XFOIL Version 6.96 Calculated polar for: NACA 0010 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.750 -1.0427 0.12024 0.11753 0.0178 1.0000 0.0088 -16.500 -1.0976 0.10476 0.10188 0.0097 1.0000 0.0086 -16.250 -1.1470 0.09107 0.08801 0.0023 1.0000 0.0084 -16.000 -1.1881 0.07916 0.07590 -0.0044 1.0000 0.0082 -15.750 -1.2206 0.06892 0.06547 -0.0106 1.0000 0.0081 -15.500 -1.2444 0.06048 0.05683 -0.0161 1.0000 0.0081 -15.250 -1.2616 0.05357 0.04973 -0.0206 1.0000 0.0082 -15.000 -1.2731 0.04808 0.04407 -0.0240 1.0000 0.0082 -14.750 -1.2810 0.04366 0.03948 -0.0262 1.0000 0.0083 -14.500 -1.2855 0.04014 0.03581 -0.0274 1.0000 0.0085 -14.250 -1.2878 0.03728 0.03279 -0.0277 1.0000 0.0086 -14.000 -1.2880 0.03492 0.03028 -0.0272 1.0000 0.0088 -13.750 -1.2866 0.03293 0.02815 -0.0261 1.0000 0.0090 -13.500 -1.2833 0.03126 0.02633 -0.0245 1.0000 0.0092 -13.250 -1.2784 0.02981 0.02473 -0.0226 1.0000 0.0094 -13.000 -1.2715 0.02855 0.02333 -0.0205 1.0000 0.0097 -12.750 -1.2605 0.02741 0.02205 -0.0188 1.0000 0.0099 -12.500 -1.2493 0.02612 0.02065 -0.0172 1.0000 0.0104 -12.250 -1.2343 0.02509 0.01954 -0.0160 1.0000 0.0109 -12.000 -1.2173 0.02420 0.01858 -0.0149 1.0000 0.0115 -11.750 -1.1994 0.02336 0.01764 -0.0139 1.0000 0.0121 -11.500 -1.1808 0.02254 0.01670 -0.0129 1.0000 0.0127 -11.250 -1.1616 0.02174 0.01577 -0.0119 1.0000 0.0132 -11.000 -1.1423 0.02091 0.01488 -0.0110 1.0000 0.0140 -10.750 -1.1210 0.02028 0.01421 -0.0103 1.0000 0.0149 -10.500 -1.0990 0.01973 0.01361 -0.0096 1.0000 0.0159 -10.250 -1.0767 0.01919 0.01299 -0.0089 1.0000 0.0170 -10.000 -1.0545 0.01862 0.01234 -0.0082 1.0000 0.0180 -9.750 -1.0318 0.01811 0.01180 -0.0076 1.0000 0.0192 -9.500 -1.0083 0.01769 0.01134 -0.0071 1.0000 0.0205 -9.250 -0.9848 0.01725 0.01084 -0.0065 1.0000 0.0218 -9.000 -0.9608 0.01688 0.01039 -0.0060 1.0000 0.0229 -8.750 -0.9380 0.01635 0.00981 -0.0053 1.0000 0.0240 -8.500 -0.9150 0.01584 0.00926 -0.0046 1.0000 0.0254 -8.250 -0.8913 0.01543 0.00883 -0.0040 1.0000 0.0267 -8.000 -0.8675 0.01506 0.00841 -0.0034 1.0000 0.0280 -7.750 -0.8435 0.01471 0.00800 -0.0027 1.0000 0.0292 -7.500 -0.8195 0.01439 0.00763 -0.0021 1.0000 0.0300 -7.250 -0.7972 0.01385 0.00705 -0.0012 1.0000 0.0315 -7.000 -0.7744 0.01341 0.00659 -0.0003 1.0000 0.0330 -6.750 -0.7513 0.01305 0.00621 0.0005 1.0000 0.0345 -6.500 -0.7280 0.01273 0.00586 0.0014 1.0000 0.0359 -6.250 -0.7046 0.01242 0.00551 0.0022 1.0000 0.0371 -6.000 -0.6812 0.01214 0.00519 0.0030 1.0000 0.0382 -5.750 -0.6582 0.01180 0.00483 0.0040 1.0000 0.0400 -5.500 -0.6352 0.01148 0.00451 0.0049 1.0000 0.0424 -5.250 -0.6121 0.01121 0.00424 0.0058 1.0000 0.0452 -5.000 -0.5834 0.01095 0.00397 0.0055 0.9986 0.0491 -4.750 -0.5495 0.01062 0.00369 0.0040 0.9957 0.0594 -4.500 -0.5162 0.01026 0.00343 0.0026 0.9925 0.0765 -4.250 -0.4831 0.00994 0.00318 0.0013 0.9886 0.0953 -4.000 -0.4488 0.00962 0.00296 -0.0002 0.9853 0.1173 -3.750 -0.4169 0.00931 0.00276 -0.0012 0.9800 0.1429 -3.500 -0.3841 0.00899 0.00256 -0.0024 0.9747 0.1722 -3.250 -0.3533 0.00869 0.00239 -0.0032 0.9673 0.2033 -3.000 -0.3212 0.00837 0.00222 -0.0042 0.9602 0.2419 -2.750 -0.2920 0.00803 0.00208 -0.0046 0.9499 0.2895 -2.500 -0.2631 0.00770 0.00194 -0.0048 0.9384 0.3398 -2.250 -0.2348 0.00742 0.00182 -0.0049 0.9246 0.3849 -2.000 -0.2075 0.00718 0.00171 -0.0047 0.9082 0.4282 -1.750 -0.1810 0.00699 0.00162 -0.0043 0.8895 0.4653 -1.500 -0.1550 0.00681 0.00153 -0.0037 0.8687 0.5057 -1.250 -0.1293 0.00665 0.00146 -0.0031 0.8455 0.5472 -0.750 -0.0775 0.00649 0.00135 -0.0018 0.7945 0.6116 -0.500 -0.0517 0.00644 0.00131 -0.0012 0.7661 0.6436 -0.250 -0.0258 0.00641 0.00129 -0.0006 0.7368 0.6754 0.000 0.0000 0.00640 0.00129 0.0000 0.7063 0.7064 0.250 0.0259 0.00641 0.00129 0.0006 0.6753 0.7366 0.500 0.0517 0.00644 0.00131 0.0012 0.6434 0.7662 0.750 0.0775 0.00650 0.00135 0.0018 0.6114 0.7944 1.250 0.1293 0.00665 0.00146 0.0031 0.5474 0.8455 1.500 0.1550 0.00681 0.00153 0.0037 0.5059 0.8687 1.750 0.1810 0.00699 0.00162 0.0043 0.4652 0.8893 2.000 0.2075 0.00718 0.00171 0.0047 0.4278 0.9082 2.250 0.2348 0.00742 0.00182 0.0049 0.3851 0.9246 2.500 0.2631 0.00770 0.00194 0.0048 0.3396 0.9383 2.750 0.2920 0.00803 0.00208 0.0046 0.2895 0.9499 3.000 0.3211 0.00837 0.00222 0.0042 0.2419 0.9603 3.250 0.3533 0.00869 0.00239 0.0032 0.2035 0.9673 3.500 0.3841 0.00899 0.00256 0.0024 0.1722 0.9747 3.750 0.4169 0.00930 0.00276 0.0012 0.1429 0.9800 4.000 0.4488 0.00961 0.00296 0.0002 0.1174 0.9853 4.250 0.4831 0.00994 0.00318 -0.0014 0.0954 0.9886 4.500 0.5162 0.01026 0.00343 -0.0026 0.0765 0.9925 4.750 0.5496 0.01061 0.00369 -0.0040 0.0594 0.9957 5.000 0.5834 0.01095 0.00397 -0.0055 0.0491 0.9986 5.250 0.6121 0.01121 0.00424 -0.0058 0.0452 1.0000 5.500 0.6352 0.01148 0.00451 -0.0049 