GOE 459 AIRFOIL (goe459-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 459 AIRFOIL (goe459-il) Reynolds number: 500,000 Max Cl/Cd: 59.03 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe459-il-500000.txt Download as CSV file: xf-goe459-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 459 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
------ -------- --------- --------- -------- -------- --------
-19.500 -0.9582 0.13933 0.13626 -0.0066 1.0000 0.0150
-19.250 -0.9769 0.13140 0.12821 -0.0108 1.0000 0.0148
-19.000 -0.9965 0.12341 0.12009 -0.0152 1.0000 0.0149
-18.750 -1.0140 0.11615 0.11271 -0.0189 1.0000 0.0149
-18.500 -1.0328 0.10862 0.10505 -0.0229 1.0000 0.0151
-18.250 -1.0472 0.10235 0.09868 -0.0260 1.0000 0.0150
-18.000 -1.0644 0.09551 0.09170 -0.0295 1.0000 0.0151
-17.750 -1.0799 0.08912 0.08519 -0.0328 1.0000 0.0152
-17.500 -1.0935 0.08321 0.07915 -0.0357 1.0000 0.0152
-17.250 -1.1066 0.07742 0.07324 -0.0386 1.0000 0.0153
-17.000 -1.1192 0.07199 0.06769 -0.0411 1.0000 0.0153
-16.750 -1.1311 0.06679 0.06235 -0.0434 1.0000 0.0154
-16.500 -1.1399 0.06212 0.05754 -0.0455 1.0000 0.0157
-16.250 -1.1495 0.05765 0.05293 -0.0473 1.0000 0.0157
-16.000 -1.1612 0.05310 0.04827 -0.0488 1.0000 0.0159
-15.750 -1.1733 0.04872 0.04379 -0.0501 1.0000 0.0162
-15.500 -1.1795 0.04521 0.04017 -0.0508 1.0000 0.0163
-15.250 -1.1865 0.04181 0.03666 -0.0512 1.0000 0.0166
-15.000 -1.1932 0.03865 0.03340 -0.0513 1.0000 0.0171
-14.750 -1.1930 0.03634 0.03101 -0.0509 1.0000 0.0175
-14.500 -1.1924 0.03422 0.02878 -0.0502 1.0000 0.0180
-14.250 -1.1910 0.03229 0.02676 -0.0491 1.0000 0.0184
-14.000 -1.1870 0.03070 0.02505 -0.0479 1.0000 0.0189
-13.750 -1.1859 0.02899 0.02323 -0.0461 1.0000 0.0194
-13.500 -1.1879 0.02722 0.02140 -0.0438 1.0000 0.0203
-13.250 -1.1838 0.02597 0.02009 -0.0417 1.0000 0.0210
-13.000 -1.1780 0.02490 0.01896 -0.0394 1.0000 0.0219
-12.750 -1.1705 0.02398 0.01794 -0.0370 1.0000 0.0232
-12.500 -1.1659 0.02298 0.01691 -0.0342 1.0000 0.0245
-12.250 -1.1564 0.02230 0.01622 -0.0317 1.0000 0.0266
-12.000 -1.1472 0.02165 0.01552 -0.0290 1.0000 0.0290
-11.750 -1.1325 0.02132 0.01523 -0.0270 1.0000 0.0325
-11.500 -1.1201 0.02094 0.01482 -0.0246 1.0000 0.0355
-11.250 -1.1031 0.02086 0.01473 -0.0227 1.0000 0.0386
-11.000 -1.0832 0.02099 0.01477 -0.0213 1.0000 0.0410
-10.750 -1.0807 0.02031 0.01410 -0.0170 1.0000 0.0432
-10.500 -1.0685 0.02008 0.01386 -0.0143 1.0000 0.0450
-10.250 -1.0531 0.01988 0.01362 -0.0121 1.0000 0.0470
-10.000 -1.0368 0.01972 0.01337 -0.0101 1.0000 0.0486
-9.750 -1.0233 0.01929 0.01287 -0.0076 1.0000 0.0501
-9.500 -1.0139 0.01853 0.01213 -0.0045 1.0000 0.0521
-9.250 -1.0000 0.01813 0.01170 -0.0021 1.0000 0.0535
-9.000 -0.9854 0.01777 0.01131 0.0003 1.0000 0.0551
-8.750 -0.9704 0.01744 0.01093 0.0026 1.0000 0.0565
-8.500 -0.9549 0.01714 0.01058 0.0049 1.0000 0.0578
