XFOIL Version 6.96 Calculated polar for: NACA 1410 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.750 -1.0860 0.10096 0.09860 -0.0040 1.0000 0.0061 -16.500 -1.2328 0.06971 0.06695 -0.0220 1.0000 0.0056 -16.250 -1.2897 0.05406 0.05100 -0.0333 1.0000 0.0055 -16.000 -1.3138 0.04558 0.04230 -0.0401 1.0000 0.0054 -15.750 -1.3270 0.04003 0.03657 -0.0441 1.0000 0.0055 -15.500 -1.3346 0.03621 0.03259 -0.0459 1.0000 0.0055 -15.250 -1.3383 0.03344 0.02969 -0.0460 1.0000 0.0056 -15.000 -1.3390 0.03135 0.02747 -0.0451 1.0000 0.0057 -14.750 -1.3371 0.02970 0.02571 -0.0434 1.0000 0.0058 -14.500 -1.3325 0.02833 0.02423 -0.0414 1.0000 0.0059 -14.250 -1.3221 0.02708 0.02287 -0.0400 1.0000 0.0060 -14.000 -1.3092 0.02593 0.02161 -0.0388 1.0000 0.0062 -13.750 -1.2944 0.02487 0.02045 -0.0377 1.0000 0.0063 -13.500 -1.2783 0.02388 0.01936 -0.0367 1.0000 0.0065 -13.250 -1.2608 0.02296 0.01834 -0.0358 1.0000 0.0067 -13.000 -1.2424 0.02212 0.01739 -0.0349 1.0000 0.0068 -12.750 -1.2229 0.02134 0.01652 -0.0341 1.0000 0.0069 -12.500 -1.2044 0.02039 0.01548 -0.0332 1.0000 0.0073 -12.250 -1.1846 0.01957 0.01459 -0.0324 1.0000 0.0076 -12.000 -1.1638 0.01886 0.01381 -0.0316 1.0000 0.0079 -11.750 -1.1424 0.01820 0.01309 -0.0309 1.0000 0.0083 -11.500 -1.1205 0.01760 0.01243 -0.0302 1.0000 0.0087 -11.250 -1.0983 0.01705 0.01180 -0.0295 1.0000 0.0091 -11.000 -1.0757 0.01654 0.01121 -0.0289 1.0000 0.0093 -10.750 -1.0540 0.01591 0.01054 -0.0280 1.0000 0.0100 -10.500 -1.0318 0.01538 0.00997 -0.0273 1.0000 0.0107 -10.250 -1.0094 0.01491 0.00946 -0.0264 1.0000 0.0113 -10.000 -0.9870 0.01447 0.00898 -0.0256 1.0000 0.0120 -9.750 -0.9646 0.01407 0.00851 -0.0247 1.0000 0.0126 -9.500 -0.9424 0.01364 0.00808 -0.0238 1.0000 0.0137 -9.250 -0.9199 0.01328 0.00770 -0.0229 1.0000 0.0150 -9.000 -0.8974 0.01295 0.00734 -0.0219 1.0000 0.0161 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0.0438 -4.000 -0.3123 0.00809 0.00217 -0.0291 0.8994 0.0514 -3.750 -0.2856 0.00791 0.00201 -0.0288 0.8853 0.0642 -3.500 -0.2587 0.00775 0.00186 -0.0285 0.8705 0.0778 -3.250 -0.2317 0.00762 0.00172 -0.0283 0.8547 0.0910 -3.000 -0.2046 0.00749 0.00160 -0.0281 0.8382 0.1059 -2.750 -0.1775 0.00736 0.00148 -0.0279 0.8211 0.1240 -2.500 -0.1505 0.00722 0.00137 -0.0276 0.8027 0.1495 -2.250 -0.1235 0.00709 0.00128 -0.0275 0.7844 0.1757 -2.000 -0.0965 0.00697 0.00119 -0.0273 0.7648 0.2056 -1.750 -0.0694 0.00685 0.00112 -0.0271 0.7444 0.2386 -1.500 -0.0422 0.00677 0.00107 -0.0269 0.7217 0.2691 -1.250 -0.0149 0.00675 0.00102 -0.0268 0.6971 0.2886 -0.750 0.0388 0.00649 0.00091 -0.0265 0.6505 0.3769 -0.500 0.0654 0.00630 0.00091 -0.0263 0.6286 0.4589 -0.250 0.0928 0.00628 0.00091 -0.0262 0.6077 0.4926 0.000 0.1204 0.00627 0.00091 -0.0261 0.5863 0.5180 0.250 0.1479 0.00630 0.00092 -0.0260 0.5641 0.5371 0.500 0.1753 0.00633 0.00093 -0.0259 0.5388 0.5590 0.750 0.2026 0.00634 0.00096 -0.0258 0.5147 0.5860 1.000 0.2296 0.00630 0.00099 -0.0256 0.4932 0.6309 1.250 0.2563 0.00626 0.00104 -0.0253 0.4716 0.6815 1.500 0.2824 0.00631 0.00110 -0.0250 0.4337 0.7278 1.750 0.3079 0.00642 0.00118 -0.0245 0.3883 0.7732 2.000 0.3337 0.00646 0.00127 -0.0240 0.3610 0.8159 2.500 0.3847 0.00673 0.00149 -0.0229 0.2945 0.8807 2.750 0.4098 0.00690 0.00161 -0.0222 0.2629 0.9086 3.000 0.4356 0.00708 0.00175 -0.0217 0.2362 0.9351 