XFOIL Version 6.96 Calculated polar for: J5012 12% 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 ------ -------- --------- --------- -------- -------- -------- -18.750 -0.9158 0.13871 0.13579 -0.0039 1.0000 0.0119 -18.500 -0.9533 0.12634 0.12324 -0.0105 1.0000 0.0118 -18.250 -0.9811 0.11650 0.11327 -0.0157 1.0000 0.0118 -18.000 -1.0057 0.10768 0.10432 -0.0204 1.0000 0.0118 -17.750 -1.0286 0.09942 0.09591 -0.0247 1.0000 0.0118 -17.500 -1.0477 0.09199 0.08835 -0.0287 1.0000 0.0119 -17.250 -1.0703 0.08430 0.08051 -0.0327 1.0000 0.0118 -17.000 -1.0842 0.07811 0.07421 -0.0360 1.0000 0.0119 -16.750 -1.0995 0.07197 0.06792 -0.0392 1.0000 0.0119 -16.500 -1.1120 0.06639 0.06221 -0.0421 1.0000 0.0121 -16.250 -1.1230 0.06131 0.05699 -0.0446 1.0000 0.0121 -16.000 -1.1326 0.05663 0.05218 -0.0467 1.0000 0.0122 -15.750 -1.1409 0.05235 0.04776 -0.0484 1.0000 0.0122 -15.500 -1.1443 0.04890 0.04419 -0.0497 1.0000 0.0124 -15.250 -1.1489 0.04548 0.04063 -0.0506 1.0000 0.0126 -15.000 -1.1489 0.04276 0.03779 -0.0510 1.0000 0.0128 -14.750 -1.1516 0.03994 0.03483 -0.0511 1.0000 0.0130 -14.500 -1.1491 0.03778 0.03256 -0.0509 1.0000 0.0132 -14.250 -1.1483 0.03561 0.03026 -0.0504 1.0000 0.0133 -14.000 -1.1451 0.03376 0.02830 -0.0495 1.0000 0.0135 -13.750 -1.1412 0.03211 0.02652 -0.0484 1.0000 0.0136 -13.500 -1.1406 0.03029 0.02462 -0.0468 1.0000 0.0139 -13.250 -1.1383 0.02874 0.02298 -0.0450 1.0000 0.0141 -13.000 -1.1343 0.02741 0.02157 -0.0431 1.0000 0.0143 -12.750 -1.1287 0.02626 0.02034 -0.0410 1.0000 0.0145 -12.500 -1.1214 0.02528 0.01929 -0.0388 1.0000 0.0148 -12.250 -1.1133 0.02441 0.01834 -0.0365 1.0000 0.0151 -12.000 -1.1058 0.02356 0.01742 -0.0339 1.0000 0.0153 -11.750 -1.0968 0.02285 0.01665 -0.0314 1.0000 0.0157 -11.500 -1.0889 0.02215 0.01587 -0.0285 1.0000 0.0161 -11.250 -1.0802 0.02157 0.01523 -0.0255 1.0000 0.0166 -11.000 -1.0728 0.02101 0.01460 -0.0222 1.0000 0.0169 -10.750 -1.0648 0.02050 0.01401 -0.0188 1.0000 0.0171 -10.500 -1.0566 0.01981 0.01327 -0.0156 1.0000 0.0176 -10.250 -1.0466 0.01919 0.01261 -0.0126 1.0000 0.0180 -10.000 -1.0351 0.01866 0.01204 -0.0098 1.0000 0.0186 -9.750 -1.0227 0.01818 0.01152 -0.0072 1.0000 0.0192 -9.500 -1.0100 0.01772 0.01102 -0.0045 1.0000 0.0198 -9.250 -0.9968 0.01729 0.01053 -0.0019 1.0000 0.0204 -9.000 -0.9833 0.01689 0.01007 0.0006 1.0000 0.0211 -8.750 -0.9657 0.01644 0.00958 0.0023 0.9996 0.0219 -8.500 -0.9366 0.01589 0.00903 0.0015 0.9975 0.0234 -8.250 -0.9066 0.01545 0.00854 0.0006 0.9951 0.0253 -8.000 -0.8772 0.01501 0.00807 -0.0001 0.9928 0.0272 -7.750 -0.8492 0.01454 0.00760 -0.0005 0.9898 0.0297 -7.500 -0.8193 