Airfoil: S7012 (B) Builder: M. Lachowski Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 60700 Number of angles of attack: 49 alpha / Cl / Cm -6.02 -0.374 -0.0400 -4.67 -0.266 -0.0400 -3.49 -0.171 -0.0400 -2.51 -0.095 -0.0400 -1.55 -0.024 -0.0400 -0.43 0.078 -0.0400 0.52 0.182 -0.0400 1.54 0.384 -0.0400 2.70 0.523 -0.0400 3.73 0.615 -0.0400 4.57 0.689 -0.0400 5.82 0.796 -0.0400 6.70 0.872 -0.0400 7.74 0.955 -0.0400 8.78 1.027 -0.0400 9.78 1.073 -0.0400 10.76 1.105 -0.0400 11.71 1.122 -0.0400 12.78 1.073 -0.0400 13.68 1.037 -0.0400 14.79 0.983 -0.0400 15.79 1.031 -0.0400 16.76 1.005 -0.0400 17.80 0.995 -0.0400 18.64 1.014 -0.0400 17.28 1.044 -0.0400 16.29 1.010 -0.0400 15.35 1.027 -0.0400 14.41 1.051 -0.0400 13.31 1.066 -0.0400 12.45 1.126 -0.0400 11.41 1.137 -0.0400 10.33 1.102 -0.0400 9.25 1.049 -0.0400 8.34 1.001 -0.0400 7.36 0.934 -0.0400 6.38 0.853 -0.0400 5.22 0.748 -0.0400 4.29 0.664 -0.0400 3.32 0.576 -0.0400 2.18 0.463 -0.0400 1.24 0.313 -0.0400 0.16 0.143 -0.0400 -0.92 0.021 -0.0400 -1.98 -0.053 -0.0400 -2.88 -0.129 -0.0400 -4.01 -0.208 -0.0400 -4.97 -0.286 -0.0400 -6.05 -0.384 -0.0400 Tabulated from data in file CL00824.DAT & reduced using program Q02.00L Average Reynolds #: 100600 Number of angles of attack: 49 alpha / Cl / Cm -6.05 -0.424 -0.0400 -4.39 -0.258 -0.0400 -3.43 -0.176 -0.0400 -2.50 -0.098 -0.0400 -1.50 -0.020 -0.0400 -0.38 0.110 -0.0400 0.53 0.259 -0.0400 1.63 0.385 -0.0400 2.77 0.493 -0.0400 3.59 0.569 -0.0400 4.71 0.675 -0.0400 5.64 0.760 -0.0400 6.65 0.850 -0.0400 7.67 0.939 -0.0400 8.66 0.995 -0.0400 9.88 1.054 -0.0400 10.73 1.080 -0.0400 11.76 1.065 -0.0400 12.80 1.019 -0.0400 13.92 0.970 -0.0400 14.73 0.971 -0.0400 15.91 0.957 -0.0400 16.88 0.957 -0.0400 17.83 0.928 -0.0400 18.69 0.964 -0.0400 17.22 0.956 -0.0400 16.36 0.957 -0.0400 15.35 0.976 -0.0400 14.36 0.969 -0.0400 13.41 0.980 -0.0400 12.25 1.045 -0.0400 11.30 1.087 -0.0400 10.28 1.063 -0.0400 9.25 1.018 -0.0400 8.19 0.960 -0.0400 7.39 0.908 -0.0400 6.25 0.795 -0.0400 5.16 0.687 -0.0400 4.29 0.601 -0.0400 3.19 0.498 -0.0400 2.11 0.398 -0.0400 1.00 0.290 -0.0400 0.16 0.181 -0.0400 -0.98 -0.010 -0.0400 -2.06 -0.081 -0.0400 -2.93 -0.149 -0.0400 -4.07 -0.248 -0.0400 -4.99 -0.323 -0.0400 -6.19 -0.427 -0.0400 Tabulated from data in file CL00837.DAT & reduced using program Q02.00L