Airfoil: MH32 Builder: J. Tonnesen Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 60100 Number of angles of attack: 49 alpha / Cl / Cm -5.85 -0.350 -0.0580 -4.55 -0.255 -0.0580 -3.51 -0.184 -0.0580 -2.60 -0.113 -0.0580 -1.58 -0.038 -0.0580 -0.52 0.069 -0.0580 0.49 0.154 -0.0580 1.50 0.320 -0.0580 2.49 0.473 -0.0580 3.68 0.625 -0.0580 4.56 0.705 -0.0580 5.63 0.793 -0.0580 6.73 0.883 -0.0580 7.62 0.952 -0.0580 8.72 1.020 -0.0580 9.79 1.081 -0.0580 10.84 1.124 -0.0580 11.86 1.153 -0.0580 12.78 1.038 -0.0580 13.77 0.957 -0.0580 14.66 0.957 -0.0580 15.68 0.947 -0.0580 16.73 0.945 -0.0580 17.74 0.972 -0.0580 18.80 0.967 -0.0580 17.41 0.969 -0.0580 16.33 0.953 -0.0580 15.29 0.957 -0.0580 14.27 0.956 -0.0580 13.33 0.998 -0.0580 12.36 1.137 -0.0580 11.29 1.132 -0.0580 10.30 1.092 -0.0580 9.31 1.040 -0.0580 8.29 0.978 -0.0580 7.23 0.907 -0.0580 6.21 0.823 -0.0580 5.35 0.746 -0.0580 4.23 0.653 -0.0580 3.20 0.547 -0.0580 2.15 0.399 -0.0580 1.27 0.244 -0.0580 0.14 0.101 -0.0580 -0.93 0.002 -0.0580 -1.96 -0.091 -0.0580 -2.98 -0.167 -0.0580 -3.88 -0.233 -0.0580 -4.95 -0.304 -0.0580 -5.91 -0.369 -0.0580 Tabulated from data in file JG00631.DAT & reduced using program Q02.00L Average Reynolds #: 100400 Number of angles of attack: 49 alpha / Cl / Cm -5.86 -0.372 -0.0580 -4.62 -0.276 -0.0580 -3.61 -0.202 -0.0580 -2.59 -0.116 -0.0580 -1.59 -0.027 -0.0580 -0.58 0.081 -0.0580 0.61 0.270 -0.0580 1.49 0.389 -0.0580 2.70 0.530 -0.0580 3.59 0.610 -0.0580 4.63 0.704 -0.0580 5.70 0.797 -0.0580 6.77 0.887 -0.0580 7.65 0.962 -0.0580 8.74 1.031 -0.0580 9.79 1.084 -0.0580 10.78 1.130 -0.0580 11.76 1.160 -0.0580 12.64 1.145 -0.0580 13.70 0.999 -0.0580 14.68 1.009 -0.0580 15.69 0.986 -0.0580 16.64 0.957 -0.0580 17.70 0.949 -0.0580 18.75 0.946 -0.0580 17.28 0.955 -0.0580 16.34 0.970 -0.0580 15.39 1.020 -0.0580 14.32 0.989 -0.0580 13.32 0.999 -0.0580 12.38 1.154 -0.0580 11.31 1.137 -0.0580 10.42 1.104 -0.0580 9.26 1.046 -0.0580 8.42 1.000 -0.0580 7.21 0.909 -0.0580 6.38 0.836 -0.0580 5.29 0.744 -0.0580 4.24 0.647 -0.0580 3.20 0.554 -0.0580 2.19 0.453 -0.0580 1.11 0.315 -0.0580 0.03 0.164 -0.0580 -0.97 0.013 -0.0580 -2.02 -0.080 -0.0580 -2.86 -0.158 -0.0580 -3.96 -0.244 -0.0580 -5.02 -0.316 -0.0580 -5.92 -0.391 -0.0580 Tabulated from data in file CL00633.DAT & reduced using program Q02.00L