0.01416 0.00719 -0.0013 0.9870 0.0325 -7.250 -0.7887 0.01374 0.00678 -0.0022 0.9846 0.0363 -7.000 -0.7567 0.01340 0.00642 -0.0034 0.9827 0.0407 -6.750 -0.7308 0.01301 0.00606 -0.0032 0.9783 0.0458 -6.500 -0.7011 0.01266 0.00571 -0.0038 0.9748 0.0513 -6.250 -0.6698 0.01231 0.00539 -0.0048 0.9722 0.0583 -6.000 -0.6374 0.01195 0.00506 -0.0060 0.9701 0.0670 -5.750 -0.6109 0.01162 0.00477 -0.0059 0.9652 0.0770 -5.500 -0.5815 0.01126 0.00447 -0.0065 0.9610 0.0918 -5.250 -0.5495 0.01088 0.00418 -0.0076 0.9580 0.1112 -5.000 -0.5164 0.01048 0.00390 -0.0090 0.9554 0.1341 -4.750 -0.4914 0.01015 0.00366 -0.0086 0.9483 0.1570 -4.500 -0.4607 0.00981 0.00341 -0.0093 0.9434 0.1830 -4.250 -0.4305 0.00943 0.00317 -0.0101 0.9384 0.2156 -4.000 -0.4038 0.00910 0.00296 -0.0100 0.9305 0.2481 -3.750 -0.3730 0.00877 0.00275 -0.0107 0.9244 0.2818 -3.500 -0.3474 0.00849 0.00258 -0.0103 0.9150 0.3146 -3.250 -0.3199 0.00819 0.00241 -0.0103 0.9067 0.3524 -3.000 -0.2941 0.00791 0.00226 -0.0099 0.8966 0.3917 -2.750 -0.2691 0.00767 0.00213 -0.0093 0.8858 0.4288 -2.500 -0.2435 0.00745 0.00201 -0.0088 0.8749 0.4623 -2.250 -0.2180 0.00728 0.00190 -0.0082 0.8629 0.4927 -2.000 -0.1937 0.00712 0.00181 -0.0074 0.8496 0.5236 -1.750 -0.1694 0.00698 0.00174 -0.0065 0.8358 0.5536 -1.500 -0.1450 0.00686 0.00167 -0.0057 0.8217 0.5821 -1.250 -0.1210 0.00676 0.00162 -0.0047 0.8068 0.6090 -1.000 -0.0967 0.00668 0.00157 -0.0038 0.7914 0.6335 -0.750 -0.0725 0.00662 0.00154 -0.0029 0.7752 0.6573 -0.500 -0.0482 0.00658 0.00152 -0.0020 0.7581 0.6786 -0.250 -0.0241 0.00656 0.00150 -0.0010 0.7400 0.7001 0.000 0.0000 0.00655 0.00150 0.0000 0.7210 0.7209 0.250 0.0241 0.00655 0.00150 0.0010 0.7003 0.7402 0.500 0.0482 0.00658 0.00152 0.0020 0.6789 0.7581 0.750 0.0724 0.00662 0.00154 0.0029 0.6569 0.7752 1.000 0.0966 0.00668 0.00157 0.0038 0.6335 0.7915 1.250 0.1209 0.00676 0.00162 0.0048 0.6087 0.8069 1.500 0.1450 0.00686 0.00167 0.0057 0.5820 0.8218 1.750 0.1694 0.00698 0.00174 0.0065 0.5539 0.8359 2.000 0.1938 0.00711 0.00181 0.0074 0.5245 0.8496 2.500 0.2435 0.00745 0.00201 0.0088 0.4626 0.8748 2.750 0.2689 0.00767 0.00213 0.0094 0.4279 0.8858 3.000 0.2942 0.00790 0.00226 0.0099 0.3926 0.8965 3.250 0.3199 0.00819 0.00241 0.0103 0.3527 0.9066 3.500 0.3473 0.00849 0.00258 0.0103 0.3145 0.9150 3.750 0.3730 0.00877 0.00275 0.0107 0.2819 0.9244 4.000 0.4037 0.00911 0.00296 0.0100 0.2473 0.9305 4.250 0.4304 0.00944 0.00317 0.0101 0.2150 0.9383 4.500 0.4607 0.00980 0.00341 0.0093 0.1839 0.9434 4.750 0.4914 0.01016 0.00366 0.0086 0.1566 0.9482 5.000 0.5163 0.01048 0.00390 0.0090 0.1340 0.9554 5.250 0.5494 0.01088 0.00418 