XFOIL Version 6.96 Calculated polar for: N-14 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.000 -1.1012 0.10667 0.10393 -0.0231 1.0000 0.0126 -18.750 -1.1331 0.09722 0.09435 -0.0282 1.0000 0.0127 -18.500 -1.1672 0.08767 0.08467 -0.0333 1.0000 0.0127 -18.250 -1.1905 0.07997 0.07683 -0.0374 1.0000 0.0127 -18.000 -1.2184 0.07169 0.06840 -0.0419 1.0000 0.0127 -17.750 -1.2405 0.06442 0.06099 -0.0459 1.0000 0.0128 -17.500 -1.2589 0.05805 0.05449 -0.0493 1.0000 0.0129 -17.250 -1.2741 0.05251 0.04883 -0.0521 1.0000 0.0132 -17.000 -1.2864 0.04782 0.04400 -0.0539 1.0000 0.0132 -16.750 -1.2913 0.04436 0.04044 -0.0549 1.0000 0.0134 -16.500 -1.2937 0.04141 0.03739 -0.0555 1.0000 0.0135 -16.250 -1.2860 0.03970 0.03564 -0.0556 1.0000 0.0139 -16.000 -1.2920 0.03674 0.03256 -0.0553 1.0000 0.0140 -15.750 -1.2857 0.03512 0.03087 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0.0368 -6.250 -0.6733 0.01101 0.00504 -0.0047 0.9773 0.0385 -6.000 -0.6406 0.01069 0.00471 -0.0059 0.9748 0.0404 -5.750 -0.6064 0.01040 0.00441 -0.0074 0.9730 0.0419 -5.500 -0.5723 0.01002 0.00403 -0.0088 0.9714 0.0455 -5.250 -0.5420 0.00967 0.00371 -0.0095 0.9683 0.0507 -5.000 -0.5161 0.00913 0.00343 -0.0093 0.9629 0.0912 -4.750 -0.4814 0.00891 0.00326 -0.0108 0.9601 0.1028 -4.500 -0.4441 0.00876 0.00310 -0.0129 0.9578 0.1079 -4.250 -0.4130 0.00857 0.00290 -0.0136 0.9510 0.1121 -4.000 -0.3790 0.00834 0.00270 -0.0150 0.9451 0.1168 -3.750 -0.3448 0.00816 0.00251 -0.0164 0.9384 0.1204 -3.500 -0.3117 0.00801 0.00234 -0.0176 0.9296 0.1234 -3.250 -0.2815 0.00783 0.00218 -0.0181 0.9204 0.1302 -3.000 -0.2507 0.00768 0.00203 -0.0187 0.9105 0.1364 -2.750 -0.2256 0.00743 0.00187 -0.0182 0.8984 0.1624 -2.500 -0.2042 0.00702 0.00172 -0.0169 0.8864 0.2346 -2.250 -0.1811 0.00675 0.00161 -0.0159 0.8755 0.2863 -2.000 -0.1588 0.00648 0.00149 -0.0148 0.8641 0.3389 -1.750 -0.1376 0.00621 0.00140 -0.0134 0.8529 0.3934 -1.500 -0.1182 0.00584 0.00130 -0.0116 0.8434 0.4723 -1.250 -0.0986 0.00554 0.00123 -0.0099 0.8341 0.5457 -1.000 -0.0779 0.00532 0.00118 -0.0082 0.8239 0.5991 -0.750 -0.0570 0.00516 0.00114 -0.0066 0.8127 0.6464 -0.500 -0.0355 0.00503 0.00113 -0.0051 0.8018 0.6884 -0.250 -0.0127 0.00494 0.00112 -0.0038 0.7910 0.7201 0.000 0.0104 0.00489 0.00112 -0.0026 0.7789 0.7455 0.250 0.0343 0.00488 0.00113 -0.0015 0.7662 0.7672 0.500 0.0582 0.00486 0.00113 -0.0004 0.7514 0.7846 0.750 0.0818 0.00486 0.00114 0.0007 0.7318 0.8015 1.000 0.1042 0.00492 0.00114 0.0021 0.7006 0.8151 1.250 0.1250 0.00505 0.00115 0.0038 0.6559 0.8271 1.500 0.1460 0.00522 0.00119 0.0054 0.6108 0.8390 1.750 0.1664 0.00544 0.00125 0.0071 0.5561 0.8501 2.000 0.1860 0.00573 0.00133 0.0089 0.4913 0.8621 2.250 0.2066 0.00603 0.00144 0.0105 0.4279 0.8749 2.500 0.2288 0.00628 0.00157 0.0118 0.3808 0.8903 2.750 0.2535 0.00648 0.00169 0.0125 0.3488 0.9051 3.000 0.2810 0.00665 0.00183 0.0126 0.3265 0.9177 3.250 0.3084 0.00683 0.00195 0.0128 0.3065 0.9285 3.500 0.3391 0.00702 0.00210 0.0121 0.2864 0.9370 3.750 0.3694 0.00726 0.00225 0.0116 0.2596 0.9445 4.000 0.4007 