XFOIL Version 6.96 Calculated polar for: NACA M6 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 ------ -------- --------- --------- -------- -------- -------- -12.500 -0.8105 0.05068 0.04766 -0.0581 1.0000 0.0217 -12.250 -0.8482 0.04510 0.04179 -0.0573 1.0000 0.0218 -12.000 -0.8733 0.04153 0.03795 -0.0540 1.0000 0.0220 -11.750 -0.8915 0.03887 0.03502 -0.0496 1.0000 0.0222 -11.500 -0.9037 0.03688 0.03280 -0.0449 1.0000 0.0223 -11.250 -0.9120 0.03533 0.03105 -0.0399 1.0000 0.0224 -11.000 -0.9189 0.03355 0.02906 -0.0350 1.0000 0.0226 -10.750 -0.9198 0.03171 0.02703 -0.0310 1.0000 0.0227 -10.500 -0.9157 0.03024 0.02544 -0.0276 1.0000 0.0230 -10.250 -0.9081 0.02907 0.02417 -0.0246 1.0000 0.0231 -10.000 -0.8986 0.02808 0.02309 -0.0217 1.0000 0.0233 -9.750 -0.8887 0.02712 0.02203 -0.0188 1.0000 0.0235 -9.500 -0.8715 0.02613 0.02094 -0.0174 0.9916 0.0237 -9.250 -0.8431 0.02524 0.01993 -0.0183 0.9794 0.0241 -9.000 -0.8114 0.02403 0.01857 -0.0198 0.9670 0.0244 -8.750 -0.7764 0.02278 0.01715 -0.0221 0.9542 0.0248 -8.500 -0.7384 0.02156 0.01574 -0.0249 0.9400 0.0252 -8.250 -0.7018 0.02041 0.01440 -0.0272 0.9232 0.0254 -8.000 -0.6711 0.01951 0.01332 -0.0282 0.9038 0.0258 -7.750 -0.6455 0.01879 0.01242 -0.0279 0.8839 0.0261 -7.500 -0.6224 0.01817 0.01163 -0.0270 0.8656 0.0264 -7.250 -0.6001 0.01768 0.01100 -0.0259 0.8484 0.0267 -7.000 -0.5779 0.01721 0.01038 -0.0248 0.8313 0.0270 -6.500 -0.5328 0.01631 0.00921 -0.0226 0.7988 0.0273 -6.250 -0.5098 0.01572 0.00852 -0.0216 0.7838 0.0275 -6.000 -0.4870 0.01507 0.00778 -0.0207 0.7702 0.0278 -5.750 -0.4643 0.01452 0.00714 -0.0197 0.7573 0.0282 -5.500 -0.4416 0.01409 0.00663 -0.0187 0.7454 0.0285 -5.250 -0.4186 0.01373 0.00620 -0.0176 0.7335 0.0288 -5.000 -0.3954 0.01338 0.00581 -0.0166 0.7229 0.0291 -4.750 -0.3722 0.01308 0.00544 -0.0156 0.7130 0.0295 -4.500 -0.3487 0.01279 0.00510 -0.0147 0.7031 0.0299 -4.250 -0.3252 0.01252 0.00478 -0.0138 0.6942 0.0303 -4.000 -0.3014 0.01229 0.00449 -0.0129 0.6850 0.0308 -3.750 -0.2775 0.01206 0.00422 -0.0120 0.6769 0.0314 -3.500 -0.2535 0.01185 0.00395 -0.0111 0.6682 0.0320 -3.250 -0.2293 0.01165 0.00371 -0.0103 0.6604 0.0325 -3.000 -0.2050 0.01147 0.00348 -0.0094 0.6524 0.0328 -2.750 -0.1805 0.01131 0.00328 -0.0087 0.6449 0.0333 -2.500 -0.1564 0.01109 0.00304 -0.0078 0.6372 0.0342 -2.250 -0.1320 0.01094 0.00284 -0.0070 0.6301 0.0352 -2.000 -0.1072 0.01079 0.00269 -0.0063 0.6225 0.0363 -1.750 -0.0827 0.01068 0.00254 -0.0055 0.6154 0.0378 -1.500 -0.0576 0.01057 0.00241 -0.0048 0.6081 0.0396 -1.250 -0.0333 0.01044 0.00229 -0.0040 0.6009 0.0453 -1.000 -0.0095 0.01021 0.00219 -0.0031 0.5942 0.0732 -0.750 0.0141 0.01002 0.00210 -0.0022 0.5871 0.1058 -0.500 0.0377 0.00984 0.00204 -0.0013 0.5803 0.1425 -0.250 0.0615 0.00966 0.00198 -0.0005 0.5735 0.1793 0.250 0.1064 0.00918 0.00187 0.0017 0.5601 0.3034 0.500 0.1160 0.00829 0.00174 0.0053 0.5538 0.5301 1.000 0.2515 0.00763 0.00235 -0.0118 0.5361 0.9128 1.250 0.2863 0.00794 0.00264 -0.0129 0.5289 0.9260 1.500 0.3239 0.00829 0.00295 -0.0147 0.5208 0.9330 1.750 0.3503 0.00845 0.00308 -0.0142 0.5132 0.9402 2.000 0.3871 0.00869 0.00325 -0.0160 0.5030 0.9434 2.250 0.4181 0.00884 0.00336 -0.0166 0.4911 0.9469 2.500 0.4393 0.00895 0.00342 -0.0151 0.4798 0.9522 2.750 0.4702 0.00906 