3.250 0.4628 0.00738 0.00191 -0.0216 0.1970 0.9537 3.500 0.4922 0.00767 0.00207 -0.0220 0.1650 0.9665 3.750 0.5228 0.00798 0.00225 -0.0227 0.1353 0.9767 4.000 0.5539 0.00830 0.00244 -0.0235 0.1070 0.9852 4.250 0.5863 0.00860 0.00263 -0.0247 0.0865 0.9909 4.500 0.6176 0.00887 0.00283 -0.0255 0.0708 0.9952 4.750 0.6497 0.00919 0.00306 -0.0266 0.0535 0.9982 5.000 0.6785 0.00947 0.00327 -0.0270 0.0436 1.0000 5.250 0.7030 0.00970 0.00348 -0.0263 0.0389 1.0000 5.500 0.7278 0.00991 0.00369 -0.0257 0.0366 1.0000 5.750 0.7527 0.01015 0.00391 -0.0251 0.0346 1.0000 6.000 0.7777 0.01041 0.00417 -0.0246 0.0323 1.0000 6.250 0.8030 0.01066 0.00444 -0.0241 0.0313 1.0000 6.500 0.8285 0.01089 0.00468 -0.0236 0.0308 1.0000 6.750 0.8541 0.01112 0.00493 -0.0232 0.0299 1.0000 7.000 0.8796 0.01138 0.00520 -0.0228 0.0289 1.0000 7.250 0.9050 0.01165 0.00549 -0.0224 0.0277 1.0000 7.500 0.9301 0.01196 0.00581 -0.0220 0.0265 1.0000 7.750 0.9548 0.01233 0.00619 -0.0215 0.0251 1.0000 8.000 0.9798 0.01266 0.00654 -0.0211 0.0242 1.0000 8.250 1.0053 0.01291 0.00683 -0.0208 0.0237 1.0000 8.500 1.0306 0.01319 0.00714 -0.0204 0.0229 1.0000 8.750 1.0557 0.01348 0.00746 -0.0200 0.0219 1.0000 9.000 1.0805 0.01380 0.00777 -0.0196 0.0206 1.0000 9.250 1.1049 0.01417 0.00814 -0.0192 0.0193 1.0000 9.500 1.1291 0.01454 0.00856 -0.0187 0.0184 1.0000 9.750 1.1535 0.01488 0.00893 -0.0182 0.0174 1.0000 10.000 1.1775 0.01524 0.00931 -0.0178 0.0161 1.0000 10.250 1.2009 0.01566 0.00971 -0.0172 0.0145 1.0000 10.500 1.2240 0.01610 0.01019 -0.0166 0.0134 1.0000 10.750 1.2467 0.01657 0.01068 -0.0160 0.0123 1.0000 11.000 1.2688 0.01709 0.01123 -0.0153 0.0113 1.0000 11.250 1.2903 0.01764 0.01182 -0.0145 0.0105 1.0000 11.500 1.3118 0.01818 0.01241 -0.0137 0.0099 1.0000 11.750 1.3324 0.01877 0.01305 -0.0128 0.0094 1.0000 12.000 1.3523 0.01940 0.01373 -0.0119 0.0088 1.0000 12.250 1.3711 0.02011 0.01448 -0.0108 0.0083 1.0000 12.500 1.3890 0.02085 0.01530 -0.0096 0.0078 1.0000 12.750 1.4071 0.02152 0.01604 -0.0085 0.0076 1.0000 13.000 1.4241 0.02224 0.01683 -0.0072 0.0073 1.0000 13.250 1.4395 0.02301 0.01768 -0.0058 0.0070 1.0000 13.500 1.4517 0.02383 0.01857 -0.0038 0.0067 1.0000 13.750 1.4621 0.02474 0.01955 -0.0017 0.0065 1.0000 14.000 1.4713 0.02576 0.02065 0.0003 0.0063 1.0000 14.250 1.4787 0.02695 0.02193 0.0023 0.0060 1.0000 14.500 1.4842 0.02834 0.02341 0.0042 0.0058 1.0000 14.750 1.4893 0.02983 0.02500 0.0058 0.0057 1.0000 15.000 1.4949 0.03138 0.02665 0.0071 0.0056 1.0000 15.250 1.4991 0.03316 0.02854 0.0081 0.0055 1.0000 15.500 1.5018 0.03521 0.03070 0.0089 0.0054 1.0000 15.750 1.5030 0.03757 0.03318 0.0092 0.0054 1.0000 16.000 1.5023 0.04031 0.03604 0.0092 0.0053 1.0000 16.250 1.4999 0.04347 0.03932 0.0087 0.0052 1.0000 16.500 1.4951 0.04712 0.04311 0.0076 0.0051 1.0000 16.750 1.4877 0.05138 0.04750 0.0061 0.0051 1.0000 17.000 1.4772 0.05629 0.05255 0.0040 0.0050 1.0000 17.250 1.4630 0.06198 0.05838 0.0013 0.0050 1.0000 17.500 1.4444 0.06857 0.06513 -0.0020 0.0050 1.0000 17.750 1.4203 0.07629 0.07300 -0.0059 0.0050 1.0000 18.000 1.3905 0.08528 0.08217 -0.0106 0.0050 1.0000 18.250 1.3541 0.09577 0.09283 -0.0161 0.0050 1.0000 18.500 1.3107 0.10791 0.10516 -0.0224 0.0051 1.0000 18.750 1.2597 0.12204 0.11947 -0.0298 0.0052 1.0000 19.000 1.2059 0.13730 0.13492 -0.0380 0.0053 1.0000