XFOIL Version 6.96 Calculated polar for: S1014 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -17.750 -0.8173 0.11507 0.11119 -0.0414 1.0000 0.0470 -17.500 -0.8765 0.09942 0.09532 -0.0510 1.0000 0.0462 -17.250 -0.9219 0.08804 0.08368 -0.0577 1.0000 0.0459 -17.000 -0.9563 0.07956 0.07495 -0.0621 1.0000 0.0458 -16.750 -0.9864 0.07255 0.06766 -0.0651 1.0000 0.0459 -16.500 -1.0102 0.06695 0.06180 -0.0667 1.0000 0.0461 -16.250 -1.0294 0.06236 0.05695 -0.0675 1.0000 0.0464 -16.000 -1.0472 0.05839 0.05270 -0.0677 1.0000 0.0468 -15.750 -1.0553 0.05464 0.04875 -0.0676 1.0000 0.0475 -15.500 -1.0439 0.05262 0.04676 -0.0679 1.0000 0.0487 -15.250 -1.0383 0.05061 0.04469 -0.0679 1.0000 0.0498 -15.000 -1.0360 0.04855 0.04251 -0.0677 1.0000 0.0510 -14.750 -1.0340 0.04641 0.04021 -0.0672 1.0000 0.0522 -14.500 -1.0352 0.04444 0.03802 -0.0664 1.0000 0.0538 -14.250 -1.0374 0.04262 0.03593 -0.0651 1.0000 0.0548 -14.000 -1.0145 0.04059 0.03390 -0.0662 0.9856 0.0570 -13.750 -0.9951 0.03925 0.03252 -0.0674 0.9772 0.0591 -13.500 -0.9789 0.03774 0.03083 -0.0682 0.9712 0.0616 -13.250 -0.9647 0.03626 0.02908 -0.0686 0.9659 0.0637 -13.000 -0.9390 0.03470 0.02753 -0.0696 0.9625 0.0668 -12.750 -0.9202 0.03372 0.02650 -0.0701 0.9585 0.0698 -12.500 -0.9028 0.03263 0.02522 -0.0701 0.9548 0.0728 -12.250 -0.8818 0.03143 0.02392 -0.0702 0.9513 0.0761 -12.000 -0.8624 0.03062 0.02314 -0.0701 0.9478 0.0794 -11.750 -0.8452 0.02984 0.02225 -0.0697 0.9446 0.0830 -11.500 -0.8252 0.02895 0.02121 -0.0695 0.9422 0.0869 -11.250 -0.8027 0.02817 0.02049 -0.0696 0.9402 0.0912 -11.000 -0.7843 0.02752 0.01977 -0.0692 0.9380 0.0956 -10.750 -0.7615 0.02674 0.01892 -0.0692 0.9362 0.1004 -10.500 -0.7417 0.02611 0.01833 -0.0689 0.9342 0.1054 -10.250 -0.7228 0.02559 0.01769 -0.0684 0.9322 0.1107 -10.000 -0.6994 0.02487 0.01704 -0.0684 0.9308 0.1166 -9.750 -0.6801 0.02437 0.01650 -0.0679 0.9291 0.1231 -9.500 -0.6586 0.02377 0.01592 -0.0676 0.9277 0.1300 -9.250 -0.6392 0.02331 0.01544 -0.0671 0.9263 0.1374 -9.000 -0.6194 0.02278 0.01494 -0.0665 0.9249 0.1457 -8.750 -0.6002 0.02236 0.01449 -0.0659 0.9232 0.1550 -8.500 -0.5816 0.02181 0.01405 -0.0653 0.9219 0.1651 -8.250 -0.5633 0.02135 0.01362 -0.0646 0.9206 0.1767 -8.000 -0.5457 0.02092 0.01323 -0.0638 0.9193 0.1902 -7.750 -0.5298 0.02048 0.01288 -0.0628 0.9180 0.2057 -7.500 -0.5164 0.02001 0.01253 -0.0613 0.9167 0.2240 -7.250 -0.5052 0.01955 0.01221 -0.0596 0.9153 0.2460 -7.000 -0.4965 0.01909 0.01190 -0.0573 0.9135 0.2733 -6.750 -0.4926 0.01861 0.01162 -0.0541 0.9116 