XFOIL Version 6.96 Calculated polar for: GOE 430 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -17.750 -0.7306 0.12681 0.12469 -0.0429 1.0000 0.0223 -17.500 -0.7890 0.11219 0.10992 -0.0514 1.0000 0.0232 -17.250 -0.8213 0.10281 0.10045 -0.0570 1.0000 0.0240 -17.000 -0.8504 0.09424 0.09179 -0.0624 1.0000 0.0245 -16.750 -0.8806 0.08573 0.08318 -0.0679 1.0000 0.0249 -16.500 -0.9140 0.07695 0.07429 -0.0738 1.0000 0.0252 -16.250 -0.9568 0.06712 0.06433 -0.0806 1.0000 0.0251 -16.000 -1.0064 0.05675 0.05381 -0.0882 1.0000 0.0249 -15.750 -1.0561 0.04676 0.04367 -0.0957 1.0000 0.0245 -15.250 -1.0890 0.03067 0.02723 -0.1153 0.9872 0.0253 -15.000 -1.0625 0.02597 0.02240 -0.1258 0.9794 0.0266 -14.750 -1.0319 0.02355 0.01986 -0.1321 0.9727 0.0281 -14.500 -1.0045 0.02226 0.01848 -0.1349 0.9661 0.0292 -14.250 -0.9771 0.02124 0.01735 -0.1369 0.9593 0.0299 -14.000 -0.9509 0.02032 0.01635 -0.1384 0.9520 0.0307 -13.750 -0.9245 0.01961 0.01559 -0.1394 0.9449 0.0316 -13.500 -0.8979 0.01903 0.01496 -0.1402 0.9388 0.0325 -13.250 -0.8713 0.01847 0.01434 -0.1409 0.9329 0.0332 -12.750 -0.8176 0.01744 0.01314 -0.1421 0.9224 0.0344 -12.500 -0.7905 0.01699 0.01261 -0.1426 0.9167 0.0349 -12.000 -0.7361 0.01601 0.01147 -0.1436 0.9062 0.0359 -11.750 -0.7087 0.01551 0.01092 -0.1442 0.9008 0.0366 -11.500 -0.6810 0.01515 0.01051 -0.1445 0.8956 0.0374 -11.250 -0.6529 0.01483 0.01016 -0.1449 0.8910 0.0381 -11.000 -0.6247 0.01454 0.00982 -0.1453 0.8863 0.0387 -10.750 -0.5964 0.01429 0.00953 -0.1456 0.8822 0.0395 -10.500 -0.5680 0.01402 0.00920 -0.1459 0.8786 0.0402 -10.250 -0.5394 0.01369 0.00881 -0.1464 0.8753 0.0406 -10.000 -0.5107 0.01336 0.00843 -0.1468 0.8717 0.0409 -9.750 -0.4821 0.01303 0.00803 -0.1472 0.8674 0.0412 -9.500 -0.4536 0.01272 0.00765 -0.1475 0.8627 0.0414 -9.250 -0.4248 0.01242 0.00729 -0.1478 0.8580 0.0416 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0.0553 -4.250 0.1579 0.00847 0.00226 -0.1534 0.6922 0.0566 -4.000 0.1868 0.00844 0.00216 -0.1535 0.6788 0.0580 -3.750 0.2157 0.00840 0.00207 -0.1536 0.6658 0.0608 -3.500 0.2447 0.00834 0.00197 -0.1538 0.6532 0.0649 -3.250 0.2736 0.00828 0.00188 -0.1540 0.6395 0.0727 -3.000 0.3026 0.00815 0.00181 -0.1542 0.6255 0.0989 -2.750 0.3314 0.00813 0.00178 -0.1544 0.6124 0.1139 -2.250 0.3891 0.00815 0.00175 -0.1546 0.5883 0.1276 -2.000 0.4178 0.00819 0.00174 -0.1547 0.5769 0.1319 -1.750 0.4465 0.00821 0.00174 -0.1548 0.5642 0.1376 -1.500 0.4752 0.00825 0.00173 -0.1548 0.5516 0.1422 -1.250 0.5039 0.00829 0.00174 -0.1549 0.5386 0.1458 -1.000 0.5323 0.00836 0.00175 -0.1549 0.5240 0.1488 -0.750 0.5606 0.00843 0.00176 -0.1549 0.5080 0.1537 -0.500 0.5889 0.00851 0.00179 -0.1549 0.4923 0.1587 -0.250 0.6169 0.00860 0.00182 -0.1549 0.4768 0.1657 0.000 0.6447 0.00870 0.00187 -0.1549 0.4589 0.1753 0.250 0.6722 0.00883 0.00195 -0.1548 0.4394 0.1900 0.500 0.7004 0.00885 0.00202 -0.1549 0.4269 0.2254 0.750 0.7286 0.00890 0.00210 -0.1550 0.4183 0.2564 1.000 0.7573 0.00892 0.00217 -0.1551 0.4129 0.2772 1.250 0.7856 0.00899 0.00224 -0.1551 0.4072 0.2913 1.500 0.8138 0.00906 0.00232 -0.1551 0.4018 0.3032 1.750 0.8423 0.00910 0.00239 -0.1551 0.3969 0.3141 2.000 0.8703 0.00918 0.00248 -0.1551 0.3901 0.3253 2.250 0.8983 0.00927 0.00257 -0.1551 0.3830 0.3398 2.500 0.9262 0.00934 0.00268 -0.1551 0.3741 0.3598 2.750 0.9541 0.00941 0.00279 -0.1550 0.3665 0.3852 3.000 0.9817 0.00950 0.00292 -0.1550 