Airfoil: MB253515 Builder: M. Bame Comment: clean Number of Reynolds #'s: 5 Average Reynolds #: 20100 Number of angles of attack: 97 alpha / Cl / Cm -6.18 -0.599 -0.0500 -5.33 -0.464 -0.0500 -5.01 -0.435 -0.0500 -4.38 -0.319 -0.0500 -3.85 -0.244 -0.0500 -3.24 -0.217 -0.0500 -2.90 -0.186 -0.0500 -2.27 -0.167 -0.0500 -1.84 -0.153 -0.0500 -1.25 -0.112 -0.0500 -0.81 -0.108 -0.0500 -0.24 -0.031 -0.0500 0.26 -0.006 -0.0500 0.67 -0.005 -0.0500 1.12 0.007 -0.0500 1.76 0.071 -0.0500 2.18 0.132 -0.0500 2.81 0.167 -0.0500 3.25 0.184 -0.0500 3.84 0.222 -0.0500 4.27 0.278 -0.0500 4.91 0.296 -0.0500 5.19 0.352 -0.0500 5.86 0.334 -0.0500 6.24 0.354 -0.0500 6.92 0.415 -0.0500 7.34 0.419 -0.0500 7.99 0.440 -0.0500 8.28 0.499 -0.0500 8.87 0.494 -0.0500 9.36 0.561 -0.0500 9.99 0.533 -0.0500 10.22 0.541 -0.0500 10.98 0.570 -0.0500 11.28 0.626 -0.0500 11.80 0.603 -0.0500 12.30 0.657 -0.0500 12.99 0.645 -0.0500 13.36 0.646 -0.0500 13.92 0.712 -0.0500 14.33 0.722 -0.0500 14.88 0.716 -0.0500 15.31 0.718 -0.0500 15.86 0.778 -0.0500 16.32 0.823 -0.0500 17.01 0.849 -0.0500 17.41 0.840 -0.0500 17.95 0.851 -0.0500 18.40 0.868 -0.0500 17.82 0.857 -0.0500 17.32 0.784 -0.0500 16.80 0.741 -0.0500 16.31 0.704 -0.0500 15.74 0.662 -0.0500 15.27 0.635 -0.0500 14.73 0.615 -0.0500 14.27 0.611 -0.0500 13.76 0.608 -0.0500 13.22 0.586 -0.0500 12.74 0.560 -0.0500 12.21 0.533 -0.0500 11.72 0.521 -0.0500 11.19 0.503 -0.0500 10.70 0.517 -0.0500 10.16 0.468 -0.0500 9.63 0.446 -0.0500 9.19 0.429 -0.0500 8.70 0.398 -0.0500 8.13 0.347 -0.0500 7.64 0.333 -0.0500 7.17 0.316 -0.0500 6.66 0.291 -0.0500 6.17 0.235 -0.0500 5.58 0.201 -0.0500 5.11 0.153 -0.0500 4.66 0.185 -0.0500 4.10 0.128 -0.0500 3.57 0.111 -0.0500 3.09 0.063 -0.0500 2.51 0.025 -0.0500 2.03 -0.016 -0.0500 1.58 -0.047 -0.0500 1.03 -0.097 -0.0500 0.51 -0.130 -0.0500 0.00 -0.162 -0.0500 -0.52 -0.193 -0.0500 -1.01 -0.219 -0.0500 -1.54 -0.232 -0.0500 -2.02 -0.251 -0.0500 -2.48 -0.263 -0.0500 -2.98 -0.296 -0.0500 -3.55 -0.318 -0.0500 -4.05 -0.344 -0.0500 -4.52 -0.371 -0.0500 -5.11 -0.509 -0.0500 -5.61 -0.532 -0.0500 -6.17 -0.612 -0.0500 Tabulated from data in file MS00367.DAT & reduced using program Q01.00L Average Reynolds #: 41600 Number of angles of attack: 97 alpha / Cl / Cm -6.16 -0.473 -0.0500 -5.41 -0.442 -0.0500 -4.93 -0.412 -0.0500 -4.36 -0.370 -0.0500 -3.82 -0.292 -0.0500 -3.42 -0.258 -0.0500 -2.81 -0.207 -0.0500 -2.39 -0.171 -0.0500 -1.84 -0.118 -0.0500 -1.43 -0.113 -0.0500 -0.94 -0.074 -0.0500 -0.31 -0.036 -0.0500 0.19 0.020 -0.0500 0.63 0.053 -0.0500 1.28 0.097 -0.0500 1.68 0.121 -0.0500 2.23 0.157 -0.0500 2.82 0.204 -0.0500 3.16 0.212 -0.0500 3.78 0.239 -0.0500 4.30 0.270 -0.0500 4.88 0.303 -0.0500 5.29 0.328 -0.0500 5.93 0.370 -0.0500 6.18 0.385 -0.0500 6.80 0.384 -0.0500 7.20 0.388 -0.0500 7.85 0.421 -0.0500 8.29 0.435 -0.0500 8.92 0.460 -0.0500 9.31 0.474 -0.0500 9.91 0.501 -0.0500 10.30 0.495 -0.0500 10.84 0.538 -0.0500 11.26 0.545 -0.0500 11.75 0.562 -0.0500 12.36 0.712 -0.0500 12.93 0.809 -0.0500 13.32 0.843 -0.0500 14.12 1.136 -0.0500 14.49 1.104 -0.0500 15.07 1.093 -0.0500 15.48 1.070 -0.0500 16.05 1.109 -0.0500 16.47 1.125 -0.0500 17.01 1.123 -0.0500 17.43 1.107 -0.0500 17.95 1.095 -0.0500 18.46 1.129 -0.0500 17.82 0.936 -0.0500 17.33 0.955 -0.0500 16.82 1.050 -0.0500 16.37 1.076 -0.0500 15.88 1.070 -0.0500 15.32 1.048 -0.0500 14.80 1.060 -0.0500 14.35 1.072 -0.0500 13.88 1.093 -0.0500 13.34 1.091 -0.0500 12.83 1.101 -0.0500 12.38 1.085 -0.0500 11.81 1.082 -0.0500 11.35 1.064 -0.0500 10.84 1.020 -0.0500 10.21 0.529 -0.0500 9.69 0.456 -0.0500 9.17 0.432 -0.0500 8.60 0.421 -0.0500 8.18 0.409 -0.0500 7.70 0.382 -0.0500 7.21 0.365 -0.0500 6.68 0.344 -0.0500 6.17 0.322 -0.0500 5.60 0.307 -0.0500 5.10 0.286 -0.0500 4.59 0.259 -0.0500 4.14 0.232 -0.0500 3.58 0.212 -0.0500 3.11 0.187 -0.0500 2.65 0.158 -0.0500 2.11 0.129 -0.0500 1.54 0.085 -0.0500 1.06 0.038 -0.0500 0.54 0.007 -0.0500 0.14 -0.029 -0.0500 -0.47 -0.085 -0.0500 -1.01 -0.130 -0.0500 -1.46 -0.155 -0.0500 -1.94 -0.178 -0.0500 -2.47 -0.238 -0.0500 -2.95 -0.275 -0.0500 -3.54 -0.331 -0.0500 -4.07 -0.396 -0.0500 -4.56 -0.427 -0.0500 -5.02 -0.452 -0.0500 -5.56 -0.469 -0.0500 -6.08 -0.496 -0.0500 Tabulated from data in file MS00366.DAT & reduced using program Q01.00L Average Reynolds #: 61400 Number of angles of attack: 97 alpha / Cl / Cm -6.15 -0.488 -0.0500 -5.50 -0.417 -0.0500 -4.88 -0.356 -0.0500 -4.40 -0.324 -0.0500 -3.99 -0.285 -0.0500 -3.45 -0.252 -0.0500 -2.95 -0.224 -0.0500 -2.38 -0.130 -0.0500 -1.90 -0.023 -0.0500 -1.36 0.038 -0.0500 -0.94 0.053 -0.0500 -0.39 0.036 -0.0500 0.09 0.056 -0.0500 0.69 0.100 -0.0500 1.23 0.139 -0.0500 1.78 0.181 -0.0500 2.16 0.211 -0.0500 2.71 0.219 -0.0500 3.21 0.244 -0.0500 3.76 0.289 -0.0500 4.18 0.328 -0.0500 4.75 0.370 -0.0500 5.22 0.390 -0.0500 5.83 0.407 -0.0500 6.17 0.423 -0.0500 6.93 0.447 -0.0500 7.25 0.446 -0.0500 7.78 0.461 -0.0500 8.22 0.492 -0.0500 8.94 0.514 -0.0500 9.31 0.520 -0.0500 9.81 0.545 -0.0500 10.22 0.563 -0.0500 10.82 0.613 -0.0500 11.33 0.647 -0.0500 11.80 0.679 -0.0500 12.33 0.740 -0.0500 13.03 1.035 -0.0500 13.37 1.042 -0.0500 13.97 1.052 -0.0500 14.34 1.060 -0.0500 14.89 1.064 -0.0500 15.41 1.071 -0.0500 16.03 1.072 -0.0500 16.37 1.074 -0.0500 16.96 1.055 -0.0500 17.32 1.030 -0.0500 17.86 1.000 -0.0500 