Airfoil: FX 63-137 (B) Builder: M. Allen Comment: clean Number of Reynolds #'s: 8 Average Reynolds #: 61500 Number of angles of attack: 53 alpha / Cl / Cm -6.11 -0.394 -0.1700 -4.63 -0.107 -0.1700 -3.60 0.049 -0.1700 -2.65 0.165 -0.1700 -1.67 0.272 -0.1700 -0.49 0.342 -0.1700 0.42 0.389 -0.1700 1.34 0.443 -0.1700 2.49 0.501 -0.1700 3.40 0.551 -0.1700 4.41 0.645 -0.1700 5.58 0.693 -0.1700 6.61 0.741 -0.1700 7.56 0.768 -0.1700 8.58 0.821 -0.1700 9.59 0.850 -0.1700 10.56 0.870 -0.1700 11.49 0.894 -0.1700 12.65 0.901 -0.1700 13.60 0.918 -0.1700 14.54 0.970 -0.1700 15.69 0.992 -0.1700 16.52 1.022 -0.1700 17.53 1.105 -0.1700 18.57 1.163 -0.1700 19.59 1.187 -0.1700 20.58 1.216 -0.1700 19.46 1.141 -0.1700 18.32 1.126 -0.1700 17.43 1.075 -0.1700 16.37 1.008 -0.1700 15.28 0.988 -0.1700 14.31 0.953 -0.1700 13.38 0.896 -0.1700 12.26 0.877 -0.1700 11.37 0.881 -0.1700 10.31 0.864 -0.1700 9.27 0.797 -0.1700 8.26 0.780 -0.1700 7.32 0.740 -0.1700 6.24 0.682 -0.1700 5.34 0.659 -0.1700 4.31 0.603 -0.1700 3.25 0.504 -0.1700 2.23 0.462 -0.1700 1.19 0.404 -0.1700 0.11 0.333 -0.1700 -0.87 0.279 -0.1700 -1.92 0.212 -0.1700 -2.95 0.100 -0.1700 -3.96 -0.028 -0.1700 -5.02 -0.206 -0.1700 -6.02 -0.433 -0.1700 Tabulated from data in file AB00504.DAT & reduced using program Q01.00L Average Reynolds #: 80400 Number of angles of attack: 65 alpha / Cl / Cm -8.04 -0.336 -0.1700 -6.99 -0.330 -0.1700 -6.06 -0.312 -0.1700 -5.03 -0.025 -0.1700 -4.00 0.123 -0.1700 -2.86 0.256 -0.1700 -1.79 0.345 -0.1700 -0.78 0.448 -0.1700 0.19 0.458 -0.1700 1.12 0.523 -0.1700 2.20 0.559 -0.1700 3.29 0.612 -0.1700 4.29 0.688 -0.1700 5.33 0.754 -0.1700 6.31 0.781 -0.1700 7.30 0.826 -0.1700 8.36 0.879 -0.1700 9.33 0.922 -0.1700 10.34 0.963 -0.1700 11.41 1.018 -0.1700 12.43 1.502 -0.1700 13.48 1.667 -0.1700 14.48 1.667 -0.1700 15.45 1.647 -0.1700 16.32 1.270 -0.1700 17.38 1.175 -0.1700 18.31 1.198 -0.1700 19.43 1.261 -0.1700 20.49 1.270 -0.1700 21.37 1.247 -0.1700 22.36 1.292 -0.1700 23.37 1.327 -0.1700 24.47 1.365 -0.1700 23.54 1.345 -0.1700 22.62 1.288 -0.1700 21.56 1.214 -0.1700 20.56 1.226 -0.1700 19.53 1.221 -0.1700 18.53 1.226 -0.1700 17.52 1.196 -0.1700 16.53 1.189 -0.1700 15.64 1.655 -0.1700 14.66 1.669 -0.1700 13.66 1.664 -0.1700 12.60 