XFOIL Version 6.96 Calculated polar for: NASA SC(2)-0714 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 = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -18.250 -0.9204 0.10182 0.09834 -0.0570 1.0000 0.0315 -18.000 -0.9840 0.08595 0.08213 -0.0669 1.0000 0.0313 -17.750 -1.0141 0.07728 0.07322 -0.0719 1.0000 0.0314 -17.500 -1.0351 0.07070 0.06644 -0.0754 1.0000 0.0315 -17.250 -1.0510 0.06534 0.06090 -0.0778 1.0000 0.0316 -17.000 -1.0635 0.06083 0.05622 -0.0795 1.0000 0.0318 -16.750 -1.0735 0.05697 0.05219 -0.0805 1.0000 0.0320 -16.500 -1.0816 0.05364 0.04870 -0.0810 1.0000 0.0322 -16.250 -1.0881 0.05076 0.04568 -0.0810 1.0000 0.0324 -16.000 -1.0937 0.04827 0.04304 -0.0805 1.0000 0.0325 -15.750 -1.0983 0.04572 0.04036 -0.0796 1.0000 0.0328 -15.500 -1.0971 0.04380 0.03840 -0.0784 1.0000 0.0332 -15.250 -1.0950 0.04225 0.03682 -0.0771 1.0000 0.0335 -15.000 -1.0931 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0.9894 0.0443 -10.250 -0.8852 0.02257 0.01621 -0.0564 0.9876 0.0456 -10.000 -0.8548 0.02199 0.01559 -0.0581 0.9860 0.0470 -9.750 -0.8231 0.02146 0.01499 -0.0599 0.9847 0.0483 -9.500 -0.7922 0.02060 0.01416 -0.0617 0.9836 0.0500 -9.250 -0.7582 0.02005 0.01363 -0.0641 0.9826 0.0517 -9.000 -0.7232 0.01959 0.01315 -0.0664 0.9818 0.0536 -8.750 -0.6878 0.01919 0.01270 -0.0688 0.9811 0.0555 -8.500 -0.6622 0.01846 0.01202 -0.0695 0.9779 0.0577 -8.250 -0.6306 0.01803 0.01159 -0.0711 0.9758 0.0601 -8.000 -0.5977 0.01767 0.01120 -0.0729 0.9743 0.0623 -7.750 -0.5626 0.01701 0.01058 -0.0755 0.9732 0.0653 -7.500 -0.5272 0.01662 0.01020 -0.0778 0.9721 0.0686 -7.250 -0.4906 0.01622 0.00979 -0.0804 0.9711 0.0721 -7.000 -0.4526 0.01573 0.00936 -0.0833 0.9704 0.0768 -6.750 -0.4148 0.01537 0.00901 -0.0860 0.9697 0.0819 -6.500 -0.3769 0.01501 0.00870 -0.0888 0.9692 0.0890 -6.250 -0.3384 0.01461 0.00837 -0.0917 0.9687 0.0982 -6.000 -0.2992 0.01422 0.00806 -0.0948 0.9682 0.1109 -5.750 -0.2593 0.01384 0.00779 -0.0980 0.9678 0.1310 -5.500 -0.2312 0.01342 0.00754 -0.0989 0.9638 0.1594 -5.250 -0.1894 0.01283 0.00722 -0.1030 0.9632 0.2159 -5.000 -0.1205 0.01150 0.00658 -0.1139 0.9680 0.3698 -4.750 -0.0695 0.01065 0.00640 -0.1203 0.9685 0.5271 -4.500 -0.0322 0.01069 0.00655 -0.1223 0.9678 0.5708 -4.250 -0.0102 0.01083 0.00671 -0.1210 0.9625 0.5876 -4.000 0.0227 0.01091 0.00676 -0.1219 0.9602 0.6018 -3.750 0.0569 0.01101 0.00686 -0.1230 0.9583 0.6135 -3.500 0.0916 0.01110 0.00697 -0.1242 0.9568 0.6221 -3.250 0.1273 0.01120 0.00708 -0.1255 0.9556 0.6301 -3.000 0.1658 0.01120 0.00705 -0.1276 0.9547 0.6360 -2.750 0.2056 0.01116 0.00706 -0.1296 0.9538 0.6405 -2.500 0.2278 0.01127 0.00720 -0.1279 0.9464 0.6459 -2.250 0.2720 0.01105 0.00698 -0.1307 0.9437 0.6537 -2.000 0.3121 0.01079 0.00680 -0.1319 0.9402 0.6581 -1.750 0.3423 0.01073 0.00678 -0.1315 0.9343 0.6620 -1.500 0.3728 0.01061 0.00667 -0.1312 0.9267 0.6671 -1.250 0.4096 0.01031 0.00632 -0.1326 0.9195 0.6712 -1.000 0.4364 0.01017 0.00622 -0.1319 0.9111 0.6729 -0.750 0.4665 0.01001 0.00607 -0.1318 0.9026 0.6743 -0.500 0.4943 0.00991 0.00597 -0.1312 0.8899 0.6757 -0.250 0.5225 0.00983 0.00590 -0.1308 0.8757 0.6771 0.000 0.5513 0.00977 0.00583 -0.1306 0.8584 0.6787 0.250 0.5807 0.00975 0.00574 -0.1304 0.8362 0.6806 0.500 0.6088 0.00978 0.00567 -0.1301 0.7995 0.6826 0.750 0.6343 0.01006 0.00560 -0.1291 0.7227 0.6850 1.000 0.6514 