XFOIL Version 6.96 Calculated polar for: DEFIANT CANARD BL20 AIRFOIL 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 ------ -------- --------- --------- -------- -------- -------- -17.500 -0.6243 0.08592 0.08076 -0.0893 0.7025 0.0206 -17.250 -0.6439 0.07968 0.07440 -0.0927 0.6981 0.0208 -17.000 -0.6647 0.07346 0.06805 -0.0960 0.6936 0.0207 -16.750 -0.6855 0.06744 0.06189 -0.0992 0.6892 0.0209 -16.500 -0.7029 0.06213 0.05645 -0.1020 0.6845 0.0210 -16.250 -0.7241 0.05665 0.05086 -0.1048 0.6810 0.0213 -16.000 -0.7420 0.05183 0.04593 -0.1070 0.6764 0.0215 -15.750 -0.7560 0.04765 0.04164 -0.1088 0.6717 0.0217 -15.500 -0.7681 0.04381 0.03769 -0.1103 0.6669 0.0221 -15.250 -0.7767 0.04043 0.03419 -0.1115 0.6629 0.0221 -15.000 -0.7830 0.03732 0.03100 -0.1125 0.6588 0.0227 -14.750 -0.7862 0.03459 0.02818 -0.1132 0.6544 0.0231 -14.500 -0.7887 0.03208 0.02556 -0.1136 0.6499 0.0236 -14.250 -0.7893 0.02996 0.02332 -0.1136 0.6455 0.0240 -14.000 -0.7904 0.02799 0.02127 -0.1132 0.6417 0.0245 -13.750 -0.7905 0.02632 0.01953 -0.1123 0.6373 0.0252 -13.500 -0.7887 0.02497 0.01811 -0.1109 0.6329 0.0259 -13.250 -0.7849 0.02387 0.01693 -0.1092 0.6288 0.0266 -13.000 -0.7799 0.02294 0.01591 -0.1072 0.6250 0.0276 -12.750 -0.7750 0.02205 0.01497 -0.1050 0.6216 0.0286 -12.500 -0.7677 0.02130 0.01417 -0.1027 0.6180 0.0297 -12.000 -0.7510 0.02000 0.01278 -0.0977 0.6101 0.0328 -11.750 -0.7410 0.01946 0.01219 -0.0952 0.6062 0.0346 -11.500 -0.7320 0.01896 0.01164 -0.0923 0.6027 0.0369 -11.250 -0.7203 0.01855 0.01120 -0.0898 0.5998 0.0393 -11.000 -0.7064 0.01808 0.01072 -0.0877 0.5966 0.0424 -10.750 -0.6902 0.01764 0.01026 -0.0859 0.5931 0.0456 -10.500 -0.6727 0.01724 0.00982 -0.0843 0.5895 0.0493 -10.000 -0.6352 0.01649 0.00901 -0.0814 0.5823 0.0577 -9.750 -0.6149 0.01612 0.00865 -0.0802 0.5793 0.0623 -9.500 -0.5937 0.01579 0.00833 -0.0791 0.5762 0.0672 -9.250 -0.5716 0.01551 0.00803 -0.0781 0.5729 0.0722 -9.000 -0.5488 0.01525 0.00776 -0.0771 0.5696 0.0773 -8.750 -0.5257 0.01503 0.00752 -0.0763 0.5662 0.0818 -8.500 -0.5017 0.01485 0.00728 -0.0755 0.5629 0.0863 -8.250 -0.4773 0.01464 0.00708 -0.0748 0.5599 0.0904 -8.000 -0.4521 0.01448 0.00688 -0.0742 0.5568 0.0941 -7.750 -0.4276 0.01428 0.00668 -0.0736 0.5537 0.0973 -7.500 -0.4024 0.01413 0.00649 -0.0730 0.5506 0.1007 -7.250 -0.3768 0.01401 0.00631 -0.0724 0.5474 0.1040 -7.000 -0.3521 0.01386 0.00615 -0.0718 0.5442 0.1081 -6.750 -0.3257 0.01374 0.00601 -0.0714 0.5413 0.1120 -6.500 -0.2999 0.01358 0.00583 -0.0709 0.5384 0.1148 -6.250 -0.2746 0.01340 0.00565 -0.0704 0.5354 0.1175 -6.000 -0.2489 0.01326 0.00548 -0.0698 0.5325 