0.0425 1.0000 5.750 0.6582 0.01180 0.00483 -0.0040 0.0400 1.0000 6.000 0.6812 0.01214 0.00519 -0.0030 0.0382 1.0000 6.250 0.7046 0.01242 0.00551 -0.0022 0.0371 1.0000 6.500 0.7280 0.01273 0.00586 -0.0013 0.0359 1.0000 6.750 0.7512 0.01305 0.00621 -0.0005 0.0345 1.0000 7.000 0.7744 0.01341 0.00659 0.0003 0.0330 1.0000 7.250 0.7972 0.01385 0.00705 0.0012 0.0315 1.0000 7.500 0.8195 0.01439 0.00763 0.0021 0.0300 1.0000 7.750 0.8435 0.01471 0.00800 0.0027 0.0292 1.0000 8.000 0.8675 0.01506 0.00841 0.0034 0.0280 1.0000 8.250 0.8913 0.01543 0.00883 0.0040 0.0267 1.0000 8.500 0.9151 0.01583 0.00926 0.0046 0.0254 1.0000 8.750 0.9380 0.01635 0.00980 0.0053 0.0240 1.0000 9.000 0.9609 0.01687 0.01038 0.0060 0.0229 1.0000 9.250 0.9848 0.01725 0.01084 0.0065 0.0218 1.0000 9.500 1.0083 0.01769 0.01134 0.0071 0.0205 1.0000 9.750 1.0318 0.01811 0.01180 0.0076 0.0192 1.0000 10.000 1.0545 0.01862 0.01234 0.0082 0.0180 1.0000 10.250 1.0767 0.01919 0.01299 0.0089 0.0170 1.0000 10.500 1.0990 0.01973 0.01361 0.0096 0.0159 1.0000 10.750 1.1211 0.02028 0.01421 0.0103 0.0149 1.0000 11.000 1.1423 0.02091 0.01488 0.0110 0.0140 1.0000 11.250 1.1616 0.02174 0.01577 0.0119 0.0132 1.0000 11.500 1.1809 0.02254 0.01670 0.0129 0.0127 1.0000 11.750 1.1995 0.02336 0.01764 0.0139 0.0120 1.0000 12.000 1.2175 0.02420 0.01857 0.0149 0.0115 1.0000 12.250 1.2346 0.02509 0.01954 0.0159 0.0109 1.0000 12.500 1.2496 0.02612 0.02065 0.0172 0.0104 1.0000 12.750 1.2609 0.02741 0.02205 0.0187 0.0099 1.0000 13.000 1.2719 0.02855 0.02333 0.0204 0.0097 1.0000 13.250 1.2789 0.02981 0.02473 0.0225 0.0094 1.0000 13.500 1.2839 0.03126 0.02633 0.0244 0.0092 1.0000 13.750 1.2872 0.03294 0.02815 0.0260 0.0090 1.0000 14.000 1.2888 0.03491 0.03027 0.0271 0.0088 1.0000 14.250 1.2886 0.03726 0.03277 0.0275 0.0086 1.0000 14.500 1.2865 0.04012 0.03579 0.0273 0.0085 1.0000 14.750 1.2820 0.04365 0.03947 0.0261 0.0083 1.0000 15.000 1.2744 0.04805 0.04403 0.0238 0.0082 1.0000 15.250 1.2628 0.05356 0.04972 0.0204 0.0082 1.0000 15.500 1.2460 0.06043 0.05678 0.0159 0.0081 1.0000 15.750 1.2223 0.06887 0.06541 0.0104 0.0081 1.0000 16.000 1.1898 0.07913 0.07587 0.0042 0.0082 1.0000 16.250 1.1483 0.09115 0.08809 -0.0026 0.0084 1.0000 16.500 1.0990 0.10483 0.10196 -0.0100 0.0086 1.0000 16.750 1.0437 0.12041 0.11770 -0.0182 0.0088 1.0000 17.000 0.9647 0.14290 0.14040 -0.0300 0.0092 1.0000