XFOIL Version 6.96 Calculated polar for: NASA SC(2)-0614 AIRFOIL 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 ------ -------- --------- --------- -------- -------- -------- -16.750 -0.9142 0.09122 0.08596 -0.0521 1.0000 0.0346 -16.500 -0.9533 0.08016 0.07460 -0.0590 1.0000 0.0347 -16.250 -0.9745 0.07312 0.06733 -0.0629 1.0000 0.0348 -16.000 -0.9892 0.06757 0.06158 -0.0657 1.0000 0.0351 -15.750 -1.0000 0.06294 0.05676 -0.0677 1.0000 0.0354 -15.500 -1.0081 0.05892 0.05256 -0.0692 1.0000 0.0357 -15.250 -1.0142 0.05542 0.04887 -0.0701 1.0000 0.0361 -15.000 -1.0179 0.05230 0.04557 -0.0706 1.0000 0.0365 -14.750 -1.0199 0.04948 0.04256 -0.0708 1.0000 0.0369 -14.500 -1.0196 0.04699 0.03988 -0.0708 1.0000 0.0373 -14.250 -1.0139 0.04521 0.03808 -0.0705 1.0000 0.0377 -14.000 -1.0081 0.04354 0.03637 -0.0702 1.0000 0.0382 -13.750 -1.0021 0.04196 0.03474 -0.0697 1.0000 0.0387 -13.500 -0.9961 0.04046 0.03318 -0.0689 1.0000 0.0393 -13.250 -0.9903 0.03902 0.03166 -0.0680 1.0000 0.0400 -13.000 -0.9847 0.03764 0.03019 -0.0668 1.0000 0.0407 -12.750 -0.9793 0.03634 0.02878 -0.0652 1.0000 0.0415 -12.500 -0.9741 0.03513 0.02743 -0.0634 1.0000 0.0422 -12.250 -0.9693 0.03403 0.02628 -0.0613 1.0000 0.0428 -12.000 -0.9666 0.03309 0.02534 -0.0588 1.0000 0.0433 -11.750 -0.9667 0.03226 0.02450 -0.0557 1.0000 0.0439 -11.500 -0.9673 0.03147 0.02370 -0.0523 1.0000 0.0445 -11.250 -0.9624 0.03062 0.02281 -0.0500 1.0000 0.0452 -11.000 -0.9554 0.02978 0.02191 -0.0479 1.0000 0.0462 -10.750 -0.9462 0.02896 0.02102 -0.0461 1.0000 0.0473 -10.500 -0.9350 0.02816 0.02013 -0.0445 1.0000 0.0485 -10.250 -0.9168 0.02728 0.01928 -0.0444 0.9991 0.0498 -10.000 -0.8876 0.02643 0.01840 -0.0463 0.9967 0.0515 -9.750 -0.8579 0.02563 0.01753 -0.0480 0.9944 0.0535 -9.500 -0.8277 0.02482 0.01666 -0.0497 0.9923 0.0555 -9.250 -0.7988 0.02403 0.01588 -0.0513 0.9893 0.0573 -9.000 -0.7684 0.02337 0.01519 -0.0530 0.9865 0.0598 -8.750 -0.7371 0.02274 0.01449 -0.0546 0.9841 0.0625 -8.500 -0.7049 0.02204 0.01383 -0.0567 0.9821 0.0652 -8.250 -0.6718 0.02146 0.01321 -0.0588 0.9803 0.0683 -8.000 -0.6436 0.02089 0.01261 -0.0597 0.9764 0.0712 -7.750 -0.6123 0.02027 0.01203 -0.0614 0.9734 0.0746 -7.500 -0.5796 0.01978 0.01151 -0.0632 0.9711 0.0786 -7.250 -0.5456 0.01919 0.01096 -0.0654 0.9693 0.0828 -7.000 -0.5103 0.01870 0.01047 -0.0677 0.9678 0.0879 -6.750 -0.4805 0.01821 0.01000 -0.0689 0.9639 0.0930 -6.500 -0.4483 0.01774 0.00955 -0.0705 0.9607 0.0994 -6.250 -0.4140 0.01724 0.00910 -0.0726 0.9584 0.1072 -6.000 -0.3785 0.01678 0.00869 -0.0749 0.9565 0.1171 -5.750 -0.3417 0.01630 0.00828 -0.0775 0.9551 0.1315 -5.500 -0.3037 0.01577 0.00787 -0.0804 0.9539 0.1521 -5.250 -0.2669 0.01523 0.00749 -0.0831 0.9519 0.1821 -5.000 -0.2339 0.01466 0.00714 -0.0851 0.9479 0.2263 -4.750 -0.1940 0.01387 0.00672 -0.0889 0.9461 0.2988 -4.500 -0.1510 0.01298 0.00636 -0.0935 0.9450 0.4046 -4.250 -0.1147 0.01270 0.00658 -0.0955 0.9431 0.5084 -4.000 -0.0817 0.01281 0.00685 -0.0962 0.9409 0.5507 -3.750 -0.0451 0.01285 0.00686 -0.0979 0.9391 0.5777 -3.500 -0.0132 0.01295 0.00696 -0.0986 0.9359 0.5930 -3.250 0.0147 0.01311 0.00713 -0.0984 0.9311 0.6037 -3.000 0.0468 0.01325 0.00727 -0.0990 0.9280 0.6165 -2.750 0.0808 0.01338 0.00738 -0.1001 0.9256 0.6289 -2.500 0.1109 0.01362 0.00768 -0.0999 0.9232 0.6357 -2.250 0.1414 0.01381 0.00786 -0.1002 0.9190 0.6467 -2.000 0.1649 0.01416 0.00828 -0.0985 0.9134 0.6522 -1.750 0.1980 0.01418 0.00829 -0.0994 0.9099 0.6579 -1.500 0.2349 0.01405 0.00814 -0.1012 0.9070 0.6629 -1.250 0.2602 0.01415 0.00829 -0.1001 0.8992 0.6654 -1.000 0.2923 0.01403 0.00819 -0.1004 0.8921 0.6682 -0.750 0.3231 0.01382 0.00798 -0.1005 0.8800 0.6710 -0.500 0.3566 0.01352 0.00763 -0.1012 0.8655 0.6738 -0.250 0.3914 0.01320 0.00724 -0.1023 0.8472 0.6777 0.000 0.4197 0.01309 0.00711 -0.1017 0.8276 0.6791 0.250 0.4479 0.01303 0.00704 -0.1012 0.8069 0.6807 0.500 0.4768 0.01299 0.00696 -0.1009 0.7853 0.6824 0.750 0.5055 0.01297 0.00687 -0.1006 0.7553 0.6842 1.000 0.5339 0.01300 0.00675 -0.1002 0.7065 0.6861 1.250 0.5585 0.01335 0.00659 -0.0991 0.5991 0.6883 1.500 0.5773 0.01427 0.00675 -0.0974 0.4631 0.6909 1.750 0.5995 0.01507 0.00702 -0.0967 0.3646 0.6937 2.000 0.6204 0.01578 0.00738 -0.0954 0.2877 0.6951 2.250 0.6433 0.01638 0.00770 -0.0946 0.2331 0.6966 2.500 0.6675 0.01688 0.00800 -0.0940 0.1934 0.6981 3.000 0.7186 0.01774 0.00859 -0.0934 0.1427 0.7018 3.250 0.7452 0.01811 0.00889 -0.0932 0.1264 0.7040 3.500 0.7723 0.01849 0.00918 -0.0933 0.1135 0.7064 3.750 0.8000 0.01889 0.00949 -0.0935 0.1036 0.7090 4.000 0.8254 0.01925 0.00986 -0.0930 0.0967 0.7104 4.250 0.8493 0.01972 0.01028 -0.0923 0.0909 0.7118 4.500 0.8742 0.02009 0.01071 -0.0916 0.0859 