0.00757 0.00242 0.0107 0.2222 0.9496 4.250 0.4250 0.00794 0.00260 0.0113 0.1787 0.9568 4.500 0.4592 0.00834 0.00286 0.0098 0.1470 0.9592 4.750 0.4944 0.00872 0.00312 0.0080 0.1239 0.9622 5.000 0.5256 0.00907 0.00338 0.0071 0.1004 0.9658 5.250 0.5507 0.00958 0.00368 0.0075 0.0656 0.9709 5.500 0.5848 0.00992 0.00398 0.0061 0.0577 0.9720 5.750 0.6179 0.01030 0.00432 0.0048 0.0527 0.9735 6.000 0.6509 0.01060 0.00464 0.0035 0.0499 0.9752 6.250 0.6830 0.01086 0.00492 0.0025 0.0480 0.9775 6.500 0.7115 0.01116 0.00523 0.0022 0.0458 0.9810 6.750 0.7402 0.01159 0.00566 0.0018 0.0429 0.9836 7.000 0.7737 0.01191 0.00599 0.0004 0.0413 0.9848 7.250 0.8071 0.01214 0.00624 -0.0010 0.0398 0.9861 7.500 0.8395 0.01242 0.00653 -0.0022 0.0382 0.9878 7.750 0.8705 0.01277 0.00688 -0.0031 0.0363 0.9899 8.000 0.8989 0.01330 0.00744 -0.0036 0.0345 0.9924 8.250 0.9299 0.01350 0.00766 -0.0044 0.0333 0.9941 8.500 0.9629 0.01374 0.00791 -0.0058 0.0319 0.9953 8.750 0.9951 0.01404 0.00819 -0.0071 0.0301 0.9968 9.000 1.0249 0.01462 0.00880 -0.0080 0.0284 0.9985 9.250 1.0575 0.01479 0.00900 -0.0092 0.0272 0.9997 9.500 1.0779 0.01502 0.00924 -0.0080 0.0260 1.0000 9.750 1.0926 0.01530 0.00952 -0.0056 0.0250 1.0000 10.000 1.1020 0.01590 0.01014 -0.0023 0.0236 1.0000 10.250 1.1181 0.01612 0.01041 -0.0001 0.0230 1.0000 10.500 1.1333 0.01640 0.01072 0.0022 0.0221 1.0000 10.750 1.1488 0.01667 0.01101 0.0045 0.0211 1.0000 11.000 1.1625 0.01705 0.01139 0.0070 0.0203 1.0000 11.250 1.1707 0.01772 0.01210 0.0104 0.0192 1.0000 11.500 1.1847 0.01806 0.01250 0.0128 0.0187 1.0000 11.750 1.1968 0.01846 0.01293 0.0156 0.0181 1.0000 12.000 1.2045 0.01886 0.01338 0.0192 0.0176 1.0000 12.250 1.2127 0.01928 0.01383 0.0226 0.0170 1.0000 12.500 1.2200 0.01982 0.01440 0.0260 0.0164 1.0000 12.750 1.2223 0.02069 0.01533 0.0299 0.0158 1.0000 13.000 1.2307 0.02137 0.01609 0.0328 0.0155 1.0000 13.250 1.2419 0.02196 0.01674 0.0350 0.0151 1.0000 13.500 1.2519 0.02265 0.01751 0.0373 0.0147 1.0000 13.750 1.2609 0.02345 0.01837 0.0396 0.0144 1.0000 14.000 1.2713 0.02421 0.01918 0.0415 0.0139 1.0000 14.250 1.2800 0.02512 0.02014 0.0434 0.0135 1.0000 14.500 1.2836 0.02642 0.02151 0.0456 0.0132 1.0000 14.750 1.2822 0.02815 0.02333 0.0478 0.0128 1.0000 15.000 1.2794 0.03013 0.02542 0.0498 0.0126 1.0000 15.250 1.2890 0.03127 0.02665 0.0508 0.0123 1.0000 15.500 1.2901 0.03318 0.02867 0.0519 0.0122 1.0000 15.750 1.2922 0.03510 0.03069 0.0527 0.0120 1.0000 16.000 1.2936 0.03723 0.03292 0.0532 0.0118 1.0000 16.250 1.2921 0.03979 0.03559 0.0534 0.0116 1.0000 16.500 1.2873 0.04290 0.03881 0.0530 0.0115 1.0000 16.750 1.2858 0.04588 0.04189 0.0523 0.0113 1.0000 17.000 1.2770 0.04997 0.04611 0.0509 0.0112 1.0000 17.250 1.2672 0.05453 0.05079 0.0490 0.0112 1.0000 17.500 1.2528 0.06009 0.05649 0.0462 0.0111 1.0000 17.750 1.2375 0.06614 0.06266 0.0430 0.0109 1.0000 18.000 1.2174 0.07314 0.06981 0.0392 0.0110 1.0000 18.250 1.1981 0.08006 0.07685 0.0355 0.0109 1.0000 18.500 1.1703 0.08842 0.08535 0.0311 0.0109 1.0000 18.750 1.1398 0.09729 0.09436 0.0265 0.0109 1.0000