0.3073 -6.500 -0.4942 0.01818 0.01141 -0.0501 0.9101 0.3476 -6.250 -0.5055 0.01798 0.01144 -0.0441 0.9085 0.3885 -6.000 -0.5384 0.01838 0.01195 -0.0337 0.9052 0.4079 -5.750 -0.5790 0.01893 0.01254 -0.0214 0.9024 0.4181 -5.500 -0.6157 0.01915 0.01286 -0.0096 0.9001 0.4378 -5.250 -0.6334 0.01880 0.01286 -0.0015 0.8981 0.4961 -5.000 -0.6288 0.01888 0.01369 0.0035 0.8971 0.6043 -4.750 -0.5837 0.02072 0.01579 0.0024 0.8966 0.6790 -4.500 -0.5725 0.02116 0.01613 0.0055 0.8949 0.7060 -4.250 -0.5456 0.02192 0.01679 0.0059 0.8936 0.7253 -4.000 -0.5583 0.02252 0.01737 0.0136 0.8917 0.7352 -3.750 -0.5635 0.02290 0.01769 0.0197 0.8896 0.7473 -3.500 -0.5431 0.02389 0.01867 0.0218 0.8876 0.7555 -3.250 -0.5267 0.02454 0.01927 0.0243 0.8852 0.7654 -3.000 -0.4968 0.02553 0.02022 0.0247 0.8832 0.7727 -2.750 -0.4673 0.02613 0.02075 0.0248 0.8807 0.7814 -2.500 -0.4111 0.02742 0.02201 0.0209 0.8790 0.7857 -2.250 -0.4150 0.02748 0.02202 0.0263 0.8750 0.7968 -2.000 -0.3919 0.02830 0.02284 0.0280 0.8712 0.8008 -1.750 -0.3882 0.02819 0.02268 0.0319 0.8668 0.8122 -1.500 -0.3266 0.02946 0.02394 0.0272 0.8648 0.8151 -1.250 -0.2380 0.03114 0.02560 0.0177 0.8641 0.8195 -1.000 -0.1857 0.03185 0.02627 0.0138 0.8623 0.8301 -0.750 -0.0855 0.03257 0.02697 0.0008 0.8625 0.8313 -0.500 -0.1571 0.03243 0.02685 0.0189 0.8505 0.8461 -0.250 -0.0743 0.03281 0.02722 0.0087 0.8494 0.8469 0.000 0.0001 0.03291 0.02732 0.0000 0.8481 0.8481 0.250 0.0745 0.03281 0.02722 -0.0087 0.8469 0.8494 0.500 0.1575 0.03242 0.02684 -0.0190 0.8461 0.8505 0.750 0.0853 0.03257 0.02698 -0.0008 0.8314 0.8626 1.000 0.1863 0.03183 0.02626 -0.0139 0.8301 0.8623 1.250 0.2405 0.03107 0.02553 -0.0181 0.8194 0.8640 1.500 0.3260 0.02950 0.02397 -0.0271 0.8152 0.8648 1.750 0.3880 0.02821 0.02270 -0.0319 0.8122 0.8669 2.000 0.3918 0.02829 0.02284 -0.0280 0.8008 0.8713 2.250 0.4145 0.02749 0.02204 -0.0263 0.7968 0.8750 2.500 0.4104 0.02745 0.02204 -0.0208 0.7858 0.8790 2.750 0.4669 0.02615 0.02077 -0.0248 0.7815 0.8807 3.000 0.4966 0.02552 0.02021 -0.0247 0.7727 0.8832 3.250 0.5265 0.02453 0.01926 -0.0243 0.7654 0.8852 3.500 0.5429 0.02390 0.01868 -0.0218 0.7557 0.8875 3.750 0.5631 0.02291 0.01771 -0.0196 0.7474 0.8896 4.000 0.5579 0.02251 0.01736 -0.0136 0.7351 0.8917 4.250 0.5456 0.02192 0.01679 -0.0060 0.7253 0.8936 4.500 0.5726 0.02114 0.01611 -0.0055 0.7054 0.8950 4.750 0.5832 0.02071 0.01578 -0.0023 0.6790 0.8965 5.000 0.6285 0.01888 0.01369 -0.0035 0.6048 0.8971 5.250 0.6333 0.01879 0.01285 0.0015 0.4965 0.8981 5.500 0.6157 0.01914 