0.0076 0.1112 0.9580 5.500 0.5816 0.01125 0.00447 0.0065 0.0923 0.9610 5.750 0.6110 0.01161 0.00476 0.0059 0.0777 0.9651 6.000 0.6375 0.01195 0.00506 0.0060 0.0672 0.9702 6.250 0.6698 0.01231 0.00539 0.0048 0.0584 0.9722 6.500 0.7011 0.01267 0.00572 0.0038 0.0513 0.9749 6.750 0.7307 0.01301 0.00606 0.0032 0.0454 0.9783 7.000 0.7567 0.01339 0.00642 0.0034 0.0403 0.9827 7.250 0.7887 0.01374 0.00678 0.0022 0.0361 0.9846 7.500 0.8194 0.01416 0.00720 0.0012 0.0324 0.9870 7.750 0.8492 0.01454 0.00760 0.0005 0.0296 0.9898 8.000 0.8771 0.01503 0.00808 0.0001 0.0268 0.9928 8.250 0.9067 0.01544 0.00854 -0.0007 0.0252 0.9952 8.500 0.9366 0.01590 0.00903 -0.0015 0.0236 0.9975 8.750 0.9657 0.01645 0.00959 -0.0023 0.0219 0.9996 9.000 0.9832 0.01690 0.01008 -0.0006 0.0210 1.0000 9.250 0.9967 0.01730 0.01054 0.0020 0.0203 1.0000 9.500 1.0097 0.01774 0.01103 0.0046 0.0197 1.0000 9.750 1.0226 0.01818 0.01152 0.0072 0.0191 1.0000 10.000 1.0349 0.01867 0.01205 0.0099 0.0186 1.0000 10.250 1.0465 0.01920 0.01261 0.0126 0.0180 1.0000 10.500 1.0565 0.01982 0.01327 0.0156 0.0176 1.0000 10.750 1.0644 0.02052 0.01403 0.0189 0.0171 1.0000 11.000 1.0721 0.02105 0.01464 0.0223 0.0169 1.0000 11.250 1.0799 0.02159 0.01525 0.0256 0.0165 1.0000 11.500 1.0879 0.02221 0.01594 0.0286 0.0162 1.0000 11.750 1.0971 0.02284 0.01664 0.0313 0.0157 1.0000 12.000 1.1053 0.02360 0.01747 0.0340 0.0154 1.0000 12.250 1.1135 0.02441 0.01835 0.0365 0.0151 1.0000 12.500 1.1217 0.02528 0.01929 0.0387 0.0148 1.0000 12.750 1.1287 0.02628 0.02037 0.0409 0.0145 1.0000 13.000 1.1349 0.02740 0.02157 0.0430 0.0144 1.0000 13.250 1.1394 0.02870 0.02295 0.0449 0.0142 1.0000 13.500 1.1405 0.03035 0.02467 0.0468 0.0138 1.0000 13.750 1.1404 0.03222 0.02663 0.0484 0.0136 1.0000 14.000 1.1452 0.03381 0.02834 0.0494 0.0135 1.0000 14.250 1.1482 0.03568 0.03033 0.0503 0.0134 1.0000 14.500 1.1497 0.03780 0.03257 0.0508 0.0132 1.0000 14.750 1.1507 0.04011 0.03500 0.0510 0.0131 1.0000 15.000 1.1500 0.04275 0.03777 0.0509 0.0129 1.0000 15.250 1.1489 0.04559 0.04074 0.0504 0.0127 1.0000 15.500 1.1438 0.04906 0.04436 0.0495 0.0126 1.0000 15.750 1.1413 0.05244 0.04785 0.0483 0.0124 1.0000 16.000 1.1333 0.05668 0.05223 0.0465 0.0123 1.0000 16.250 1.1242 0.06131 0.05700 0.0444 0.0122 1.0000 16.500 1.1129 0.06645 0.06228 0.0419 0.0121 1.0000 16.750 1.0993 0.07219 0.06815 0.0389 0.0120 1.0000 17.000 1.0858 0.07810 0.07419 0.0358 0.0120 1.0000 17.250 1.0668 0.08510 0.08134 0.0321 0.0119 1.0000 17.500 1.0524 0.09155 0.08791 0.0286 0.0118 1.0000 17.750 1.0301 0.09947 0.09597 0.0244 0.0118 1.0000 18.000 1.0076 0.10771 0.10434 0.0200 0.0118 1.0000