XFOIL Version 6.96 Calculated polar for: NACA 0010-66 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.750 -1.0137 0.09712 0.09509 -0.0381 1.0000 0.0096 -16.500 -1.1347 0.06734 0.06502 -0.0552 1.0000 0.0090 -16.250 -1.1877 0.05424 0.05164 -0.0633 1.0000 0.0089 -16.000 -1.2176 0.04901 0.04623 -0.0626 1.0000 0.0088 -15.750 -1.2398 0.04547 0.04254 -0.0599 1.0000 0.0089 -15.500 -1.2587 0.04265 0.03957 -0.0562 1.0000 0.0089 -15.250 -1.2740 0.04035 0.03713 -0.0520 1.0000 0.0090 -15.000 -1.2860 0.03847 0.03511 -0.0476 1.0000 0.0091 -14.750 -1.2850 0.03657 0.03305 -0.0455 0.9993 0.0092 -14.500 -1.2799 0.03509 0.03143 -0.0435 0.9986 0.0093 -14.250 -1.2722 0.03383 0.03003 -0.0415 0.9978 0.0094 -14.000 -1.2865 0.03082 0.02672 -0.0367 0.9964 0.0097 -13.750 -1.2818 0.02923 0.02499 -0.0340 0.9955 0.0100 -13.500 -1.2694 0.02822 0.02388 -0.0324 0.9948 0.0103 -13.250 -1.2542 0.02743 0.02301 -0.0310 0.9943 0.0106 -13.000 -1.2468 0.02673 0.02222 -0.0277 0.9924 0.0109 -12.750 -1.2357 0.02605 0.02145 -0.0251 0.9909 0.0112 -12.500 -1.2228 0.02535 0.02065 -0.0228 0.9894 0.0115 -12.250 -1.2081 0.02465 0.01984 -0.0209 0.9882 0.0118 -12.000 -1.1895 0.02400 0.01907 -0.0197 0.9872 0.0121 -11.750 -1.1679 0.02343 0.01839 -0.0191 0.9864 0.0124 -11.500 -1.1532 0.02195 0.01675 -0.0174 0.9856 0.0131 -11.250 -1.1296 0.02147 0.01623 -0.0172 0.9851 0.0137 -11.000 -1.1043 0.02114 0.01587 -0.0172 0.9847 0.0142 -10.750 -1.0784 0.02086 0.01553 -0.0174 0.9843 0.0149 -10.500 -1.0735 0.02055 0.01517 -0.0127 0.9810 0.0153 -10.250 -1.0546 0.02027 0.01481 -0.0111 0.9793 0.0157 -10.000 -1.0361 0.01951 0.01395 -0.0096 0.9780 0.0164 -9.750 -1.0143 0.01893 0.01334 -0.0088 0.9770 0.0172 -9.500 -0.9888 0.01870 0.01310 -0.0088 0.9761 0.0180 -9.250 -0.9632 0.01846 0.01281 -0.0087 0.9754 0.0187 -9.000 -0.9374 0.01818 0.01248 -0.0086 0.9748 0.0196 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-4.000 -0.4828 0.01260 0.00631 0.0090 0.9530 0.0412 -3.750 -0.4591 0.01243 0.00613 0.0098 0.9518 0.0437 -3.500 -0.4337 0.01222 0.00597 0.0102 0.9509 0.0498 -3.250 -0.4077 0.01197 0.00582 0.0105 0.9501 0.0682 -3.000 -0.3823 0.01170 0.00571 0.0107 0.9494 0.1024 -2.750 -0.3563 0.01150 0.00564 0.0109 0.9489 0.1303 -2.500 -0.3301 0.01130 0.00557 0.0111 0.9483 0.1640 -2.250 -0.3047 0.01102 0.00551 0.0113 0.9478 0.2154 -2.000 -0.2799 0.01074 0.00547 0.0117 0.9473 0.2787 -1.750 -0.2561 0.01041 0.00543 0.0123 0.9468 0.3546 -1.500 -0.2609 0.01023 0.00546 0.0196 0.9411 0.4166 -1.250 -0.2499 0.00943 0.00525 0.0231 0.9381 0.5696 -1.000 -0.2438 0.00806 0.00518 0.0286 0.9359 0.8951 -0.750 -0.1998 0.00792 0.00505 0.0253 0.9347 0.9176 -0.500 -0.1417 0.00791 0.00506 0.0189 0.9341 0.9273 -0.250 -0.0722 0.00737 0.00449 0.0099 0.9334 0.9328 0.000 0.0000 0.00721 0.00433 0.0000 0.9332 0.9332 0.250 0.0728 0.00736 0.00448 -0.0101 0.9328 0.9333 0.500 0.1420 0.00791 0.00506 -0.0189 0.9273 0.9342 0.750 0.1997 0.00792 0.00505 -0.0253 0.9176 0.9347 1.000 0.2445 0.00805 0.00517 -0.0288 0.8939 0.9359 1.250 0.2501 0.00943 0.00525 -0.0232 0.5706 0.9381 1.500 0.2609 0.01022 0.00546 -0.0196 0.4176 0.9412 1.750 0.2561 