1.646 -0.1700 11.71 1.617 -0.1700 10.62 1.570 -0.1700 9.55 1.491 -0.1700 8.57 1.402 -0.1700 7.44 0.841 -0.1700 6.36 0.772 -0.1700 5.44 0.743 -0.1700 4.38 0.678 -0.1700 3.40 0.605 -0.1700 2.38 0.566 -0.1700 1.39 0.512 -0.1700 0.35 0.452 -0.1700 -0.67 0.410 -0.1700 -1.64 0.359 -0.1700 -2.69 0.249 -0.1700 -3.74 0.140 -0.1700 -4.76 -0.004 -0.1700 -5.83 -0.307 -0.1700 -6.85 -0.352 -0.1700 -7.89 -0.334 -0.1700 Tabulated from data in file MS00297.DAT & reduced using program Q01.00L Average Reynolds #: 89800 Number of angles of attack: 65 alpha / Cl / Cm -7.76 -0.317 -0.1700 -6.95 -0.338 -0.1700 -5.96 -0.286 -0.1700 -4.87 0.014 -0.1700 -3.93 0.159 -0.1700 -2.81 0.287 -0.1700 -1.79 0.364 -0.1700 -0.87 0.422 -0.1700 0.23 0.485 -0.1700 1.20 0.547 -0.1700 2.22 0.601 -0.1700 3.19 0.629 -0.1700 4.25 0.707 -0.1700 5.26 0.782 -0.1700 6.26 0.837 -0.1700 7.40 1.357 -0.1700 8.40 1.443 -0.1700 9.44 1.521 -0.1700 10.50 1.590 -0.1700 11.52 1.638 -0.1700 12.47 1.657 -0.1700 13.50 1.676 -0.1700 14.49 1.675 -0.1700 15.49 1.666 -0.1700 16.51 1.647 -0.1700 17.29 1.176 -0.1700 18.32 1.199 -0.1700 19.38 1.232 -0.1700 20.39 1.218 -0.1700 21.33 1.297 -0.1700 22.34 1.281 -0.1700 23.34 1.333 -0.1700 24.44 1.351 -0.1700 23.61 1.372 -0.1700 22.67 1.313 -0.1700 21.54 1.304 -0.1700 20.55 1.286 -0.1700 19.52 1.223 -0.1700 18.48 1.165 -0.1700 17.48 1.185 -0.1700 16.48 1.161 -0.1700 15.49 1.155 -0.1700 14.44 1.158 -0.1700 13.70 1.688 -0.1700 12.75 1.666 -0.1700 11.71 1.652 -0.1700 10.65 1.610 -0.1700 9.57 1.537 -0.1700 8.59 1.456 -0.1700 7.51 1.359 -0.1700 6.51 1.249 -0.1700 5.43 0.769 -0.1700 4.39 0.725 -0.1700 3.37 0.649 -0.1700 2.33 0.590 -0.1700 1.31 0.542 -0.1700 0.33 0.484 -0.1700 -0.69 0.430 -0.1700 -1.61 0.372 -0.1700 -2.57 0.304 -0.1700 -3.80 0.167 -0.1700 -4.77 0.031 -0.1700 -5.85 -0.290 -0.1700 -6.78 -0.333 -0.1700 -7.79 -0.337 -0.1700 Tabulated from data in file MS00299.DAT & reduced using program Q01.00L Average Reynolds #: 101700 Number of angles of attack: 53 alpha / Cl / Cm -5.95 -0.280 -0.1700 -5.04 -0.019 -0.1700 -3.72 0.165 -0.1700 -2.83 0.274 -0.1700 -1.75 0.399 -0.1700 -0.55 0.491 -0.1700 0.26 0.543 -0.1700 1.20 0.617 -0.1700 2.18 0.696 -0.1700 3.41 0.827 -0.1700 4.31 1.001 -0.1700 5.58 1.201 -0.1700 