.0400 14.31 0.996 -0.0400 15.61 0.991 -0.0400 17.11 0.990 -0.0400 18.83 0.990 -0.0400 16.73 0.981 -0.0400 15.28 1.006 -0.0400 13.89 0.997 -0.0400 12.35 1.081 -0.0400 10.98 1.099 -0.0400 9.49 1.045 -0.0400 7.92 0.950 -0.0400 6.29 0.820 -0.0400 4.91 0.681 -0.0400 3.34 0.515 -0.0400 1.83 0.357 -0.0400 0.12 0.183 -0.0400 -1.26 0.004 -0.0400 -2.90 -0.152 -0.0400 -4.30 -0.278 -0.0400 -6.09 -0.436 -0.0400 Tabulated from data in file PG00564.DAT & reduced using program Q01.00L Average Reynolds #: 203200 Number of angles of attack: 33 alpha / Cl / Cm -5.90 -0.430 -0.0400 -4.40 -0.292 -0.0400 -2.83 -0.146 -0.0400 -1.35 0.015 -0.0400 0.16 0.169 -0.0400 1.76 0.341 -0.0400 3.34 0.510 -0.0400 4.80 0.663 -0.0400 6.45 0.826 -0.0400 7.98 0.943 -0.0400 9.51 1.038 -0.0400 11.00 1.085 -0.0400 12.51 1.074 -0.0400 14.00 1.003 -0.0400 15.34 0.991 -0.0400 16.89 0.929 -0.0400 18.27 0.917 -0.0400 16.75 0.932 -0.0400 15.50 0.955 -0.0400 13.93 1.001 -0.0400 12.51 1.090 -0.0400 11.14 1.089 -0.0400 9.52 1.036 -0.0400 8.02 0.944 -0.0400 6.45 0.824 -0.0400 4.98 0.680 -0.0400 3.50 0.524 -0.0400 1.96 0.357 -0.0400 0.42 0.196 -0.0400 -1.25 0.024 -0.0400 -2.79 -0.149 -0.0400 -4.21 -0.282 -0.0400 -5.90 -0.434 -0.0400 Tabulated from data in file AB00089.DAT & reduced using program Q01.00L Average Reynolds #: 304700 Number of angles of attack: 33 alpha / Cl / Cm -5.89 -0.440 -0.0400 -4.27 -0.286 -0.0400 -2.70 -0.123 -0.0400 -1.18 0.045 -0.0400 0.24 0.179 -0.0400 1.74 0.347 -0.0400 3.35 0.524 -0.0400 4.89 0.692 -0.0400 6.55 0.856 -0.0400 7.86 0.966 -0.0400 9.61 1.081 -0.0400 11.04 1.137 -0.0400 12.43 1.143 -0.0400 13.80 1.111 -0.0400 15.42 1.003 -0.0400 16.80 0.960 -0.0400 18.36 0.962 -0.0400 16.94 0.953 -0.0400 15.42 0.998 -0.0400 14.04 1.079 -0.0400 12.66 1.135 -0.0400 11.11 1.138 -0.0400 9.53 1.074 -0.0400 8.04 0.976 -0.0400 6.55 0.852 -0.0400 4.85 0.683 -0.0400 3.31 0.516 -0.0400 1.80 0.349 -0.0400 0.32 0.180 -0.0400 -1.33 0.025 -0.0400 -2.95 -0.162 -0.0400 -4.49 -0.314 -0.0400 -6.21 -0.476 -0.0400 Tabulated from data in file AB00087.DAT & reduced using program Q01.00L File s7012b.lft created on 12-05-1997 at 15:25:51 using program FORMAT