Average Reynolds #: 200700 Number of angles of attack: 49 alpha / Cl / Cm -5.95 -0.397 -0.0580 -4.54 -0.266 -0.0580 -3.51 -0.158 -0.0580 -2.61 -0.033 -0.0580 -1.45 0.102 -0.0580 -0.52 0.192 -0.0580 0.47 0.299 -0.0580 1.50 0.399 -0.0580 2.51 0.500 -0.0580 3.62 0.611 -0.0580 4.64 0.709 -0.0580 5.70 0.805 -0.0580 6.73 0.894 -0.0580 7.74 0.974 -0.0580 8.74 1.041 -0.0580 9.74 1.096 -0.0580 10.69 1.142 -0.0580 11.82 1.176 -0.0580 12.74 1.177 -0.0580 13.33 1.095 -0.0580 14.85 1.102 -0.0580 15.65 1.092 -0.0580 16.62 1.046 -0.0580 17.73 0.989 -0.0580 18.71 0.938 -0.0580 17.28 1.001 -0.0580 16.23 1.019 -0.0580 15.38 1.084 -0.0580 14.42 1.099 -0.0580 13.46 1.121 -0.0580 12.43 1.177 -0.0580 11.35 1.158 -0.0580 10.35 1.119 -0.0580 9.40 1.070 -0.0580 8.41 1.009 -0.0580 7.32 0.932 -0.0580 6.38 0.855 -0.0580 5.20 0.751 -0.0580 4.35 0.671 -0.0580 3.30 0.567 -0.0580 2.23 0.460 -0.0580 1.12 0.351 -0.0580 0.19 0.257 -0.0580 -0.79 0.157 -0.0580 -1.95 0.042 -0.0580 -2.96 -0.087 -0.0580 -3.96 -0.221 -0.0580 -4.98 -0.309 -0.0580 -5.98 -0.400 -0.0580 Tabulated from data in file CL00635.DAT & reduced using program Q02.00L Average Reynolds #: 301100 Number of angles of attack: 49 alpha / Cl / Cm -5.94 -0.389 -0.0580 -4.59 -0.217 -0.0580 -3.59 -0.104 -0.0580 -2.69 -0.008 -0.0580 -1.59 0.094 -0.0580 -0.54 0.187 -0.0580 0.57 0.305 -0.0580 1.54 0.405 -0.0580 2.60 0.517 -0.0580 3.66 0.624 -0.0580 4.70 0.724 -0.0580 5.69 0.815 -0.0580 6.64 0.899 -0.0580 7.85 0.995 -0.0580 8.76 1.060 -0.0580 9.74 1.120 -0.0580 10.83 1.173 -0.0580 11.68 1.199 -0.0580 12.77 1.207 -0.0580 13.72 1.205 -0.0580 14.32 1.151 -0.0580 15.56 1.112 -0.0580 16.56 1.088 -0.0580 17.53 0.994 -0.0580 18.53 0.960 -0.0580 17.42 1.007 -0.0580 16.38 1.083 -0.0580 15.38 1.122 -0.0580 14.49 1.161 -0.0580 13.50 1.180 -0.0580 12.38 1.203 -0.0580 11.38 1.186 -0.0580 10.30 1.143 -0.0580 9.34 1.089 -0.0580 8.33 1.022 -0.0580 7.29 0.944 -0.0580 6.35 0.865 -0.0580 5.33 0.773 -0.0580 4.22 0.664 -0.0580 3.25 0.571 -0.0580 2.24 0.469 -0.0580 1.06 0.347 -0.0580 0.19 0.257 -0.0580 -0.99 0.140 -0.0580 -2.02 0.053 -0.0580 -2.99 -0.043 -0.0580 -4.09 -0.163 -0.0580 -5.03 -0.269 -0.0580 -5.98 -0.391 -0.0580 Tabulated from data in file CL00637.DAT & reduced using program Q02.00L File mh32.lft created on 09-12-1997 at 13:46:18 using program FORMAT