6.44 1.297 -0.1700 7.43 1.393 -0.1700 8.35 1.470 -0.1700 9.61 1.566 -0.1700 10.59 1.630 -0.1700 11.46 1.667 -0.1700 12.55 1.702 -0.1700 13.64 1.697 -0.1700 14.70 1.697 -0.1700 15.48 1.707 -0.1700 16.54 1.705 -0.1700 17.64 1.696 -0.1700 18.39 1.145 -0.1700 19.39 1.184 -0.1700 20.32 1.259 -0.1700 19.60 1.191 -0.1700 18.47 1.154 -0.1700 17.59 1.149 -0.1700 16.49 1.120 -0.1700 15.58 1.100 -0.1700 14.46 1.182 -0.1700 13.79 1.698 -0.1700 12.78 1.702 -0.1700 11.78 1.681 -0.1700 10.76 1.632 -0.1700 9.69 1.568 -0.1700 8.74 1.500 -0.1700 7.55 1.388 -0.1700 6.50 1.280 -0.1700 5.57 1.179 -0.1700 4.56 0.999 -0.1700 3.50 0.870 -0.1700 2.37 0.683 -0.1700 1.32 0.613 -0.1700 0.32 0.541 -0.1700 -0.61 0.473 -0.1700 -1.73 0.389 -0.1700 -2.65 0.289 -0.1700 -3.79 0.148 -0.1700 -4.55 0.045 -0.1700 -5.82 -0.278 -0.1700 Tabulated from data in file MS00158.DAT & reduced using program Q01.00L Average Reynolds #: 149500 Number of angles of attack: 65 alpha / Cl / Cm -8.04 -0.246 -0.1700 -6.87 -0.154 -0.1700 -5.82 0.078 -0.1700 -4.70 0.245 -0.1700 -3.76 0.356 -0.1700 -2.61 0.493 -0.1700 -1.53 0.596 -0.1700 -0.71 0.672 -0.1700 0.28 0.766 -0.1700 1.37 0.863 -0.1700 2.33 0.950 -0.1700 3.46 1.047 -0.1700 4.38 1.129 -0.1700 5.40 1.238 -0.1700 6.46 1.339 -0.1700 7.42 1.423 -0.1700 8.49 1.505 -0.1700 9.42 1.569 -0.1700 10.44 1.632 -0.1700 11.46 1.676 -0.1700 12.46 1.690 -0.1700 13.45 1.694 -0.1700 14.48 1.694 -0.1700 15.44 1.693 -0.1700 16.56 1.689 -0.1700 17.48 1.683 -0.1700 18.47 1.658 -0.1700 19.07 1.168 -0.1700 20.49 1.248 -0.1700 21.69 1.271 -0.1700 22.42 1.306 -0.1700 23.59 1.289 -0.1700 24.32 1.318 -0.1700 23.32 1.319 -0.1700 22.30 1.266 -0.1700 21.44 1.255 -0.1700 20.31 1.211 -0.1700 19.34 1.167 -0.1700 18.33 1.167 -0.1700 17.37 1.190 -0.1700 16.37 1.142 -0.1700 15.44 1.113 -0.1700 14.79 1.695 -0.1700 13.67 1.692 -0.1700 12.63 1.691 -0.1700 11.75 1.684 -0.1700 10.62 1.637 -0.1700 9.57 1.574 -0.1700 8.58 1.508 -0.1700 7.62 1.433 -0.1700 6.51 1.336 -0.1700 5.50 1.240 -0.1700 4.42 1.123 -0.1700 3.39 1.030 -0.1700 2.49 0.951 -0.1700 1.33 0.846 -0.1700 0.32 0.754 -0.1700 -0.71 0.657 -0.1700 -1.72 0.563 -0.1700 -2.77 0.461 -0.1700 -3.67 0.352 -0.1700 -4.88 0.204 -0.1700 -5.86 0.058 -0.1700 -6.74 -0.141 -0.1700 -7.83 -0.239 -0.1700 Tabulated from data in file MS00298.DAT & reduced using program Q01.00L Average Reynolds #: 202700 Number of angles of attack: 65 alpha / Cl / Cm -8.38 -0.233 -0.1700 -6.81 -0.089 -0.1700 -5.90 0.116 -0.1700 -4.88 0.244 -0.1700 -3.88 0.348 -0.1700 -2.87 0.460 -0.1700 -1.86 0.568 -0.1700 -0.83 0.668 -0.1700 0.28 0.775 -0.1700 1.25 0.867 -0.1700 2.31 0.972 -0.1700 3.29 1.068 -0.1700 4.39 1.172 -0.1700 5.36 1.253 -0.1700 6.47 1.358 -0.1700 7.60 1.452 -0.1700 8.71 1.538 -0.1700 9.72 1.603 -0.1700 10.76 1.660 -0.1700 11.71 1.696 -0.1700 12.64 1.705 -0.1700 13.68 1.712 -0.1700 14.67 1.720 -0.1700 15.69 1.726 -0.1700 16.69 1.723 -0.1700 17.67 1.712 -0.1700 18.72 1.691 -0.1700 19.76 1.677 -0.1700 20.63 1.667 -0.1700 21.25 1.250 -0.1700 22.35 1.259 -0.1700 23.35 1.331 -0.1700 24.40 1.345 -0.1700 23.45 1.316 -0.1700 22.45 1.322 -0.1700 21.46 1.254 -0.1700 20.45 1.217 -0.1700 19.44 1.207 -0.1700 18.44 1.148 -0.1700 17.41 1.133 -0.1700 16.47 1.150 -0.1700 15.46 1.158 -0.1700 14.72 1.719 -0.1700 13.55 1.708 -0.1700 12.57 1.703 -0.1700 11.56 1.691 -0.1700 10.45 1.642 -0.1700 9.48 1.587 -0.1700 8.27 1.505 -0.1700 7.23 1.419 -0.1700 6.17 1.324 -0.1700 5.31 1.240 -0.1700 4.39 1.159 -0.1700 3.40 1.063 -0.1700 2.33 0.961 -0.1700 1.30 0.859 -0.1700 0.38 0.768 -0.1700 -0.69 0.665 -0.1700 -1.70 0.567 -0.1700 -2.69 0.465 -0.1700 -3.77 0.346 -0.1700 -4.80 0.235 -0.1700 -5.82 0.107 -0.1700 -6.82 -0.108 -0.1700 -7.83 -0.204 -0.1700 Tabulated from data in file JG00507.DAT & reduced using program Q01.00L Average Reynolds #: 252800 Number of angles of attack: 65 alpha / Cl / Cm -8.04 -0.188 -0.1700 -6.99 -0.074 -0.1700 -5.89 0.132 -0.1700 -4.88 0.243 -0.1700 -3.86 0.353 -0.1700 -2.83 0.464 -0.1700 -1.79 0.579 -0.1700 -0.79 0.679 -0.1700 0.25 0.783 -0.1700 1.28 0.884 -0.1700 2.32 0.987 -0.1700 3.33 1.086 -0.1700 4.35 1.186 -0.1700 5.42 1.281 -0.1700 6.41 1.364 -0.1700 7.42 1.452 -0.1700 8.46 1.530 -0.1700 9.48 1.594 -0.1700 10.49 1.650 -0.1700 11.55 1.689 -0.1700 12.62 1.702 -0.1700 13.69 1.712 -0.1700 14.68 1.725 -0.1700 15.67 1.736 -0.1700 16.79 1.729 -0.1700 17.67 1.728 -0.1700 18.71 1.720 -0.1700 19.68 1.698 -0.1700 20.66 1.684 -0.1700 21.54 1.668 -0.1700 22.45 1.652 -0.1700 23.42 1.621 -0.1700 