XFOIL Version 6.96 Calculated polar for: WORTMANN FX 2 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -18.000 -0.3538 0.09274 0.08733 -0.1695 0.8568 0.0173 -17.750 -0.3830 0.08421 0.07858 -0.1739 0.8565 0.0172 -17.500 -0.4051 0.07750 0.07168 -0.1772 0.8561 0.0174 -17.250 -0.4206 0.07226 0.06626 -0.1795 0.8557 0.0176 -17.000 -0.4324 0.06784 0.06167 -0.1812 0.8553 0.0178 -16.750 -0.4423 0.06390 0.05756 -0.1823 0.8548 0.0180 -16.500 -0.4482 0.06063 0.05413 -0.1831 0.8543 0.0182 -16.250 -0.4528 0.05766 0.05097 -0.1836 0.8538 0.0186 -16.000 -0.4550 0.05505 0.04818 -0.1838 0.8533 0.0189 -15.750 -0.4559 0.05271 0.04580 -0.1838 0.8528 0.0193 -15.500 -0.4546 0.05070 0.04370 -0.1837 0.8522 0.0197 -15.250 -0.4521 0.04890 0.04184 -0.1836 0.8517 0.0202 -15.000 -0.4483 0.04722 0.04007 -0.1832 0.8511 0.0207 -14.750 -0.4434 0.04569 0.03845 -0.1828 0.8506 0.0213 -14.500 -0.4377 0.04428 0.03695 -0.1823 0.8499 0.0222 -14.250 -0.4308 0.04296 0.03550 -0.1817 0.8492 0.0231 -14.000 -0.4226 0.04173 0.03413 -0.1809 0.8483 0.0239 -13.750 -0.4166 0.04047 0.03286 -0.1801 0.8476 0.0248 -13.500 -0.4087 0.03939 0.03174 -0.1793 0.8471 0.0256 -13.250 -0.3997 0.03843 0.03070 -0.1785 0.8465 0.0267 -13.000 -0.3897 0.03753 0.02974 -0.1777 0.8459 0.0281 -12.750 -0.3782 0.03674 0.02884 -0.1768 0.8454 0.0300 -12.500 -0.3694 0.03588 0.02799 -0.1758 0.8448 0.0317 -12.250 -0.3585 0.03516 0.02723 -0.1749 0.8443 0.0335 -12.000 -0.3467 0.03450 0.02650 -0.1739 0.8438 0.0360 -11.750 -0.3356 0.03383 0.02580 -0.1729 0.8432 0.0382 -11.500 -0.3240 0.03327 0.02520 -0.1719 0.8427 0.0412 -11.250 -0.3107 0.03279 0.02463 -0.1709 0.8422 0.0445 -11.000 -0.3001 0.03221 0.02406 -0.1697 0.8418 0.0472 -10.750 -0.2877 0.03176 0.02358 -0.1686 0.8413 0.0503 -10.500 -0.2734 0.03141 0.02313 -0.1676 0.8408 0.0539 -10.250 -0.2675 0.03102 0.02277 -0.1653 0.8397 0.0564 -10.000 -0.2615 0.03075 0.02251 -0.1630 0.8386 0.0591 -9.750 -0.2547 0.03059 0.02233 -0.1606 0.8376 0.0622 -9.500 -0.2486 0.03051 0.02221 -0.1580 0.8365 0.0648 -9.250 -0.2461 0.03043 0.02211 -0.1548 0.8353 0.0672 -9.000 -0.2490 0.03030 0.02203 -0.1508 0.8338 0.0698 -8.750 -0.2517 0.03030 0.02204 -0.1467 0.8323 0.0724 -8.500 -0.2507 0.03019 0.02190 -0.1431 0.8306 0.0755 -8.250 -0.2488 0.03008 0.02175 -0.1396 0.8292 0.0785 -8.000 -0.2486 0.02995 0.02158 -0.1359 0.8280 0.0812 -7.750 -0.2517 0.02972 0.02136 -0.1317 0.8268 0.0843 -7.500 -0.4161 0.03319 0.02496 -0.0974 0.8153 0.0727 -7.250 -0.4229 0.03289 0.02462 -0.0924 0.8132 0.0752 -7.000 -0.4234 0.03248 0.02415 -0.0885 0.8117 0.0779 -6.500 -0.4882 0.03262 0.02421 -0.0700 0.8031 0.0781 -6.250 -0.4856 0.03227 0.02381 -0.0668 0.8005 0.0812 -6.000 -0.4744 0.03164 0.02317 -0.0651 0.7986 0.0861 -5.750 -0.4577 0.03118 0.02268 -0.0642 0.7974 0.0910 -5.500 -0.4381 0.03072 0.02220 -0.0638 0.7964 0.0982 -5.250 -0.4163 0.03013 0.02168 -0.0638 0.7955 0.1134 -5.000 -0.3934 0.02940 0.02111 -0.0642 0.7948 0.1527 -4.750 -0.4104 0.02962 0.02141 -0.0577 0.7882 0.1707 -4.500 -0.3949 0.02863 0.02082 -0.0573 0.7857 0.2519 -4.250 -0.3758 0.02695 0.01998 -0.0583 0.7842 0.4209 -4.000 -0.3544 0.02682 0.02047 -0.0574 0.7829 0.5499 -3.750 -0.3281 0.02720 0.02093 -0.0569 0.7819 0.5824 -3.500 -0.2997 0.02774 0.02149 -0.0567 0.7810 0.6072 -3.250 -0.2695 0.02824 0.02194 -0.0569 0.7803 0.6233 -3.000 -0.2734 0.02906 0.02276 -0.0520 0.7735 0.6320 -2.750 -0.2501 0.02955 0.02317 -0.0513 0.7711 0.6414 -2.500 -0.2221 0.02985 0.02335 -0.0517 0.7694 0.6517 -2.250 -0.1953 0.03037 0.02385 -0.0512 0.7682 0.6568 -2.000 -0.1641 0.03041 0.02375 -0.0526 0.7673 0.6646 -1.750 -0.1355 0.03068 0.02399 -0.0527 0.7664 0.6671 -1.500 -0.1353 0.03133 0.02464 -0.0485 0.7593 0.6700 -1.250 -0.1115 0.03158 0.02485 -0.0481 0.7570 0.6744 -1.000 -0.0813 0.03150 0.02463 -0.0496 0.7555 0.6800 -0.750 -0.0533 0.03160 0.02471 -0.0498 0.7543 0.6815 -0.500 -0.0232 0.03157 0.02463 -0.0506 0.7533 0.6827 -0.250 -0.0149 0.03198 0.02504 -0.0480 0.7474 0.6844 0.000 0.0070 0.03211 0.02514 -0.0476 0.7441 0.6862 0.250 0.0350 0.03209 0.02507 -0.0482 0.7423 0.6881 0.500 0.0650 0.03202 0.02495 -0.0492 0.7409 0.6902 0.750 0.0962 0.03193 0.02480 -0.0505 0.7399 0.6926 1.000 0.1293 0.03180 0.02459 -0.0522 0.7391 0.6955 1.500 0.1579 0.03237 0.02519 -0.0489 0.7285 0.6979 1.750 0.1876 0.03230 0.02512 -0.0497 0.7271 0.6992 2.000 0.2183 0.03220 0.02502 -0.0505 0.7260 0.7007 2.500 0.2515 0.03275 0.02557 -0.0482 0.7153 0.7049 2.750 0.2818 0.03263 0.02545 -0.0492 0.7137 0.7071 3.000 0.3140 0.03245 0.02525 -0.0504 0.7125 0.7094 3.500 0.3498 0.03290 0.02573 -0.0486 0.7012 0.7127 3.750 0.3798 0.03271 0.02558 -0.0492 0.6995 0.7139 4.000 0.4111 0.03247 0.02538 -0.0501 0.6983 0.7153 4.500 0.4473 0.03295 0.02594 -0.0482 0.6864 0.7185 4.750 0.4786 0.03268 0.02571 -0.0491 0.6847 0.7203 5.000 0.5110 0.03236 0.02542 -0.0502 0.6835 0.7221 5.250 0.5191 0.03308 0.02617 -0.0480 0.6732 0.7241 5.500 0.5499 0.03283 0.02596 -0.0489 0.6710 0.7260 5.750 0.5815 0.03244 0.02562 -0.0498 0.6694 0.7275 6.250 0.6206 0.03277 0.02611 -0.0481 0.6569 0.7303 6.500 0.6544 0.03194 0.02535 -0.0489 0.6540 0.7317 6.750 0.6690 0.03225 0.02573 -0.0474 0.6427 0.7332 7.000 0.7064 0.03117 0.02469 -0.0486 0.6380 0.7347 7.250 0.7270 0.03115 0.02472 -0.0478 0.6247 0.7362 7.500 0.7535 0.03086 0.02448 -0.0477 0.6124 0.7378 7.750 0.7867 0.03023 0.02387 -0.0486 0.6019 0.7393 8.000 0.8251 0.02931 0.02297 -0.0501 0.5901 0.7407 8.250 0.8581 0.02876 0.02243 -0.0510 0.5725 0.7421 8.500 0.8902 0.02823 0.02189 -0.0517 0.5509 0.7431 8.750 0.9231 0.02764 0.02122 -0.0524 0.5233 0.7442 9.000 0.9449 0.02767 0.02109 -0.0517 0.4853 0.7454 9.250 0.9565 0.02830 0.02151 -0.0497 0.4454 0.7467 9.500 0.9605 0.02940 0.02239 -0.0468 0.4022 0.7480 9.750 0.9615 0.03076 0.02353 -0.0438 0.3600 0.7493 10.000 0.9622 0.03226 0.02481 -0.0409 0.3170 0.7506 10.250 0.9606 0.03398 0.02627 -0.0379 0.2706 0.7517 10.500 0.9612 0.03567 0.02774 -0.0354 0.2276 0.7528 10.750 0.9634 0.03735 0.02920 -0.0332 0.1903 0.7539 11.000 0.9681 0.03894 0.03061 -0.0313 0.1589 0.7552 11.250 0.9764 0.04032 0.03188 -0.0299 0.1330 0.7567 11.500 0.9840 0.04179 0.03323 -0.0286 0.1083 0.7581 11.750 0.9925 0.04316 0.03453 -0.0272 0.0932 0.7595 12.000 1.0024 0.04446 0.03583 -0.0261 0.0833 0.7610 12.250 1.0121 0.04581 0.03722 -0.0249 0.0756 0.7625 12.500 1.0237 0.04705 0.03852 -0.0241 0.0689 0.7635 12.750 1.0336 0.04847 0.03996 -0.0231 0.0614 0.7644 13.000 1.0455 0.04976 0.04130 -0.0224 0.0533 0.7652 13.250 1.0560 0.05119 0.04275 -0.0216 0.0448 0.7660 13.500 1.0651 0.05278 0.04431 -0.0208 0.0363 0.7668 13.750 1.0735 0.05447 0.04602 -0.0200 0.0317 0.7676 14.000 1.0808 0.05630 0.04788 -0.0192 0.0285 0.7684 14.250 1.0884 0.05814 0.04981 -0.0185 0.0264 0.7695 14.500 1.0960 0.06002 0.05177 -0.0179 0.0248 0.7705 14.750 1.1014 0.06218 0.05399 -0.0172 0.0231 0.7714 15.000 1.1049 0.06460 0.05647 -0.0166 0.0220 0.7721 15.250 1.1122 0.06665 0.05865 -0.0163 0.0212 0.7728 15.500 1.1178 0.06894 0.06105 -0.0159 0.0202 0.7735 15.750 1.1226 0.07131 0.06354 -0.0156 0.0194 0.7742 16.000 1.1272 0.07375 0.06610 -0.0154 0.0188 0.7748 16.250 1.1306 0.07637 0.06882 -0.0152 0.0182 0.7755 16.500 1.1320 0.07926 0.07181 -0.0152 0.0176 0.7762 16.750 1.1331 0.08226 0.07490 -0.0152 0.0170 0.7769 17.000 1.1381 0.08483 0.07762 -0.0154 0.0165 0.7776 17.250 1.1416 0.08760 0.08053 -0.0156 0.0160 0.7784 17.500 1.1447 0.09045 0.08351 -0.0160 0.0156 0.7792 17.750 1.1472 0.09343 0.08662 -0.0164 0.0152 0.7801 18.000 1.1494 0.09649 0.08980 -0.0170 0.0148 0.7809 18.250 1.1513 0.09961 0.09305 -0.0177 0.0146 0.7818 18.500 1.1527 0.10282 0.09637 -0.0185 0.0143 0.7827 18.750 1.1534 0.10614 0.09978 -0.0195 0.0140 0.7836 19.000 1.1543 0.10943 0.10317 -0.0205 0.0137 0.7846 19.250 1.1550 0.11274 0.10655 -0.0216 0.0135 0.7855