0.7134 4.750 0.8983 0.02056 0.01116 -0.0910 0.0815 0.7153 5.000 0.9228 0.02102 0.01163 -0.0904 0.0778 0.7175 5.250 0.9479 0.02146 0.01209 -0.0899 0.0741 0.7200 5.500 0.9722 0.02202 0.01260 -0.0895 0.0711 0.7226 5.750 0.9982 0.02248 0.01310 -0.0893 0.0683 0.7255 6.000 1.0210 0.02296 0.01363 -0.0883 0.0657 0.7271 6.250 1.0433 0.02351 0.01419 -0.0874 0.0634 0.7287 6.500 1.0658 0.02409 0.01481 -0.0864 0.0612 0.7305 6.750 1.0889 0.02462 0.01541 -0.0856 0.0590 0.7325 7.000 1.1116 0.02518 0.01600 -0.0848 0.0570 0.7347 7.250 1.1334 0.02585 0.01666 -0.0840 0.0554 0.7371 7.500 1.1563 0.02653 0.01740 -0.0832 0.0538 0.7397 7.750 1.1787 0.02719 0.01813 -0.0824 0.0519 0.7422 8.000 1.1986 0.02782 0.01883 -0.0811 0.0504 0.7440 8.250 1.2175 0.02853 0.01956 -0.0797 0.0490 0.7460 8.500 1.2368 0.02934 0.02045 -0.0784 0.0477 0.7482 8.750 1.2563 0.03014 0.02138 -0.0772 0.0463 0.7506 9.000 1.2752 0.03097 0.02229 -0.0759 0.0451 0.7531 9.250 1.2931 0.03180 0.02317 -0.0745 0.0441 0.7557 9.500 1.3091 0.03266 0.02405 -0.0729 0.0433 0.7585 9.750 1.3218 0.03363 0.02506 -0.0706 0.0425 0.7602 10.000 1.3365 0.03465 0.02628 -0.0687 0.0416 0.7622 10.250 1.3506 0.03572 0.02752 -0.0668 0.0406 0.7644 10.500 1.3641 0.03680 0.02872 -0.0650 0.0397 0.7671 10.750 1.3770 0.03789 0.02992 -0.0632 0.0389 0.7700 11.000 1.3893 0.03902 0.03111 -0.0615 0.0382 0.7731 11.250 1.4008 0.04023 0.03238 -0.0598 0.0377 0.7757 11.500 1.4104 0.04161 0.03381 -0.0578 0.0372 0.7776 11.750 1.4180 0.04329 0.03574 -0.0557 0.0367 0.7797 12.000 1.4243 0.04510 0.03778 -0.0537 0.0361 0.7820 12.250 1.4292 0.04703 0.03992 -0.0517 0.0356 0.7844 12.500 1.4327 0.04909 0.04217 -0.0499 0.0351 0.7870 12.750 1.4350 0.05128 0.04454 -0.0483 0.0347 0.7897 13.000 1.4361 0.05360 0.04702 -0.0468 0.0343 0.7922 13.250 1.4357 0.05600 0.04959 -0.0453 0.0339 0.7941 13.500 1.4345 0.05854 0.05228 -0.0441 0.0336 0.7962 13.750 1.4327 0.06124 0.05512 -0.0432 0.0333 0.7984 14.000 1.4301 0.06416 0.05816 -0.0426 0.0330 0.8008 14.250 1.4271 0.06725 0.06136 -0.0424 0.0328 0.8034 14.500 1.4225 0.07071 0.06492 -0.0425 0.0325 0.8060 14.750 1.4094 0.07557 0.07000 -0.0433 0.0323 0.8084 15.000 1.3882 0.08184 0.07659 -0.0453 0.0321 0.8099 15.250 1.3632 0.08943 0.08449 -0.0487 0.0320 0.8113 15.500 1.3326 0.09895 0.09433 -0.0542 0.0319 0.8125 15.750 1.2898 0.11216 0.10790 -0.0631 0.0319 0.8131