0.1201 -5.750 -0.2228 0.01315 0.00531 -0.0694 0.5294 0.1226 -5.500 -0.1966 0.01307 0.00516 -0.0689 0.5262 0.1246 -5.250 -0.1712 0.01289 0.00498 -0.0684 0.5234 0.1272 -5.000 -0.1452 0.01273 0.00483 -0.0679 0.5207 0.1300 -4.750 -0.1189 0.01260 0.00469 -0.0675 0.5179 0.1328 -4.500 -0.0923 0.01250 0.00455 -0.0671 0.5149 0.1355 -4.250 -0.0660 0.01239 0.00442 -0.0667 0.5119 0.1383 -4.000 -0.0403 0.01227 0.00427 -0.0662 0.5088 0.1418 -3.750 -0.0141 0.01217 0.00415 -0.0658 0.5059 0.1454 -3.500 0.0129 0.01207 0.00406 -0.0655 0.5034 0.1492 -3.250 0.0394 0.01195 0.00395 -0.0651 0.5008 0.1540 -3.000 0.0659 0.01184 0.00385 -0.0648 0.4978 0.1598 -2.750 0.0923 0.01174 0.00376 -0.0644 0.4947 0.1671 -2.500 0.1183 0.01164 0.00366 -0.0640 0.4916 0.1782 -2.250 0.1440 0.01153 0.00358 -0.0635 0.4888 0.1936 -2.000 0.1701 0.01137 0.00351 -0.0631 0.4864 0.2148 -1.750 0.1959 0.01120 0.00345 -0.0627 0.4837 0.2428 -1.500 0.2216 0.01105 0.00341 -0.0622 0.4806 0.2717 -1.250 0.2474 0.01094 0.00338 -0.0618 0.4775 0.3001 -1.000 0.2734 0.01087 0.00337 -0.0614 0.4746 0.3250 -0.750 0.2994 0.01084 0.00337 -0.0610 0.4718 0.3456 -0.500 0.3260 0.01082 0.00338 -0.0606 0.4692 0.3626 -0.250 0.3529 0.01079 0.00340 -0.0604 0.4663 0.3774 0.000 0.3798 0.01078 0.00342 -0.0601 0.4632 0.3899 0.250 0.4065 0.01079 0.00344 -0.0598 0.4603 0.4027 0.500 0.4328 0.01080 0.00347 -0.0594 0.4573 0.4144 0.750 0.4591 0.01085 0.00350 -0.0590 0.4541 0.4256 1.000 0.4854 0.01086 0.00354 -0.0587 0.4514 0.4369 1.250 0.5121 0.01087 0.00360 -0.0584 0.4487 0.4504 1.500 0.5383 0.01088 0.00365 -0.0580 0.4457 0.4648 1.750 0.5642 0.01091 0.00371 -0.0576 0.4424 0.4767 2.000 0.5898 0.01096 0.00376 -0.0571 0.4391 0.4886 2.250 0.6148 0.01101 0.00382 -0.0566 0.4361 0.5003 2.750 0.6662 0.01105 0.00396 -0.0557 0.4305 0.5274 3.000 0.6910 0.01106 0.00404 -0.0551 0.4271 0.5439 3.250 0.7153 0.01109 0.00411 -0.0544 0.4238 0.5606 3.500 0.7386 0.01112 0.00420 -0.0536 0.4208 0.5815 3.750 0.7610 0.01114 0.00430 -0.0526 0.4178 0.6110 4.000 0.7832 0.01108 0.00442 -0.0515 0.4149 0.6549 4.250 0.8031 0.01099 0.00454 -0.0499 0.4117 0.7174 4.500 0.8215 0.01087 0.00469 -0.0479 0.4085 0.7963 4.750 0.8504 0.01086 0.00491 -0.0481 0.4051 0.8781 5.000 0.9083 0.01111 0.00520 -0.0545 0.4009 0.9288 5.250 0.9637 0.01133 0.00544 -0.0603 0.3970 0.9505 5.500 1.0040 0.01153 0.00563 -0.0631 0.3931 0.9641 5.750 1.0394 0.01174 0.00583 -0.0649 0.3892 0.9739 6.000 1.0711 0.01199 0.00604 -0.0660 0.3854 0.9832 6.250 1.1040 0.01219 0.00625 -0.0673 0.3820 0.9909 6.500 1.1372 0.01241 0.00647 -0.0687 0.3783 0.9973 6.750 1.1684 0.01264 0.00670 -0.0698 0.3744 1.0000 