-8.250 -0.9388 0.01691 0.01029 0.0071 1.0000 0.0588
-8.000 -0.9276 0.01633 0.00967 0.0100 1.0000 0.0604
-7.750 -0.9169 0.01576 0.00909 0.0131 1.0000 0.0621
-7.500 -0.9039 0.01537 0.00869 0.0158 1.0000 0.0638
-7.250 -0.8894 0.01509 0.00839 0.0182 1.0000 0.0656
-7.000 -0.8702 0.01480 0.00807 0.0196 0.9995 0.0673
-6.750 -0.8333 0.01452 0.00775 0.0175 0.9968 0.0696
-6.500 -0.7957 0.01405 0.00723 0.0151 0.9938 0.0714
-6.250 -0.7616 0.01351 0.00668 0.0135 0.9897 0.0743
-6.000 -0.7262 0.01309 0.00627 0.0117 0.9862 0.0774
-5.750 -0.6899 0.01276 0.00591 0.0097 0.9838 0.0810
-5.500 -0.6586 0.01234 0.00553 0.0088 0.9799 0.0879
-5.250 -0.6280 0.01180 0.00516 0.0079 0.9753 0.1107
-5.000 -0.5952 0.01118 0.00481 0.0065 0.9722 0.1614
-4.750 -0.5601 0.01072 0.00452 0.0047 0.9700 0.1975
-4.500 -0.5347 0.01031 0.00426 0.0051 0.9629 0.2301
-4.250 -0.5003 0.00992 0.00402 0.0035 0.9595 0.2653
-4.000 -0.4641 0.00954 0.00377 0.0016 0.9572 0.2985
-3.750 -0.4378 0.00916 0.00352 0.0019 0.9502 0.3312
-3.500 -0.4063 0.00867 0.00326 0.0010 0.9460 0.3813
-3.250 -0.3713 0.00820 0.00306 -0.0007 0.9430 0.4452
-3.000 -0.3429 0.00789 0.00290 -0.0007 0.9353 0.4887
-2.750 -0.3078 0.00761 0.00273 -0.0023 0.9300 0.5226
-2.500 -0.2737 0.00736 0.00258 -0.0035 0.9231 0.5509
-2.250 -0.2389 0.00714 0.00243 -0.0049 0.9138 0.5767
-2.000 -0.2081 0.00696 0.00232 -0.0053 0.9017 0.6046
-1.750 -0.1781 0.00681 0.00224 -0.0056 0.8891 0.6323
-1.500 -0.1491 0.00672 0.00217 -0.0056 0.8759 0.6557
-1.250 -0.1223 0.00664 0.00211 -0.0051 0.8611 0.6769
-1.000 -0.0973 0.00658 0.00207 -0.0042 0.8451 0.7003
-0.750 -0.0727 0.00653 0.00204 -0.0032 0.8281 0.7193
-0.500 -0.0482 0.00649 0.00201 -0.0022 0.8113 0.7376
-0.250 -0.0239 0.00647 0.00199 -0.0011 0.7935 0.7556
0.000 0.0000 0.00646 0.00199 0.0000 0.7747 0.7746
0.250 0.0240 0.00647 0.00200 0.0011 0.7559 0.7938
0.500 0.0481 0.00649 0.00201 0.0022 0.7377 0.8118
0.750 0.0726 0.00653 0.00204 0.0032 0.7195 0.8287
1.000 0.0971 0.00658 0.00207 0.0042 0.6992 0.8453
1.250 0.1225 0.00664 0.00212 0.0050 0.6784 0.8612
1.500 0.1491 0.00672 0.00217 0.0056 0.6551 0.8758
1.750 0.1781 0.00681 0.00224 0.0056 0.6319 0.8891
2.000 0.2080 0.00697 0.00232 0.0053 0.6038 0.9017
2.250 0.2390 0.00715 0.00243 0.0048 0.5762 0.9140
2.500 0.2736 0.00737 0.00258 0.0035 0.5501 0.9231
2.750 0.3077 0.00761 0.00273 0.0023 0.5216 0.9300
3.000 0.3428 0.00789 0.00290 0.0008 0.4874 0.9353
3.250 0.3713 0.00820 0.00306 0.0007 0.4445 0.9430
3.500 0.4063 0.00866 0.00326 -0.0010 0.3820 0.9460
3.750 0.4378 0.00916 0.00352 -0.0019 0.3311 0.9502
4.000 0.4641 0.00954 0.00377 -0.0016 0.2981 0.9572
4.250 0.5004 0.00992 0.00402 -0.0035 0.2653 0.9595
4.500 0.5347 0.01031 0.00426 -0.0051 0.2297 0.9629
4.750 0.5598 0.01073 0.00452 -0.0046 0.1967 0.9702
5.000 0.5952 0.01119 0.00481 -0.0065 0.1607 0.9722
5.250 0.6283 0.01179 0.00516 -0.0080 0.1112 0.9753