0.3560 0.4177 3.250 1.0089 0.00963 0.00307 -0.1549 0.3419 0.4480 3.500 1.0287 0.01042 0.00349 -0.1536 0.2619 0.4695 3.750 1.0516 0.01095 0.00386 -0.1528 0.2266 0.4860 4.000 1.0772 0.01121 0.00410 -0.1523 0.2144 0.5021 4.250 1.1037 0.01139 0.00429 -0.1521 0.2078 0.5177 4.500 1.1292 0.01164 0.00453 -0.1517 0.1989 0.5311 4.750 1.1558 0.01179 0.00472 -0.1514 0.1942 0.5492 5.000 1.1820 0.01195 0.00493 -0.1511 0.1895 0.5717 5.250 1.2078 0.01215 0.00516 -0.1507 0.1846 0.5938 5.500 1.2337 0.01233 0.00540 -0.1503 0.1803 0.6208 5.750 1.2595 0.01251 0.00562 -0.1499 0.1753 0.6451 6.000 1.2837 0.01281 0.00589 -0.1493 0.1656 0.6628 6.250 1.3080 0.01309 0.00616 -0.1487 0.1543 0.6778 6.500 1.3310 0.01345 0.00646 -0.1479 0.1399 0.6904 6.750 1.3512 0.01400 0.00690 -0.1467 0.1147 0.7034 7.000 1.3696 0.01465 0.00743 -0.1451 0.0924 0.7196 7.250 1.3910 0.01503 0.00784 -0.1441 0.0850 0.7441 7.500 1.4082 0.01495 0.00817 -0.1420 0.0821 1.0000 7.750 1.4298 0.01532 0.00854 -0.1409 0.0797 1.0000 8.000 1.4504 0.01572 0.00892 -0.1397 0.0767 1.0000 8.250 1.4700 0.01608 0.00929 -0.1382 0.0741 1.0000 8.500 1.4896 0.01641 0.00965 -0.1368 0.0727 1.0000 8.750 1.5086 0.01680 0.01005 -0.1353 0.0707 1.0000 9.000 1.5261 0.01727 0.01052 -0.1337 0.0676 1.0000 9.250 1.5421 0.01784 0.01107 -0.1318 0.0631 1.0000 9.500 1.5594 0.01833 0.01157 -0.1302 0.0582 1.0000 9.750 1.5567 0.02004 0.01304 -0.1259 0.0262 1.0000 10.000 1.5660 0.02110 0.01408 -0.1234 0.0189 1.0000 10.250 1.5789 0.02195 0.01494 -0.1214 0.0165 1.0000 10.500 1.5921 0.02281 0.01582 -0.1196 0.0150 1.0000 10.750 1.6052 0.02368 0.01673 -0.1179 0.0140 1.0000 11.000 1.6175 0.02464 0.01771 -0.1161 0.0131 1.0000 11.250 1.6289 0.02569 0.01879 -0.1143 0.0123 1.0000 11.500 1.6413 0.02668 0.01982 -0.1126 0.0118 1.0000 11.750 1.6529 0.02775 0.02094 -0.1110 0.0114 1.0000 12.000 1.6637 0.02891 0.02214 -0.1093 0.0109 1.0000 12.250 1.6736 0.03017 0.02344 -0.1077 0.0104 1.0000 12.500 1.6822 0.03156 0.02487 -0.1060 0.0100 1.0000 12.750 1.6897 0.03307 0.02643 -0.1043 0.0096 1.0000 13.000 1.6981 0.03455 0.02797 -0.1028 0.0094 1.0000 13.250 1.7062 0.03608 0.02955 -0.1014 0.0092 1.0000 13.500 1.7134 0.03772 0.03126 -0.1000 0.0090 1.0000 13.750 1.7199 0.03948 0.03307 -0.0987 0.0087 1.0000 14.000 1.7257 0.04135 0.03501 -0.0974 0.0085 1.0000 14.250 1.7309 0.04335 0.03707 -0.0962 0.0083 1.0000 14.500 1.7351 0.04549 0.03927 -0.0951 0.0081 1.0000 14.750 1.7386 0.04778 0.04162 -0.0941 0.0079 1.0000 15.000 1.7411 0.05025 0.04415 -0.0932 0.0077 1.0000 15.250 1.7425 0.05291 0.04689 -0.0924 0.0075 1.0000 15.500 1.7417 0.05587 0.04993 -0.0917 0.0073 1.0000 15.750 1.7437 0.05856 0.05269 -0.0912 0.0072 1.0000 16.000 1.7448 0.06141 0.05562 -0.0907 0.0071 1.0000 16.250 1.7452 0.06441 0.05870 -0.0903 0.0069 1.0000 16.500 1.7444 0.06760 0.06197 -0.0901 0.0068 1.0000 16.750 1.7425 0.07094 0.06540 -0.0899 0.0067 1.0000 17.000 1.7397 0.07446 0.06900 -0.0899 0.0066 1.0000 17.250 1.7361 0.07815 0.07278 -0.0899 0.0065 1.0000 17.500 1.7319 0.08198 0.07669 -0.0901 0.0064 1.0000 17.750 1.7270 0.08594 0.08075 -0.0905 0.0064 1.0000 18.000 1.7211 0.09006 0.08497 -0.0909 0.0063 1.0000 18.250 1.7149 0.09432 0.08931 -0.0915 0.0062 1.0000 18.500 1.7080 0.09873 0.09381 -0.0922 0.0061 1.0000 18.750 1.7003 0.10330 0.09847 -0.0932 0.0060 1.0000 19.000 1.6921 0.10798 0.10325 -0.0942 0.0060 1.0000 19.250 1.6833 0.11278 0.10815 -0.0954 0.0059 1.0000