Average Reynolds #: 201000 Number of angles of attack: 49 alpha / Cl / Cm -6.09 -0.417 -0.0400 -4.33 -0.251 -0.0400 -3.39 -0.165 -0.0400 -2.38 -0.063 -0.0400 -1.36 0.049 -0.0400 -0.39 0.146 -0.0400 0.73 0.262 -0.0400 1.72 0.362 -0.0400 2.55 0.450 -0.0400 3.70 0.571 -0.0400 4.63 0.666 -0.0400 5.82 0.785 -0.0400 6.77 0.874 -0.0400 7.68 0.945 -0.0400 8.83 1.024 -0.0400 9.69 1.064 -0.0400 10.75 1.088 -0.0400 11.76 1.121 -0.0400 12.93 1.090 -0.0400 13.65 1.057 -0.0400 14.82 0.994 -0.0400 15.61 1.001 -0.0400 16.83 0.973 -0.0400 17.80 0.973 -0.0400 18.67 0.935 -0.0400 17.26 0.954 -0.0400 16.17 0.984 -0.0400 15.35 0.991 -0.0400 14.22 1.038 -0.0400 13.10 1.059 -0.0400 12.27 1.121 -0.0400 11.22 1.092 -0.0400 10.36 1.079 -0.0400 9.29 1.041 -0.0400 8.16 0.966 -0.0400 7.27 0.900 -0.0400 6.33 0.815 -0.0400 5.11 0.694 -0.0400 4.17 0.599 -0.0400 3.23 0.500 -0.0400 1.97 0.369 -0.0400 0.99 0.268 -0.0400 0.01 0.164 -0.0400 -1.00 0.070 -0.0400 -2.07 -0.042 -0.0400 -3.04 -0.139 -0.0400 -4.13 -0.243 -0.0400 -5.19 -0.342 -0.0400 -6.02 -0.414 -0.0400 Tabulated from data in file CF00839.DAT & reduced using program Q02.00L Average Reynolds #: 301400 Number of angles of attack: 49 alpha / Cl / Cm -5.61 -0.378 -0.0400 -4.56 -0.275 -0.0400 -3.39 -0.152 -0.0400 -2.55 -0.064 -0.0400 -1.19 0.068 -0.0400 -0.35 0.141 -0.0400 0.72 0.248 -0.0400 1.78 0.364 -0.0400 2.54 0.448 -0.0400 3.81 0.581 -0.0400 4.74 0.679 -0.0400 5.85 0.791 -0.0400 6.83 0.881 -0.0400 7.77 0.960 -0.0400 8.78 1.036 -0.0400 9.80 1.091 -0.0400 10.74 1.115 -0.0400 11.83 1.148 -0.0400 12.53 1.151 -0.0400 13.75 1.121 -0.0400 14.73 1.104 -0.0400 15.74 1.008 -0.0400 16.67 0.989 -0.0400 17.68 0.985 -0.0400 18.78 0.969 -0.0400 16.98 0.990 -0.0400 16.23 1.003 -0.0400 15.10 1.079 -0.0400 14.22 1.090 -0.0400 13.24 1.149 -0.0400 12.09 1.136 -0.0400 11.39 1.127 -0.0400 10.32 1.102 -0.0400 9.28 1.060 -0.0400 8.29 0.993 -0.0400 7.37 0.921 -0.0400 6.06 0.804 -0.0400 5.31 0.732 -0.0400 4.22 0.619 -0.0400 3.10 0.499 -0.0400 1.97 0.376 -0.0400 1.05 0.275 -0.0400 0.09 0.172 -0.0400 -1.06 0.070 -0.0400 -2.08 -0.022 -0.0400 -3.12 -0.132 -0.0400 -4.16 -0.237 -0.0400 -5.12 -0.332 -0.0400 -6.21 -0.431 -0.0400 Tabulated from data in file CF00841.DAT & reduced using program Q02.00L File s7012b.lft created on 09-12-1997 at 13:46:18 using program FORMAT