18.34 1.008 -0.0500 17.86 0.980 -0.0500 17.35 1.055 -0.0500 16.88 1.048 -0.0500 16.35 1.059 -0.0500 15.82 1.058 -0.0500 15.31 1.055 -0.0500 14.86 1.057 -0.0500 14.35 1.047 -0.0500 13.87 1.040 -0.0500 13.35 1.033 -0.0500 12.89 1.039 -0.0500 12.34 1.057 -0.0500 11.85 1.076 -0.0500 11.36 1.091 -0.0500 10.85 1.090 -0.0500 10.33 1.082 -0.0500 9.86 1.049 -0.0500 9.18 0.511 -0.0500 8.67 0.495 -0.0500 8.18 0.483 -0.0500 7.64 0.458 -0.0500 7.22 0.460 -0.0500 6.70 0.432 -0.0500 6.15 0.428 -0.0500 5.71 0.422 -0.0500 5.22 0.391 -0.0500 4.67 0.363 -0.0500 4.19 0.318 -0.0500 3.62 0.280 -0.0500 3.17 0.258 -0.0500 2.64 0.244 -0.0500 2.17 0.204 -0.0500 1.61 0.177 -0.0500 1.13 0.136 -0.0500 0.59 0.101 -0.0500 0.12 0.055 -0.0500 -0.39 0.044 -0.0500 -0.93 0.056 -0.0500 -1.42 0.034 -0.0500 -1.97 -0.045 -0.0500 -2.44 -0.151 -0.0500 -3.02 -0.240 -0.0500 -3.55 -0.259 -0.0500 -3.97 -0.280 -0.0500 -4.54 -0.337 -0.0500 -5.04 -0.380 -0.0500 -5.59 -0.437 -0.0500 -6.09 -0.484 -0.0500 Tabulated from data in file MS00365.DAT & reduced using program Q01.00L Average Reynolds #: 81600 Number of angles of attack: 97 alpha / Cl / Cm -5.84 -0.387 -0.0500 -5.32 -0.340 -0.0500 -4.70 -0.292 -0.0500 -4.37 -0.267 -0.0500 -3.81 -0.229 -0.0500 -3.37 -0.189 -0.0500 -2.83 -0.158 -0.0500 -2.19 -0.073 -0.0500 -1.90 -0.039 -0.0500 -1.25 0.071 -0.0500 -0.86 0.125 -0.0500 -0.15 0.128 -0.0500 0.17 0.143 -0.0500 0.81 0.159 -0.0500 1.32 0.184 -0.0500 1.72 0.200 -0.0500 2.15 0.219 -0.0500 2.79 0.247 -0.0500 3.17 0.269 -0.0500 3.84 0.306 -0.0500 4.29 0.330 -0.0500 4.91 0.364 -0.0500 5.19 0.395 -0.0500 5.84 0.400 -0.0500 6.31 0.464 -0.0500 7.00 0.488 -0.0500 7.24 0.471 -0.0500 7.87 0.509 -0.0500 8.37 0.522 -0.0500 9.04 0.549 -0.0500 9.27 0.558 -0.0500 9.87 0.570 -0.0500 10.30 0.620 -0.0500 10.97 1.070 -0.0500 11.43 1.053 -0.0500 11.88 1.039 -0.0500 12.35 1.027 -0.0500 13.01 1.023 -0.0500 13.39 1.026 -0.0500 14.08 1.040 -0.0500 14.43 1.033 -0.0500 14.92 1.040 -0.0500 15.35 1.038 -0.0500 16.05 1.036 -0.0500 16.40 1.037 -0.0500 16.89 1.036 -0.0500 17.38 1.023 -0.0500 18.05 1.025 -0.0500 18.44 0.968 -0.0500 17.84 1.030 -0.0500 17.36 1.028 -0.0500 16.86 1.029 -0.0500 16.31 1.035 -0.0500 15.90 1.038 -0.0500 15.34 1.038 -0.0500 14.89 1.034 -0.0500 14.36 1.028 -0.0500 13.86 1.025 -0.0500 13.32 1.018 -0.0500 12.86 1.014 -0.0500 12.31 1.020 -0.0500 11.88 1.027 -0.0500 11.35 1.046 -0.0500 10.85 1.063 -0.0500 10.34 1.072 -0.0500 9.83 1.064 -0.0500 9.35 1.020 -0.0500 8.79 0.971 -0.0500 8.35 0.934 -0.0500 7.80 0.884 -0.0500 7.21 0.456 -0.0500 6.69 0.457 -0.0500 6.23 0.420 -0.0500 5.60 0.406 -0.0500 5.16 0.368 -0.0500 4.67 0.348 -0.0500 4.15 