7.000 1.1818 0.01286 0.00690 -0.0672 0.3709 1.0000 7.250 1.1949 0.01309 0.00711 -0.0647 0.3675 1.0000 7.500 1.2088 0.01328 0.00732 -0.0622 0.3643 1.0000 7.750 1.2189 0.01347 0.00753 -0.0590 0.3610 1.0000 8.000 1.2283 0.01372 0.00777 -0.0558 0.3574 1.0000 8.250 1.2372 0.01404 0.00807 -0.0527 0.3538 1.0000 8.500 1.2493 0.01436 0.00840 -0.0503 0.3506 1.0000 8.750 1.2635 0.01467 0.00874 -0.0483 0.3472 1.0000 9.000 1.2766 0.01505 0.00914 -0.0462 0.3437 1.0000 9.250 1.2879 0.01554 0.00963 -0.0440 0.3400 1.0000 9.500 1.2971 0.01616 0.01023 -0.0418 0.3362 1.0000 9.750 1.3117 0.01665 0.01078 -0.0403 0.3330 1.0000 10.000 1.3245 0.01728 0.01143 -0.0389 0.3291 1.0000 10.250 1.3357 0.01804 0.01221 -0.0373 0.3253 1.0000 10.500 1.3443 0.01902 0.01319 -0.0358 0.3215 1.0000 10.750 1.3559 0.01993 0.01414 -0.0347 0.3178 1.0000 11.000 1.3679 0.02089 0.01514 -0.0338 0.3139 1.0000 11.250 1.3780 0.02204 0.01631 -0.0329 0.3101 1.0000 11.500 1.3854 0.02339 0.01767 -0.0319 0.3063 1.0000 11.750 1.3945 0.02466 0.01897 -0.0311 0.3029 1.0000 12.000 1.4049 0.02588 0.02023 -0.0304 0.2990 1.0000 12.250 1.4126 0.02729 0.02167 -0.0296 0.2952 1.0000 12.500 1.4172 0.02892 0.02332 -0.0287 0.2911 1.0000 12.750 1.4230 0.03048 0.02489 -0.0278 0.2877 1.0000 13.000 1.4313 0.03189 0.02636 -0.0272 0.2842 1.0000 13.250 1.4371 0.03349 0.02800 -0.0265 0.2802 1.0000 13.500 1.4396 0.03537 0.02990 -0.0257 0.2763 1.0000 13.750 1.4430 0.03723 0.03176 -0.0249 0.2724 1.0000 14.000 1.4499 0.03886 0.03346 -0.0244 0.2690 1.0000 14.250 1.4553 0.04064 0.03527 -0.0239 0.2652 1.0000 14.500 1.4528 0.04315 0.03778 -0.0233 0.2598 1.0000 14.750 1.4573 0.04510 0.03977 -0.0229 0.2554 1.0000 15.000 1.4608 0.04717 0.04189 -0.0225 0.2513 1.0000 15.250 1.4633 0.04934 0.04408 -0.0222 0.2472 1.0000 15.500 1.4626 0.05185 0.04660 -0.0218 0.2428 1.0000 15.750 1.4689 0.05373 0.04853 -0.0216 0.2393 1.0000 16.000 1.4695 0.05619 0.05103 -0.0214 0.2348 1.0000 16.250 1.4707 0.05857 0.05343 -0.0212 0.2311 1.0000 16.500 1.4713 0.06108 0.05598 -0.0211 0.2268 1.0000 16.750 1.4726 0.06356 0.05850 -0.0210 0.2220 1.0000 17.000 1.4720 0.06622 0.06118 -0.0209 0.2179 1.0000 17.250 1.4705 0.06902 0.06400 -0.0209 0.2136 1.0000 17.500 1.4730 0.07142 0.06646 -0.0209 0.2092 1.0000 17.750 1.4686 0.07461 0.06968 -0.0210 0.2043 1.0000 18.000 1.4671 0.07746 0.07254 -0.0211 0.1999 1.0000 18.250 1.4660 0.08035 0.07548 -0.0214 0.1952 1.0000 18.500 1.4616 0.08360 0.07875 -0.0216 0.1900 1.0000 18.750 1.4592 0.08667 0.08185 -0.0219 0.1859 1.0000 19.000 1.4593 0.08945 0.08468 -0.0222 0.1818 1.0000 19.250 1.4555 0.09270 0.08796 -0.0226 0.1772 1.0000