0.01099 0.00578 -0.1268 0.5786 0.6874 1.250 0.6702 0.01199 0.00609 -0.1252 0.4407 0.6893 1.500 0.6914 0.01277 0.00635 -0.1242 0.3325 0.6908 2.000 0.7365 0.01405 0.00688 -0.1224 0.1819 0.6930 2.250 0.7611 0.01453 0.00715 -0.1218 0.1447 0.6940 2.500 0.7869 0.01489 0.00740 -0.1213 0.1224 0.6951 2.750 0.8129 0.01524 0.00766 -0.1209 0.1069 0.6963 3.000 0.8390 0.01557 0.00793 -0.1206 0.0965 0.6975 3.250 0.8649 0.01595 0.00824 -0.1201 0.0885 0.6988 3.500 0.8918 0.01620 0.00848 -0.1199 0.0831 0.7004 3.750 0.9175 0.01660 0.00884 -0.1194 0.0783 0.7021 4.000 0.9446 0.01685 0.00909 -0.1193 0.0749 0.7037 4.250 0.9710 0.01720 0.00939 -0.1190 0.0714 0.7052 4.500 0.9969 0.01761 0.00979 -0.1187 0.0685 0.7067 4.750 1.0238 0.01791 0.01010 -0.1185 0.0661 0.7081 5.000 1.0500 0.01827 0.01043 -0.1182 0.0637 0.7093 5.250 1.0728 0.01886 0.01099 -0.1173 0.0612 0.7106 5.500 1.0984 0.01908 0.01128 -0.1167 0.0594 0.7118 5.750 1.1231 0.01940 0.01162 -0.1160 0.0572 0.7129 6.000 1.1466 0.01981 0.01203 -0.1152 0.0553 0.7141 6.250 1.1680 0.02046 0.01269 -0.1139 0.0534 0.7155 6.500 1.1920 0.02082 0.01312 -0.1131 0.0518 0.7170 6.750 1.2154 0.02122 0.01354 -0.1122 0.0501 0.7185 7.000 1.2378 0.02173 0.01403 -0.1112 0.0485 0.7200 7.250 1.2584 0.02249 0.01481 -0.1099 0.0470 0.7215 7.500 1.2816 0.02291 0.01530 -0.1090 0.0456 0.7231 7.750 1.3040 0.02337 0.01578 -0.1081 0.0442 0.7248 8.000 1.3254 0.02390 0.01630 -0.1069 0.0430 0.7264 8.250 1.3437 0.02487 0.01725 -0.1054 0.0418 0.7278 8.500 1.3639 0.02553 0.01798 -0.1041 0.0410 0.7292 8.750 1.3832 0.02608 0.01863 -0.1025 0.0401 0.7306 9.000 1.4007 0.02670 0.01933 -0.1006 0.0392 0.7319 9.250 1.4152 0.02732 0.02002 -0.0982 0.0385 0.7334 9.500 1.4297 0.02799 0.02073 -0.0959 0.0378 0.7349 9.750 1.4451 0.02881 0.02157 -0.0939 0.0371 0.7366 10.000 1.4601 0.03021 0.02300 -0.0920 0.0363 0.7383 10.250 1.4756 0.03089 0.02380 -0.0900 0.0358 0.7401 10.500 1.4908 0.03170 0.02472 -0.0881 0.0352 0.7419 10.750 1.5052 0.03262 0.02574 -0.0861 0.0346 0.7438 11.000 1.5190 0.03359 0.02680 -0.0841 0.0340 0.7456 11.250 1.5321 0.03461 0.02788 -0.0821 0.0335 0.7472 11.500 1.5443 0.03561 0.02895 -0.0801 0.0331 0.7488 11.750 1.5552 0.03669 0.03010 -0.0779 0.0327 0.7502 12.000 1.5653 0.03791 0.03138 -0.0757 0.0323 0.7517 12.250 1.5737 0.03949 0.03302 -0.0735 0.0319 0.7532 12.500 1.5796 0.04149 0.03516 -0.0710 0.0315 0.7549 12.750 1.5850 0.04303 0.03686 -0.0686 0.0313 0.7569 13.000 1.5892 0.04475 0.03874 -0.0662 0.0310 0.7589 13.250 1.5921 0.04666 0.04082 -0.0640 0.0307 0.7610 13.500 1.5937 0.04877 0.04307 -0.0618 0.0304 0.7629 13.750 1.5940 0.05103 0.04549 -0.0599 0.0302 0.7646 14.000 1.5930 0.05346 0.04807 -0.0580 0.0299 0.7661 14.250 1.5903 0.05608 0.05085 -0.0564 0.0296 0.7676 14.500 1.5865 0.05888 0.05381 -0.0550 0.0294 0.7690 14.750 1.5820 0.06186 0.05694 -0.0539 0.0291 0.7705 15.000 1.5763 0.06516 0.06038 -0.0532 0.0289 0.7720 15.250 1.5697 0.06875 0.06411 -0.0530 0.0287 0.7736 15.500 1.5630 0.07256 0.06805 -0.0532 0.0285 0.7753 15.750 1.5530 0.07714 0.07277 -0.0540 0.0284 0.7770 16.000 1.5431 0.08195 0.07772 -0.0554 0.0282 0.7786 16.250 1.5292 0.08773 0.08365 -0.0575 0.0282 0.7801 16.500 1.5144 0.09396 0.09003 -0.0604 0.0280 0.7815 16.750 1.4935 0.10167 0.09793 -0.0646 0.0280 0.7825 17.000 1.4674 0.11092 0.10741 -0.0703 0.0279 0.7834 17.250 1.4167 0.12628 0.12313 -0.0812 0.0280 0.7833