0.01041 0.00543 -0.0123 0.3546 0.9468 2.000 0.2799 0.01074 0.00546 -0.0117 0.2781 0.9473 2.250 0.3047 0.01102 0.00551 -0.0113 0.2150 0.9478 2.500 0.3302 0.01129 0.00556 -0.0111 0.1644 0.9483 2.750 0.3563 0.01150 0.00564 -0.0109 0.1302 0.9489 3.000 0.3823 0.01170 0.00571 -0.0108 0.1024 0.9494 3.250 0.4076 0.01197 0.00581 -0.0104 0.0680 0.9501 3.500 0.4336 0.01222 0.00597 -0.0102 0.0497 0.9509 3.750 0.4590 0.01243 0.00613 -0.0098 0.0437 0.9519 4.000 0.4828 0.01260 0.00631 -0.0090 0.0411 0.9530 4.250 0.5042 0.01273 0.00645 -0.0077 0.0398 0.9545 4.500 0.4979 0.01272 0.00649 0.0000 0.0391 0.9598 4.750 0.5266 0.01289 0.00666 -0.0004 0.0373 0.9602 5.000 0.5549 0.01313 0.00689 -0.0008 0.0356 0.9606 5.250 0.5818 0.01352 0.00731 -0.0008 0.0338 0.9611 5.500 0.6088 0.01383 0.00767 -0.0008 0.0327 0.9615 5.750 0.6362 0.01401 0.00788 -0.0009 0.0320 0.9620 6.000 0.6629 0.01426 0.00815 -0.0009 0.0311 0.9625 6.250 0.6893 0.01449 0.00841 -0.0008 0.0299 0.9631 6.500 0.7151 0.01473 0.00866 -0.0007 0.0288 0.9638 6.750 0.7396 0.01507 0.00900 -0.0002 0.0277 0.9646 7.000 0.7597 0.01605 0.01006 0.0011 0.0260 0.9654 7.250 0.7836 0.01611 0.01015 0.0018 0.0255 0.9666 7.500 0.8044 0.01626 0.01034 0.0031 0.0248 0.9684 7.750 0.8056 0.01642 0.01055 0.0090 0.0243 0.9726 8.000 0.8331 0.01666 0.01082 0.0087 0.0233 0.9730 8.250 0.8604 0.01688 0.01105 0.0085 0.0224 0.9734 8.500 0.8867 0.01723 0.01141 0.0083 0.0214 0.9739 8.750 0.9103 0.01803 0.01229 0.0088 0.0202 0.9743 9.000 0.9373 0.01818 0.01249 0.0086 0.0196 0.9748 9.250 0.9632 0.01845 0.01281 0.0087 0.0187 0.9754 9.500 0.9887 0.01870 0.01309 0.0088 0.0180 0.9761 9.750 1.0143 0.01892 0.01333 0.0088 0.0172 0.9770 10.000 1.0361 0.01950 0.01394 0.0096 0.0164 0.9780 10.250 1.0546 0.02026 0.01480 0.0111 0.0157 0.9794 10.500 1.0736 0.02052 0.01513 0.0126 0.0153 0.9810 10.750 1.0787 0.02085 0.01552 0.0173 0.0148 0.9843 11.000 1.1046 0.02113 0.01586 0.0172 0.0142 0.9847 11.250 1.1300 0.02146 0.01622 0.0171 0.0136 0.9851 11.500 1.1535 0.02195 0.01675 0.0173 0.0131 0.9856 11.750 1.1684 0.02343 0.01839 0.0190 0.0123 0.9864 12.000 1.1901 0.02400 0.01907 0.0196 0.0121 0.9872 12.250 1.2086 0.02466 0.01985 0.0208 0.0118 0.9882 12.500 1.2234 0.02535 0.02065 0.0227 0.0115 0.9895 12.750 1.2365 0.02602 0.02142 0.0249 0.0112 0.9909 13.000 1.2471 0.02675 0.02225 0.0276 0.0109 0.9925 13.250 1.2548 0.02744 0.02303 0.0309 0.0106 0.9943 13.500 1.2703 0.02821 0.02388 0.0322 0.0103 0.9948 13.750 1.2829 0.02922 0.02498 0.0338 0.0100 0.9955 14.000 1.2872 0.03085 0.02676 0.0365 0.0097 0.9965 14.250 1.2731 0.03384 0.03004 0.0413 0.0094 0.9978 14.500 1.2809 0.03509 0.03143 0.0432 0.0093 0.9986 14.750 1.2858 0.03659 0.03308 0.0453 0.0092 0.9994 15.000 1.2867 0.03843 0.03507 0.0475 0.0091 1.0000 15.250 1.2746 0.04032 0.03710 0.0520 0.0090 1.0000 15.500 1.2589 0.04265 0.03957 0.0562 0.0089 1.0000 15.750 1.2408 0.04539 0.04246 0.0598 0.0089 1.0000 16.000 1.2172 0.04905 0.04628 0.0626 0.0088 1.0000 16.250 1.1882 0.05419 0.05159 0.0633 0.0089 1.0000 16.500 1.1295 0.06881 0.06651 0.0539 0.0090 1.0000 16.750 1.0135 0.09727 0.09525 0.0379 0.0096 1.0000