Airfoil: SD7037 (A) Builder: H. Michaelis Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 61400 Number of angles of attack: 33 alpha / Cl / Cm -6.81 -0.419 -0.0850 -4.22 -0.234 -0.0850 -3.11 -0.152 -0.0850 -1.76 -0.042 -0.0850 0.01 0.128 -0.0850 1.43 0.329 -0.0850 3.08 0.581 -0.0850 4.55 0.741 -0.0850 6.01 0.869 -0.0850 7.73 1.007 -0.0850 9.11 1.088 -0.0850 10.57 1.154 -0.0850 12.16 1.212 -0.0850 13.72 1.116 -0.0850 15.23 1.012 -0.0850 16.61 1.069 -0.0850 18.22 1.096 -0.0850 16.63 1.081 -0.0850 15.20 1.027 -0.0850 13.81 1.018 -0.0850 12.31 1.196 -0.0850 10.76 1.153 -0.0850 9.29 1.082 -0.0850 7.78 0.997 -0.0850 6.24 0.877 -0.0850 4.66 0.744 -0.0850 3.07 0.584 -0.0850 1.46 0.344 -0.0850 -0.09 0.126 -0.0850 -1.53 -0.013 -0.0850 -3.18 -0.149 -0.0850 -4.57 -0.250 -0.0850 -6.17 -0.368 -0.0850 Tabulated from data in file JG00103.DAT & reduced using program Q01.00L Average Reynolds #: 102000 Number of angles of attack: 33 alpha / Cl / Cm -6.29 -0.402 -0.0850 -4.42 -0.254 -0.0850 -2.84 -0.094 -0.0850 -1.56 0.063 -0.0850 0.22 0.292 -0.0850 1.73 0.481 -0.0850 3.31 0.635 -0.0850 4.76 0.759 -0.0850 6.23 0.887 -0.0850 7.82 1.015 -0.0850 9.27 1.086 -0.0850 10.77 1.162 -0.0850 12.26 1.192 -0.0850 13.70 1.013 -0.0850 15.17 0.962 -0.0850 16.66 0.973 -0.0850 18.42 0.959 -0.0850 16.46 0.991 -0.0850 14.80 0.956 -0.0850 13.47 1.007 -0.0850 12.12 1.178 -0.0850 10.67 1.140 -0.0850 8.90 1.048 -0.0850 7.60 0.979 -0.0850 5.96 0.836 -0.0850 4.44 0.700 -0.0850 2.82 0.557 -0.0850 1.41 0.411 -0.0850 -0.21 0.201 -0.0850 -1.73 0.007 -0.0850 -3.39 -0.189 -0.0850 -4.72 -0.298 -0.0850 -6.39 -0.427 -0.0850 Tabulated from data in file JG00222.DAT & reduced using program Q01.00L Average Reynolds #: 203000 Number of angles of attack: 33 alpha / Cl / Cm -6.29 -0.425 -0.0850 -4.51 -0.186 -0.0850 -2.94 -0.011 -0.0850 -1.31 0.152 -0.0850 0.14 0.294 -0.0850 1.55 0.441 -0.0850 3.20 0.608 -0.0850 4.77 0.755 -0.0850 6.44 0.902 -0.0850 7.84 1.001 -0.0850 9.27 1.088 -0.0850 10.77 1.161 -0.0850 12.31 1.192 -0.0850 13.72 1.041 -0.0850 15.34 0.980 -0.0850 16.68 0.970 -0.0850 18.28 0.964 -0.0850 16.37 0.973 -0.0850 14.76 0.961 -0.0850 13.42 1.093 -0.0850 12.06 1.189 -0.0850 10.58 1.152 -0.0850 8.90 1.061 -0.0850 7.58 0.979 -0.0850 6.00 0.857 -0.0850 4.42 0.713 -0.0850 2.69 0.547 -0.0850 1.36 0.410 -0.0850 -0.36 0.228 -0.0850 -1.90 0.084 -0.0850 -3.32 -0.065 -0.0850 -5.00 -0.262 -0.0850 -6.37 -0.444 -0.0850 Tabulated from data in file AB00224.DAT & reduced using program Q01.00L Average Reynolds #: 304200 Number of angles of attack: 33 alpha / Cl / Cm -6.26 -0.372 -0.0850 -4.64 -0.174 -0.0850 -3.21 -0.034 -0.0850 -1.45 0.127 -0.0850 -0.08 0.267 -0.0850 1.66 0.449 -0.0850 3.27 0.612 -0.0850 5.02 0.779 -0.0850 6.35 0.893 -0.0850 7.96 1.008 -0.0850 9.39 1.104 -0.0850 10.96 1.181 -0.0850 12.36 1.215 -0.0850 13.38 1.152 -0.0850 14.67 1.086 -0.0850 16.58 1.027 -0.0850 17.95 0.978 -0.0850 16.50 1.015 -0.0850 15.08 1.066 -0.0850 13.59 1.169 -0.0850 12.11 1.206 -0.0850 10.59 1.164 -0.0850 8.99 1.076 -0.0850 7.40 0.966 -0.0850 5.87 0.846 -0.0850 4.30 0.705 -0.0850 2.42 0.518 -0.0850 1.28 0.402 -0.0850 -0.41 0.220 -0.0850 -1.75 0.092 -0.0850 -3.41 -0.061 -0.0850 -4.83 -0.199 -0.0850 -6.29 -0.392 -0.0850 Tabulated from data in file AB00226.DAT & reduced using program Q01.00L File sd7037a.lft created on 12-05-1997 at 15:25:52 using program FORMAT