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 = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.750 -1.0726 0.11154 0.10754 -0.0362 1.0000 0.0236 -19.500 -1.0931 0.10386 0.09971 -0.0405 1.0000 0.0237 -19.250 -1.1110 0.09680 0.09250 -0.0443 1.0000 0.0238 -19.000 -1.1263 0.09033 0.08590 -0.0478 1.0000 0.0238 -18.750 -1.1388 0.08444 0.07986 -0.0509 1.0000 0.0240 -18.500 -1.1491 0.07904 0.07433 -0.0538 1.0000 0.0241 -18.250 -1.1570 0.07414 0.06930 -0.0563 1.0000 0.0242 -18.000 -1.1630 0.06963 0.06467 -0.0585 1.0000 0.0243 -17.750 -1.1693 0.06529 0.06024 -0.0605 1.0000 0.0244 -17.500 -1.1740 0.06131 0.05617 -0.0622 1.0000 0.0246 -17.250 -1.1765 0.05772 0.05249 -0.0637 1.0000 0.0248 -17.000 -1.1772 0.05450 0.04919 -0.0649 1.0000 0.0250 -16.750 -1.1763 0.05157 0.04619 -0.0658 1.0000 0.0252 -16.500 -1.1738 0.04893 0.04347 -0.0666 1.0000 0.0255 -16.250 -1.1701 0.04652 0.04098 -0.0672 1.0000 0.0257 -16.000 -1.1655 0.04428 0.03867 -0.0676 1.0000 0.0260 -15.750 -1.1596 0.04226 0.03658 -0.0678 1.0000 0.0262 -15.500 -1.1531 0.04039 0.03464 -0.0679 1.0000 0.0266 -15.250 -1.1462 0.03865 0.03282 -0.0679 1.0000 0.0269 -15.000 -1.1383 0.03704 0.03114 -0.0677 1.0000 0.0273 -14.750 -1.1298 0.03554 0.02957 -0.0674 1.0000 0.0276 -14.500 -1.1208 0.03415 0.02810 -0.0669 1.0000 0.0280 -14.250 -1.1121 0.03281 0.02669 -0.0663 1.0000 0.0283 -14.000 -1.1059 0.03137 0.02522 -0.0655 1.0000 0.0287 -13.750 -1.0988 0.03014 0.02396 -0.0644 1.0000 0.0290 -13.500 -1.0922 0.02904 0.02284 -0.0629 1.0000 0.0294 -13.250 -1.0865 0.02805 0.02182 -0.0611 1.0000 0.0298 -13.000 -1.0828 0.02715 0.02089 -0.0588 1.0000 0.0302 -12.750 -1.0831 0.02634 0.02005 -0.0556 1.0000 0.0306 -12.500 -1.0907 0.02564 0.01931 -0.0510 1.0000 0.0309 -12.250 -1.0692 0.02469 0.01832 -0.0518 0.9979 0.0315 -12.000 -1.0425 0.02378 0.01735 -0.0535 0.9956 0.0322 -11.750 -1.0152 0.02285 0.01638 -0.0553 0.9936 0.0330 -11.500 -0.9883 0.02201 0.01554 -0.0569 0.9916 0.0340 -11.250 -0.9614 0.02128 0.01479 -0.0583 0.9889 0.0351 -11.000 -0.9326 0.02059 0.01406 -0.0599 0.9865 0.0363 -10.750 -0.9022 0.01990 0.01333 -0.0618 0.9845 0.0375 -10.500 -0.8709 0.01920 0.01265 -0.0639 0.9829 0.0389 -10.250 -0.8385 0.01860 0.01203 -0.0660 0.9817 0.0404 -10.000 -0.8053 0.01804 0.01144 -0.0682 0.9807 0.0420 -9.750 -0.7777 0.01747 0.01086 -0.0692 0.9769 0.0435 -9.500 -0.7464 0.01694 0.01033 -0.0709 0.9744 0.0454 -9.250 -0.7138 0.01647 0.00984 -0.0727 0.9724 0.0475 -9.000 -0.6808 0.01597 0.00933 -0.0747 0.9707 0.0495 -8.750 -0.6472 0.01548 0.00885 -0.0767 0.9691 0.0518 -8.500 -0.6132 0.01506 0.00841 -0.0787 0.9677 0.0540 -8.250 -0.5833 0.01465 0.00800 -0.0798 0.9641 0.0560 -8.000 -0.5522 0.01424 0.00761 -0.0811 0.9610 0.0584 -7.750 -0.5198 0.01390 0.00726 -0.0826 0.9585 0.0611 -7.500 -0.4868 