5.500 0.6587 0.01234 0.00553 -0.0088 0.0878 0.9799
5.750 0.6901 0.01276 0.00592 -0.0097 0.0808 0.9838
6.000 0.7265 0.01309 0.00627 -0.0117 0.0776 0.9863
6.250 0.7618 0.01350 0.00668 -0.0135 0.0744 0.9897
6.500 0.7958 0.01405 0.00723 -0.0151 0.0715 0.9938
6.750 0.8332 0.01452 0.00774 -0.0175 0.0697 0.9968
7.000 0.8701 0.01480 0.00807 -0.0196 0.0675 0.9995
7.250 0.8896 0.01507 0.00837 -0.0182 0.0655 1.0000
7.500 0.9038 0.01537 0.00869 -0.0158 0.0639 1.0000
7.750 0.9169 0.01576 0.00909 -0.0131 0.0622 1.0000
8.000 0.9277 0.01631 0.00965 -0.0101 0.0604 1.0000
8.250 0.9384 0.01694 0.01032 -0.0070 0.0589 1.0000
8.500 0.9544 0.01718 0.01061 -0.0048 0.0579 1.0000
8.750 0.9703 0.01744 0.01093 -0.0026 0.0566 1.0000
9.000 0.9853 0.01778 0.01132 -0.0003 0.0551 1.0000
9.250 1.0001 0.01812 0.01170 0.0020 0.0536 1.0000
9.500 1.0139 0.01853 0.01212 0.0045 0.0521 1.0000
9.750 1.0231 0.01930 0.01288 0.0076 0.0500 1.0000
10.000 1.0367 0.01973 0.01338 0.0101 0.0486 1.0000
10.250 1.0534 0.01986 0.01360 0.0121 0.0470 1.0000
10.500 1.0688 0.02007 0.01385 0.0142 0.0450 1.0000
10.750 1.0813 0.02028 0.01407 0.0169 0.0431 1.0000
11.000 1.0835 0.02099 0.01476 0.0212 0.0410 1.0000
11.250 1.1029 0.02088 0.01476 0.0228 0.0387 1.0000
11.500 1.1198 0.02096 0.01485 0.0246 0.0357 1.0000
11.750 1.1331 0.02131 0.01521 0.0269 0.0322 1.0000
12.000 1.1472 0.02167 0.01553 0.0290 0.0288 1.0000
12.250 1.1570 0.02229 0.01620 0.0316 0.0265 1.0000
12.500 1.1662 0.02298 0.01691 0.0341 0.0246 1.0000
12.750 1.1711 0.02398 0.01794 0.0370 0.0231 1.0000
13.000 1.1784 0.02490 0.01896 0.0393 0.0221 1.0000
13.250 1.1844 0.02595 0.02009 0.0416 0.0212 1.0000
13.500 1.1882 0.02724 0.02141 0.0438 0.0201 1.0000
13.750 1.1875 0.02892 0.02315 0.0460 0.0195 1.0000
14.000 1.1889 0.03059 0.02493 0.0477 0.0190 1.0000
14.250 1.1909 0.03235 0.02681 0.0490 0.0185 1.0000
14.500 1.1941 0.03414 0.02870 0.0500 0.0178 1.0000
14.750 1.1948 0.03625 0.03091 0.0507 0.0175 1.0000
15.000 1.1953 0.03852 0.03327 0.0511 0.0170 1.0000
15.250 1.1902 0.04153 0.03638 0.0511 0.0167 1.0000
15.500 1.1840 0.04482 0.03977 0.0507 0.0164 1.0000
15.750 1.1767 0.04845 0.04351 0.0499 0.0162 1.0000
16.000 1.1633 0.05298 0.04815 0.0486 0.0159 1.0000
16.250 1.1508 0.05762 0.05290 0.0471 0.0157 1.0000
16.500 1.1422 0.06206 0.05748 0.0453 0.0155 1.0000
16.750 1.1324 0.06679 0.06234 0.0432 0.0155 1.0000
17.000 1.1211 0.07190 0.06758 0.0409 0.0154 1.0000
17.250 1.1104 0.07719 0.07301 0.0383 0.0152 1.0000
17.500 1.0958 0.08314 0.07909 0.0354 0.0152 1.0000
17.750 1.0825 0.08900 0.08506 0.0325 0.0152 1.0000
18.000 1.0673 0.09537 0.09156 0.0293 0.0151 1.0000
18.250 1.0495 0.10234 0.09867 0.0257 0.0149 1.0000
18.500 1.0331 0.10911 0.10556 0.0222 0.0149 1.0000
18.750 1.0152 0.11634 0.11291 0.0185 0.0148 1.0000
19.000 0.9986 0.12351 0.12020 0.0147 0.0148 1.0000
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