0.01285 0.0096 0.4382 0.9001 5.750 0.5792 0.01892 0.01254 0.0214 0.4185 0.9024 6.000 0.5386 0.01838 0.01195 0.0337 0.4080 0.9052 6.250 0.5054 0.01798 0.01144 0.0441 0.3882 0.9085 6.500 0.4945 0.01817 0.01141 0.0500 0.3478 0.9101 6.750 0.4926 0.01861 0.01161 0.0541 0.3070 0.9117 7.000 0.4966 0.01909 0.01190 0.0572 0.2731 0.9136 7.250 0.5053 0.01955 0.01221 0.0595 0.2458 0.9153 7.500 0.5165 0.02001 0.01253 0.0613 0.2238 0.9167 7.750 0.5300 0.02048 0.01287 0.0627 0.2056 0.9180 8.000 0.5460 0.02092 0.01323 0.0638 0.1903 0.9193 8.250 0.5636 0.02134 0.01362 0.0646 0.1767 0.9206 8.500 0.5819 0.02181 0.01404 0.0653 0.1650 0.9219 8.750 0.6005 0.02235 0.01448 0.0659 0.1550 0.9233 9.000 0.6198 0.02277 0.01494 0.0664 0.1457 0.9250 9.250 0.6396 0.02330 0.01543 0.0670 0.1374 0.9264 9.500 0.6590 0.02377 0.01591 0.0675 0.1299 0.9277 9.750 0.6805 0.02437 0.01649 0.0678 0.1229 0.9291 10.000 0.7000 0.02486 0.01703 0.0683 0.1167 0.9308 10.250 0.7229 0.02557 0.01768 0.0684 0.1106 0.9323 10.500 0.7419 0.02610 0.01832 0.0689 0.1053 0.9343 10.750 0.7622 0.02674 0.01892 0.0691 0.1003 0.9362 11.000 0.7844 0.02751 0.01976 0.0692 0.0954 0.9381 11.250 0.8030 0.02815 0.02047 0.0696 0.0911 0.9403 11.500 0.8265 0.02896 0.02121 0.0693 0.0868 0.9422 11.750 0.8456 0.02983 0.02224 0.0696 0.0830 0.9447 12.000 0.8630 0.03062 0.02314 0.0700 0.0793 0.9479 12.250 0.8824 0.03142 0.02390 0.0701 0.0760 0.9515 12.500 0.9033 0.03262 0.02522 0.0700 0.0727 0.9549 12.750 0.9206 0.03371 0.02649 0.0700 0.0696 0.9587 13.000 0.9401 0.03470 0.02753 0.0695 0.0668 0.9626 13.250 0.9656 0.03624 0.02906 0.0685 0.0637 0.9661 13.500 0.9792 0.03771 0.03081 0.0681 0.0614 0.9715 13.750 0.9964 0.03925 0.03252 0.0672 0.0591 0.9775 14.000 1.0160 0.04057 0.03388 0.0660 0.0570 0.9861 14.250 1.0380 0.04262 0.03593 0.0650 0.0548 1.0000 14.500 1.0358 0.04444 0.03802 0.0663 0.0537 1.0000 14.750 1.0357 0.04647 0.04026 0.0670 0.0524 1.0000 15.000 1.0373 0.04852 0.04248 0.0675 0.0510 1.0000 15.250 1.0395 0.05062 0.04470 0.0677 0.0498 1.0000 15.500 1.0459 0.05253 0.04666 0.0677 0.0487 1.0000 15.750 1.0570 0.05463 0.04874 0.0674 0.0475 1.0000 16.000 1.0490 0.05833 0.05264 0.0675 0.0468 1.0000 16.250 1.0306 0.06238 0.05697 0.0674 0.0464 1.0000 16.500 1.0106 0.06706 0.06192 0.0665 0.0461 1.0000 16.750 0.9873 0.07256 0.06768 0.0649 0.0458 1.0000 17.000 0.9590 0.07935 0.07473 0.0620 0.0457 1.0000 17.250 0.9220 0.08821 0.08386 0.0574 0.0458 1.0000 17.500 0.8790 0.09921 0.09511 0.0509 0.0462 1.0000 17.750 0.8136 0.11615 0.11229 0.0404 0.0470 1.0000