24.00 1.354 -0.1700 23.45 1.368 -0.1700 22.48 1.311 -0.1700 21.45 1.263 -0.1700 20.42 1.238 -0.1700 19.43 1.200 -0.1700 18.49 1.167 -0.1700 17.42 1.155 -0.1700 16.44 1.242 -0.1700 15.93 1.731 -0.1700 14.52 1.722 -0.1700 13.57 1.710 -0.1700 12.47 1.698 -0.1700 11.30 1.678 -0.1700 10.42 1.641 -0.1700 9.48 1.588 -0.1700 8.43 1.520 -0.1700 7.51 1.451 -0.1700 6.50 1.365 -0.1700 5.47 1.276 -0.1700 4.44 1.183 -0.1700 3.43 1.084 -0.1700 2.37 0.980 -0.1700 1.38 0.882 -0.1700 0.36 0.781 -0.1700 -0.70 0.674 -0.1700 -1.70 0.574 -0.1700 -2.73 0.461 -0.1700 -3.79 0.346 -0.1700 -4.78 0.241 -0.1700 -5.83 0.125 -0.1700 -6.76 -0.054 -0.1700 -7.87 -0.179 -0.1700 Tabulated from data in file JG00508.DAT & reduced using program Q01.00L Average Reynolds #: 303400 Number of angles of attack: 65 alpha / Cl / Cm -7.66 -0.125 -0.1700 -6.93 -0.033 -0.1700 -5.89 0.143 -0.1700 -4.88 0.253 -0.1700 -3.85 0.364 -0.1700 -2.80 0.480 -0.1700 -1.76 0.594 -0.1700 -0.73 0.700 -0.1700 0.30 0.804 -0.1700 1.31 0.907 -0.1700 2.34 1.012 -0.1700 3.37 1.117 -0.1700 4.42 1.219 -0.1700 5.43 1.310 -0.1700 6.46 1.391 -0.1700 7.47 1.477 -0.1700 8.50 1.548 -0.1700 9.52 1.611 -0.1700 10.50 1.662 -0.1700 11.48 1.697 -0.1700 12.52 1.713 -0.1700 13.57 1.723 -0.1700 14.58 1.739 -0.1700 15.68 1.747 -0.1700 16.74 1.747 -0.1700 17.61 1.742 -0.1700 18.65 1.748 -0.1700 19.65 1.733 -0.1700 20.52 1.728 -0.1700 21.43 1.693 -0.1700 22.45 1.678 -0.1700 22.92 1.339 -0.1700 24.42 1.353 -0.1700 23.44 1.358 -0.1700 22.47 1.320 -0.1700 21.41 1.273 -0.1700 20.46 1.240 -0.1700 19.46 1.199 -0.1700 18.44 1.170 -0.1700 17.51 1.225 -0.1700 16.93 1.741 -0.1700 15.27 1.742 -0.1700 14.31 1.734 -0.1700 13.18 1.716 -0.1700 12.32 1.707 -0.1700 11.37 1.690 -0.1700 10.48 1.656 -0.1700 9.51 1.600 -0.1700 8.50 1.534 -0.1700 7.47 1.458 -0.1700 6.49 1.379 -0.1700 5.47 1.299 -0.1700 4.45 1.207 -0.1700 3.38 1.096 -0.1700 2.39 0.997 -0.1700 1.35 0.891 -0.1700 0.33 0.785 -0.1700 -0.70 0.679 -0.1700 -1.71 0.574 -0.1700 -2.72 0.458 -0.1700 -3.75 0.343 -0.1700 -4.79 0.232 -0.1700 -5.82 0.122 -0.1700 -6.88 -0.064 -0.1700 -7.96 -0.174 -0.1700 Tabulated from data in file JG00510.DAT & reduced using program Q01.00L File fx63137b.lft created on 12-05-1997 at 15:25:49 using program FORMAT