0.01352 0.00690 -0.0842 0.9562 0.0639 -7.250 -0.4532 0.01316 0.00655 -0.0859 0.9542 0.0672 -7.000 -0.4210 0.01288 0.00625 -0.0872 0.9515 0.0702 -6.750 -0.3904 0.01254 0.00595 -0.0882 0.9474 0.0742 -6.500 -0.3586 0.01224 0.00567 -0.0895 0.9440 0.0788 -6.250 -0.3258 0.01191 0.00539 -0.0909 0.9412 0.0847 -6.000 -0.2925 0.01162 0.00512 -0.0924 0.9386 0.0914 -5.750 -0.2608 0.01133 0.00488 -0.0935 0.9348 0.1002 -5.500 -0.2290 0.01104 0.00464 -0.0947 0.9305 0.1108 -5.250 -0.1962 0.01073 0.00441 -0.0961 0.9270 0.1257 -5.000 -0.1629 0.01043 0.00419 -0.0976 0.9241 0.1451 -4.750 -0.1289 0.01006 0.00395 -0.0993 0.9211 0.1722 -4.500 -0.0954 0.00970 0.00375 -0.1010 0.9170 0.2069 -4.250 -0.0608 0.00930 0.00352 -0.1029 0.9130 0.2493 -4.000 -0.0240 0.00880 0.00326 -0.1055 0.9097 0.3132 -3.750 0.0153 0.00816 0.00295 -0.1087 0.9070 0.3978 -3.500 0.0538 0.00765 0.00280 -0.1117 0.9039 0.4898 -3.250 0.0863 0.00753 0.00283 -0.1127 0.8992 0.5325 -3.000 0.1177 0.00750 0.00287 -0.1133 0.8944 0.5598 -2.750 0.1488 0.00751 0.00287 -0.1138 0.8900 0.5770 -2.500 0.1789 0.00753 0.00291 -0.1141 0.8828 0.5887 -2.250 0.2092 0.00754 0.00287 -0.1143 0.8742 0.5973 -2.000 0.2385 0.00757 0.00292 -0.1143 0.8629 0.6056 -1.750 0.2681 0.00761 0.00290 -0.1144 0.8492 0.6147 -1.500 0.2969 0.00768 0.00295 -0.1142 0.8345 0.6218 -1.250 0.3265 0.00776 0.00294 -0.1142 0.8169 0.6288 -1.000 0.3545 0.00784 0.00298 -0.1139 0.7911 0.6335 -0.750 0.3826 0.00797 0.00299 -0.1136 0.7616 0.6370 -0.500 0.4108 0.00812 0.00301 -0.1134 0.7285 0.6403 -0.250 0.4377 0.00839 0.00302 -0.1129 0.6698 0.6434 0.000 0.4603 0.00911 0.00315 -0.1118 0.5464 0.6456 0.250 0.4836 0.00981 0.00340 -0.1110 0.4466 0.6471 0.500 0.5087 0.01036 0.00362 -0.1106 0.3672 0.6484 0.750 0.5343 0.01089 0.00383 -0.1102 0.2961 0.6499 1.000 0.5604 0.01134 0.00404 -0.1099 0.2405 0.6514 1.250 0.5875 0.01170 0.00422 -0.1098 0.2034 0.6531 1.500 0.6148 0.01202 0.00440 -0.1097 0.1724 0.6551 1.750 0.6423 0.01233 0.00458 -0.1096 0.1493 0.6571 2.000 0.6700 0.01260 0.00475 -0.1095 0.1314 0.6589 2.250 0.6977 0.01288 0.00493 -0.1095 0.1146 0.6607 2.500 0.7252 0.01315 0.00512 -0.1094 0.1019 0.6622 2.750 0.7525 0.01340 0.00534 -0.1092 0.0925 0.6636 3.000 0.7799 0.01364 0.00556 -0.1090 0.0855 0.6651 3.250 0.8069 0.01392 0.00580 -0.1088 0.0792 0.6666 3.500 0.8341 0.01418 0.00604 -0.1086 0.0739 0.6683 3.750 0.8611 0.01446 0.00629 -0.1083 0.0696 0.6701 4.000 0.8883 0.01471 0.00653 -0.1081 0.0660 0.6719 4.250 0.9150 0.01502 0.00681 -0.1078 0.0627 0.6738 4.500 0.9420 0.01528 0.00707 -0.1076 0.0603 0.6757 4.750 0.9688 0.01556 0.00733 -0.1073 0.0578 0.6776 5.000 0.9947 0.01588 0.00765 -0.1069 0.0557 0.6791 5.250 1.0207 0.01617 0.00797 -0.1064 0.0540 0.6806 5.500 1.0466 0.01647 0.00830 -0.1060 0.0522 0.6824 5.750 1.0721 0.01681 0.00865 -0.1055 0.0504 0.6846 6.000 1.0970 0.01721 0.00904 -0.1049 0.0486 0.6870 6.250 1.1226 0.01752 0.00938 -0.1044 0.0471 0.6894 6.500 1.1479 0.01786 0.00975 -0.1038 0.0456 0.6916 6.750 1.1727 0.01824 0.01012 -0.1033 0.0441 0.6935 7.000 1.1964 0.01867 0.01056 -0.1025 0.0427 0.6952 7.250 1.2206 0.01904 0.01098 -0.1017 0.0416 0.6969 7.500 1.2445 0.01942 0.01142 -0.1009 0.0403 0.6988 7.750 1.2680 0.01983 0.01185 -0.1001 0.0390 0.7009 8.000 1.2909 0.02028 0.01231 -0.0992 0.0378 0.7032 8.250 1.3134 0.02075 0.01281 -0.0982 0.0367 0.7057 8.500 1.3361 0.02118 0.01329 -0.0973 0.0355 0.7082 8.750 1.3580 0.02164 0.01379 -0.0962 0.0345 0.7102 9.000 1.3791 0.02213 0.01432 -0.0950 0.0335 0.7120 9.250 1.3990 0.02267 0.01489 -0.0937 0.0327 0.7139 9.500 1.4183 0.02323 0.01551 -0.0922 0.0320 0.7160 9.750 1.4371 0.02379 0.01613 -0.0906 0.0314 0.7182 10.000 1.4549 0.02437 0.01678 -0.0889 0.0307 0.7205 10.250 1.4702 0.02496 0.01742 -0.0868 0.0301 0.7228 10.500 1.4847 0.02559 0.01810 -0.0845 0.0295 0.7250 10.750 1.4998 0.02628 0.01885 -0.0825 0.0290 0.7270 11.000 1.5142 0.02705 0.01967 -0.0804 0.0285 0.7291 11.250 1.5275 0.02792 0.02060 -0.0783 0.0280 0.7315 11.500 1.5417 0.02874 0.02151 -0.0763 0.0276 0.7341 11.750 1.5553 0.02960 0.02246 -0.0744 0.0272 0.7366 12.000 1.5683 0.03052 0.02346 -0.0724 0.0267 0.7390 12.250 1.5804 0.03151 0.02453 -0.0705 0.0264 0.7413 12.500 1.5918 0.03257 0.02568 -0.0685 0.0260 0.7434 12.750 1.6023 0.03369 0.02689 -0.0665 0.0257 0.7454 13.000 1.6119 0.03490 0.02819 -0.0646 0.0254 0.7476 13.250 1.6204 0.03624 0.02961 -0.0626 0.0251 0.7500 13.500 1.6275 0.03771 0.03117 -0.0607 0.0248 0.7524 13.750 1.6331 0.03936 0.03289 -0.0588 0.0245 0.7549 14.000 1.6366 0.04125 0.03487 -0.0569 0.0243 0.7572 14.250 1.6402 0.04319 0.03691 -0.0552 0.0241 0.7593 14.500 1.6440 0.04515 0.03900 -0.0537 0.0239 0.7613 14.750 1.6467 0.04729 0.04129 -0.0523 0.0238 0.7634 15.000 1.6481 0.04965 0.04378 -0.0511 0.0236 0.7656 15.250 1.6480 0.05223 0.04650 -0.0501 0.0234 0.7679 15.500 1.6463 0.05510 0.04949 -0.0493 0.0232 0.7701 15.750 1.6433 0.05824 0.05277 -0.0488 0.0231 0.7724 16.000 1.6393 0.06170 0.05636 -0.0487 0.0229 0.7745 16.250 1.6336 0.06553 0.06034 -0.0489 0.0227 0.7764 16.500 1.6261 0.06983 0.06479 -0.0497 0.0226 0.7782 16.750 1.6168 0.07466 0.06978 -0.0510 0.0224 0.7802 17.000 1.6057 0.08006 0.07535 -0.0529 0.0223 0.7822 17.250 1.5914 0.08625 0.08170 -0.0555 0.0222 0.7841 17.500 1.5743 0.09323 0.08885 -0.0589 0.0221 0.7859 17.750 1.5542 0.10103 0.09683 -0.0630 0.0220 0.7875 18.000 1.5304 0.10971 0.10569 -0.0678 0.0219 0.7889 18.250 1.5035 0.11919 0.11535 -0.0733 0.0219 0.7900 18.500 1.4742 0.12940 0.12575 -0.0796 0.0218 0.7909 18.750 1.4432 0.14024 0.13677 -0.0866 0.0218 0.7917 19.000 1.4105 0.15177 0.14848 -0.0944 0.0217 0.7923