0.00347 -0.0158 0.4690 0.9533 3.000 0.5008 0.00914 0.00353 -0.0165 0.4590 0.9545 3.250 0.5305 0.00925 0.00361 -0.0170 0.4497 0.9562 3.500 0.5588 0.00935 0.00368 -0.0171 0.4405 0.9582 3.750 0.5839 0.00946 0.00377 -0.0166 0.4312 0.9612 4.000 0.6079 0.00960 0.00388 -0.0158 0.4195 0.9643 4.250 0.6380 0.00975 0.00397 -0.0164 0.4044 0.9654 4.750 0.6954 0.01007 0.00420 -0.0171 0.3748 0.9685 5.000 0.7221 0.01026 0.00435 -0.0170 0.3587 0.9710 5.250 0.7435 0.01049 0.00454 -0.0158 0.3440 0.9746 5.500 0.7728 0.01073 0.00470 -0.0164 0.3196 0.9756 5.750 0.8010 0.01103 0.00488 -0.0168 0.2932 0.9769 6.000 0.8277 0.01140 0.00512 -0.0169 0.2618 0.9785 6.250 0.8538 0.01176 0.00538 -0.0169 0.2369 0.9806 6.500 0.8772 0.01218 0.00570 -0.0164 0.2127 0.9835 6.750 0.9023 0.01260 0.00602 -0.0163 0.1895 0.9853 7.000 0.9297 0.01302 0.00634 -0.0167 0.1646 0.9865 7.250 0.9560 0.01350 0.00670 -0.0170 0.1387 0.9881 7.500 0.9788 0.01424 0.00721 -0.0168 0.0985 0.9902 7.750 1.0024 0.01482 0.00769 -0.0165 0.0813 0.9923 8.000 1.0269 0.01531 0.00816 -0.0164 0.0701 0.9942 8.250 1.0542 0.01577 0.00857 -0.0169 0.0591 0.9955 8.500 1.0806 0.01623 0.00900 -0.0173 0.0502 0.9971 8.750 1.1065 0.01670 0.00946 -0.0176 0.0443 0.9986 9.000 1.1323 0.01719 0.00995 -0.0179 0.0400 0.9999 9.250 1.1477 0.01764 0.01042 -0.0159 0.0374 1.0000 9.500 1.1610 0.01814 0.01093 -0.0135 0.0353 1.0000 9.750 1.1733 0.01867 0.01149 -0.0111 0.0334 1.0000 10.000 1.1859 0.01915 0.01202 -0.0086 0.0321 1.0000 10.250 1.1966 0.01967 0.01258 -0.0059 0.0304 1.0000 10.500 1.2043 0.02025 0.01319 -0.0027 0.0293 1.0000 10.750 1.2040 0.02085 0.01382 0.0020 0.0281 1.0000 11.000 1.2071 0.02141 0.01444 0.0058 0.0273 1.0000 11.250 1.2112 0.02207 0.01517 0.0093 0.0265 1.0000 11.500 1.2161 0.02282 0.01599 0.0122 0.0256 1.0000 11.750 1.2206 0.02372 0.01694 0.0150 0.0246 1.0000 12.000 1.2246 0.02478 0.01803 0.0175 0.0236 1.0000 12.250 1.2278 0.02600 0.01930 0.0197 0.0227 1.0000 12.500 1.2338 0.02714 0.02053 0.0215 0.0221 1.0000 12.750 1.2398 0.02839 0.02184 0.0232 0.0212 1.0000 13.000 1.2452 0.02975 0.02328 0.0246 0.0204 1.0000 13.250 1.2495 0.03130 0.02489 0.0259 0.0198 1.0000 13.500 1.2532 0.03298 0.02662 0.0271 0.0191 1.0000 13.750 1.2543 0.03497 0.02867 0.0281 0.0186 1.0000 14.000 1.2584 0.03677 0.03055 0.0289 0.0180 1.0000 14.250 1.2613 0.03872 0.03259 0.0297 0.0175 1.0000 14.500 1.2632 0.04083 0.03478 0.0303 0.0170 1.0000 14.750 1.2656 0.04295 0.03699 0.0307 0.0165 1.0000 15.000 1.2672 0.04520 0.03928 0.0311 0.0158 1.0000 15.250 1.2651 0.04791 0.04207 0.0313 0.0155 1.0000 15.500 1.2634 0.05065 0.04489 0.0314 0.0152 1.0000 15.750 1.2614 0.05351 0.04782 0.0314 0.0147 1.0000 16.000 1.2596 0.05646 0.05087 0.0312 0.0144 1.0000 16.250 1.2569 0.05959 0.05410 0.0308 0.0142 1.0000 16.500 1.2539 0.06284 0.05745 0.0304 0.0139 1.0000 16.750 1.2506 0.06620 0.06090 0.0298 0.0136 1.0000 17.000 1.2471 0.06968 0.06448 0.0291 0.0134 1.0000 17.250 1.2428 0.07336 0.06824 0.0282 0.0131 1.0000 17.500 1.2373 0.07725 0.07223 0.0272 0.0129 1.0000 17.750 1.2320 0.08121 0.07628 0.0261 0.0127 1.0000 18.000 1.2243 0.08559 0.08076 0.0247 0.0126 1.0000 18.250 1.2167 0.09003 0.08528 0.0233 0.0123 1.0000 18.500 1.2083 0.09467 0.09000 0.0217 0.0121 1.0000 18.750 1.1989 0.09955 0.09497 0.0200 0.0120 1.0000