0.323 -0.0500 3.59 0.269 -0.0500 3.11 0.252 -0.0500 2.66 0.233 -0.0500 2.16 0.209 -0.0500 1.61 0.192 -0.0500 1.06 0.175 -0.0500 0.62 0.161 -0.0500 0.11 0.133 -0.0500 -0.41 0.137 -0.0500 -0.90 0.106 -0.0500 -1.43 0.035 -0.0500 -1.96 -0.047 -0.0500 -2.44 -0.100 -0.0500 -2.97 -0.144 -0.0500 -3.49 -0.196 -0.0500 -4.00 -0.254 -0.0500 -4.50 -0.281 -0.0500 -4.98 -0.313 -0.0500 -5.52 -0.359 -0.0500 -6.10 -0.426 -0.0500 Tabulated from data in file MS00368.DAT & reduced using program Q01.00L Average Reynolds #: 101400 Number of angles of attack: 97 alpha / Cl / Cm -6.18 -0.373 -0.0500 -5.20 -0.271 -0.0500 -4.95 -0.255 -0.0500 -4.21 -0.216 -0.0500 -3.79 -0.191 -0.0500 -3.26 -0.104 -0.0500 -2.87 -0.085 -0.0500 -2.31 -0.063 -0.0500 -1.75 -0.020 -0.0500 -1.25 0.049 -0.0500 -0.67 0.174 -0.0500 -0.11 0.286 -0.0500 0.23 0.343 -0.0500 0.79 0.364 -0.0500 1.25 0.370 -0.0500 1.93 0.373 -0.0500 2.20 0.380 -0.0500 2.91 0.424 -0.0500 3.19 0.471 -0.0500 3.94 0.545 -0.0500 4.20 0.589 -0.0500 4.92 0.670 -0.0500 5.28 0.712 -0.0500 6.01 0.781 -0.0500 6.30 0.809 -0.0500 7.03 0.878 -0.0500 7.37 0.908 -0.0500 8.08 0.969 -0.0500 8.39 0.994 -0.0500 9.06 1.050 -0.0500 9.42 1.090 -0.0500 10.09 1.083 -0.0500 10.42 1.081 -0.0500 10.98 1.059 -0.0500 11.50 1.044 -0.0500 12.11 1.031 -0.0500 12.38 1.027 -0.0500 12.95 1.029 -0.0500 13.42 1.035 -0.0500 14.00 1.038 -0.0500 14.47 1.043 -0.0500 15.05 1.053 -0.0500 15.50 1.056 -0.0500 16.11 1.053 -0.0500 16.38 1.049 -0.0500 16.93 1.037 -0.0500 17.44 1.023 -0.0500 18.03 1.010 -0.0500 18.36 0.972 -0.0500 17.70 1.015 -0.0500 17.31 1.020 -0.0500 16.81 1.018 -0.0500 16.38 1.036 -0.0500 15.85 1.035 -0.0500 15.34 1.036 -0.0500 14.80 1.029 -0.0500 14.35 1.025 -0.0500 13.83 1.020 -0.0500 13.37 1.013 -0.0500 12.89 1.005 -0.0500 12.33 1.003 -0.0500 11.81 1.011 -0.0500 11.36 1.025 -0.0500 10.80 1.050 -0.0500 10.36 1.060 -0.0500 9.81 1.071 -0.0500 9.32 1.057 -0.0500 8.82 1.005 -0.0500 8.35 0.963 -0.0500 7.81 0.921 -0.0500 7.35 0.881 -0.0500 6.77 0.827 -0.0500 6.24 0.778 -0.0500 5.66 0.716 -0.0500 5.24 0.669 -0.0500 4.68 0.605 -0.0500 4.26 0.563 -0.0500 3.71 0.484 -0.0500 3.15 0.428 -0.0500 2.62 0.388 -0.0500 2.20 0.369 -0.0500 1.68 0.365 -0.0500 1.15 0.349 -0.0500 0.64 0.328 -0.0500 0.10 0.303 -0.0500 -0.43 0.200 -0.0500 -0.90 0.116 -0.0500 -1.39 0.018 -0.0500 -1.95 -0.053 -0.0500 -2.45 -0.086 -0.0500 -2.95 -0.094 -0.0500 -3.48 -0.133 -0.0500 -4.00 -0.209 -0.0500 -4.50 -0.232 -0.0500 -5.01 -0.262 -0.0500 -5.49 -0.289 -0.0500 -6.14 -0.357 -0.0500 Tabulated from data in file MS00369.DAT & reduced using program Q01.00L File mb253515.lft created on 12-05-1997 at 15:25:50 using program FORMAT