XFOIL Version 6.96 Calculated polar for: NACA 63(3)-618 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -17.250 -0.6652 0.10265 0.09802 -0.0671 1.0000 0.0263 -17.000 -0.7052 0.09128 0.08638 -0.0739 1.0000 0.0264 -16.750 -0.7357 0.08237 0.07720 -0.0793 1.0000 0.0266 -16.500 -0.7434 0.07779 0.07254 -0.0818 1.0000 0.0269 -16.250 -0.7495 0.07362 0.06829 -0.0839 1.0000 0.0271 -16.000 -0.7526 0.07003 0.06465 -0.0857 1.0000 0.0275 -15.750 -0.7578 0.06626 0.06080 -0.0875 1.0000 0.0279 -15.500 -0.7630 0.06265 0.05709 -0.0892 1.0000 0.0283 -15.250 -0.7680 0.05923 0.05354 -0.0905 1.0000 0.0287 -15.000 -0.7730 0.05598 0.05016 -0.0917 1.0000 0.0294 -14.750 -0.7783 0.05287 0.04688 -0.0925 1.0000 0.0301 -14.500 -0.7827 0.05002 0.04383 -0.0929 1.0000 0.0307 -14.250 -0.7807 0.04803 0.04183 -0.0929 1.0000 0.0312 -14.000 -0.7782 0.04620 0.03998 -0.0927 1.0000 0.0317 -13.750 -0.7763 0.04442 0.03817 -0.0923 1.0000 0.0322 -13.500 -0.7749 0.04271 0.03641 -0.0917 1.0000 0.0329 -13.250 -0.7750 0.04109 0.03472 -0.0908 1.0000 0.0337 -12.750 -0.7509 0.03745 0.03085 -0.0929 0.9834 0.0357 -12.500 -0.7275 0.03582 0.02920 -0.0957 0.9718 0.0368 -12.250 -0.7022 0.03422 0.02751 -0.0987 0.9605 0.0381 -12.000 -0.6753 0.03267 0.02581 -0.1016 0.9492 0.0397 -11.750 -0.6466 0.03120 0.02424 -0.1046 0.9387 0.0412 -11.500 -0.6189 0.02989 0.02287 -0.1074 0.9265 0.0427 -11.250 -0.5923 0.02870 0.02157 -0.1096 0.9143 0.0444 -11.000 -0.5668 0.02764 0.02033 -0.1112 0.9025 0.0461 -10.750 -0.5471 0.02657 0.01924 -0.1119 0.8899 0.0475 -10.500 -0.5302 0.02567 0.01828 -0.1119 0.8777 0.0491 -10.250 -0.5133 0.02484 0.01734 -0.1117 0.8669 0.0509 -10.000 -0.4986 0.02409 0.01647 -0.1108 0.8558 0.0523 -9.750 -0.4870 0.02322 0.01556 -0.1097 0.8460 0.0539 -9.500 -0.4762 0.02248 0.01477 -0.1083 0.8361 0.0554 -9.250 -0.4656 0.02184 0.01406 -0.1067 0.8274 0.0571 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0.4479 -4.250 -0.0101 0.01276 0.00544 -0.1031 0.7028 0.4695 -4.000 0.0187 0.01277 0.00542 -0.1033 0.6975 0.4865 -3.750 0.0471 0.01279 0.00542 -0.1034 0.6917 0.4999 -3.500 0.0758 0.01280 0.00538 -0.1035 0.6867 0.5100 -3.250 0.1053 0.01283 0.00529 -0.1038 0.6824 0.5212 -3.000 0.1331 0.01287 0.00537 -0.1038 0.6768 0.5313 -2.750 0.1622 0.01290 0.00532 -0.1041 0.6715 0.5413 -2.500 0.1907 0.01291 0.00529 -0.1041 0.6668 0.5469 -2.250 0.2196 0.01293 0.00526 -0.1043 0.6621 0.5534 -2.000 0.2485 0.01294 0.00522 -0.1046 0.6569 0.5599 -1.750 0.2768 0.01296 0.00523 -0.1047 0.6521 0.5648 -1.500 0.3059 0.01299 0.00519 -0.1049 0.6479 0.5707 -1.250 0.3349 0.01302 0.00517 -0.1052 0.6428 0.5769 -1.000 0.3629 0.01304 0.00521 -0.1053 0.6376 0.5816 -0.750 0.3914 0.01307 0.00522 -0.1054 0.6332 0.5864 -0.500 0.4207 0.01312 0.00520 -0.1058 0.6294 0.5920 -0.250 0.4495 0.01317 0.00523 -0.1061 0.6246 0.5975 0.000 0.4772 0.01320 0.00531 -0.1061 0.6195 0.6014 0.250 0.5057 0.01325 0.00534 -0.1062 0.6150 0.6062 0.500 0.5349 0.01332 0.00534 -0.1065 0.6112 0.6120 0.750 0.5632 0.01339 0.00544 -0.1068 0.6066 0.6172 1.000 0.5908 0.01346 0.00556 -0.1068 0.6019 0.6214 1.250 0.6191 0.01353 0.00563 -0.1069 0.5976 0.6263 1.500 0.6482 0.01361 0.00566 -0.1072 0.5937 0.6319 1.750 0.6759 0.01370 0.00580 -0.1073 0.5890 0.6372 2.000 0.7032 0.01380 0.00596 -0.1073 0.5844 0.6421 2.250 0.7313 0.01389 0.00607 -0.1074 0.5801 0.6476 2.500 0.7603 0.01400 0.00612 -0.1078 0.5762 0.6534 2.750 0.7872 0.01411 0.00632 -0.1077 0.5715 0.6581 3.000 0.8141 0.01423 0.00651 -0.1076 0.5666 0.6634 3.250 0.8419 0.01434 0.00663 -0.1077 0.5620 0.6698 3.750 0.8961 0.01460 0.00699 -0.1076 0.5528 0.6806 4.000 0.9228 0.01474 0.00719 -0.1076 0.5477 0.6866 4.250 0.9507 0.01487 0.00733 -0.1077 0.5432 0.6933 4.500 0.9772 0.01502 0.00753 -0.1075 0.5388 0.6986 4.750 1.0027 0.01518 0.00780 -0.1072 0.5334 0.7050 5.000 1.0294 0.01534 0.00800 -0.1072 0.5281 0.7118 5.250 1.0559 0.01548 0.00816 -0.1070 0.5234 0.7173 5.500 1.0799 0.01565 0.00847 -0.1065 0.5169 0.7240 5.750 1.1052 0.01581 0.00867 -0.1061 0.5101 0.7313 6.000 1.1291 0.01596 0.00888 -0.1055 0.5031 0.7371 6.250 1.1521 0.01613 0.00914 -0.1048 0.4946 0.7442 6.500 1.1763 0.01631 0.00934 -0.1042 0.4873 0.7513 6.750 1.1974 0.01650 0.00966 -0.1032 0.4785 0.7582 7.000 1.2201 0.01671 0.00988 -0.1024 0.4699 0.7660 7.250 1.2398 0.01692 0.01022 -0.1011 0.4601 0.7729 7.500 1.2597 0.01717 0.01052 -0.0999 0.4506 0.7810 7.750 1.2774 0.01744 0.01083 -0.0983 0.4389 0.7890 8.000 1.2915 0.01775 0.01120 -0.0961 0.4240 0.7975 8.250 1.3004 0.01813 0.01157 -0.0931 0.4061 0.8066 8.500 1.3061 0.01864 0.01207 -0.0896 0.3858 0.8165 8.750 1.3111 0.01929 0.01270 -0.0863 0.3634 0.8272 9.000 1.3142 0.02012 0.01349 -0.0829 0.3415 0.8393 9.250 1.3147 0.02110 0.01443 -0.0794 0.3210 0.8525 9.500 1.3145 0.02220 0.01551 -0.0760 0.3004 0.8680 9.750 1.3120 0.02347 0.01676 -0.0726 0.2802 0.8882 10.000 1.3073 0.02482 0.01810 -0.0690 0.2609 0.9232 10.250 1.3039 0.02645 0.01968 -0.0664 0.2412 1.0000 10.500 1.3048 0.02839 0.02155 -0.0648 0.2208 1.0000 10.750 1.3048 0.03049 0.02357 -0.0633 0.2015 1.0000 11.000 1.3049 0.03267 0.02568 -0.0620 0.1842 1.0000 11.250 1.3048 0.03496 0.02791 -0.0608 0.1679 1.0000 11.500 1.3051 0.03728 0.03019 -0.0598 0.1533 1.0000 11.750 1.3059 0.03966 0.03253 -0.0590 0.1399 1.0000 12.000 1.3070 0.04209 0.03495 -0.0583 0.1277 1.0000 12.250 1.3080 0.04462 0.03746 -0.0577 0.1162 1.0000 12.500 1.3090 0.04724 0.04006 -0.0572 0.1059 1.0000 12.750 1.3097 0.04997 0.04277 -0.0568 0.0961 1.0000 13.000 1.3117 0.05263 0.04543 -0.0566 0.0872 1.0000 13.250 1.3136 0.05539 0.04820 -0.0565 0.0793 1.0000 13.500 1.3151 0.05825 0.05108 -0.0564 0.0729 1.0000 13.750 1.3165 0.06119 0.05404 -0.0565 0.0674 1.0000 14.000 1.3192 0.06405 0.05695 -0.0566 0.0626 1.0000 14.500 1.3229 0.07014 0.06312 -0.0572 0.0550 1.0000 14.750 1.3233 0.07345 0.06646 -0.0577 0.0520 1.0000 15.000 1.3260 0.07652 0.06961 -0.0581 0.0492 1.0000 15.250 1.3277 0.07977 0.07292 -0.0587 0.0467 1.0000 15.500 1.3278 0.08330 0.07648 -0.0594 0.0447 1.0000 15.750 1.3315 0.08638 0.07966 -0.0601 0.0425 1.0000 16.000 1.3327 0.08984 0.08317 -0.0610 0.0407 1.0000 16.250 1.3320 0.09361 0.08697 -0.0620 0.0393 1.0000 16.500 1.3353 0.09685 0.09034 -0.0628 0.0378 1.0000 16.750 1.3374 0.10029 0.09386 -0.0639 0.0365 1.0000 17.000 1.3384 0.10392 0.09757 -0.0650 0.0354 1.0000