WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=500,000 Ncrit=5
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Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Reynolds number: 500,000 Max Cl/Cd: 125.49 at α=3.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx62k131-il-500000-n5.txt Download as CSV file: xf-fx62k131-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 62-K-131 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.1910 0.09773 0.09495 -0.0903 0.8852 0.0050
-10.250 -0.1888 0.09316 0.09034 -0.0925 0.8779 0.0046
-10.000 -0.1936 0.08583 0.08301 -0.0960 0.8709 0.0041
-9.750 -0.1918 0.08131 0.07846 -0.0986 0.8649 0.0041
-9.500 -0.1906 0.07657 0.07372 -0.1015 0.8591 0.0040
-9.250 -0.1904 0.07136 0.06849 -0.1051 0.8538 0.0040
-9.000 -0.1914 0.06538 0.06252 -0.1100 0.8491 0.0040
-8.750 -0.1961 0.05618 0.05328 -0.1199 0.8435 0.0040
-8.500 -0.2027 0.04977 0.04673 -0.1262 0.8381 0.0039
-8.250 -0.2083 0.04369 0.04045 -0.1324 0.8328 0.0039
-8.000 -0.2048 0.03820 0.03468 -0.1363 0.8286 0.0040
-7.750 -0.1931 0.03396 0.03014 -0.1386 0.8253 0.0042
-7.500 -0.1762 0.03047 0.02634 -0.1403 0.8225 0.0043
-7.250 -0.1566 0.02694 0.02249 -0.1417 0.8193 0.0045
-7.000 -0.1330 0.02517 0.02051 -0.1427 0.8164 0.0048
-6.750 -0.1082 0.02287 0.01790 -0.1436 0.8139 0.0054
-6.500 -0.0822 0.02022 0.01485 -0.1444 0.8116 0.0058
-6.000 -0.0286 0.01622 0.01021 -0.1452 0.8069 0.0059
-5.750 -0.0016 0.01494 0.00874 -0.1454 0.8044 0.0061
-5.500 0.0259 0.01396 0.00760 -0.1457 0.8020 0.0063
-5.250 0.0542 0.01325 0.00677 -0.1462 0.7996 0.0066
-5.000 0.0839 0.01225 0.00568 -0.1473 0.7974 0.0074
-4.500 0.1443 0.01144 0.00478 -0.1493 0.7929 0.0094
-4.250 0.1745 0.01116 0.00444 -0.1502 0.7901 0.0107
-4.000 0.2069 0.01060 0.00382 -0.1517 0.7872 0.0127
-3.750 0.2379 0.01033 0.00347 -0.1528 0.7841 0.0151
-3.500 0.2695 0.01007 0.00315 -0.1539 0.7813 0.0204
-3.250 0.3011 0.00979 0.00292 -0.1551 0.7781 0.0383
-3.000 0.3366 0.00922 0.00268 -0.1577 0.7753 0.1394
-2.750 0.3896 0.00782 0.00235 -0.1654 0.7731 0.4727
-2.500 0.4282 0.00748 0.00241 -0.1683 0.7708 0.6139
-2.250 0.4585 0.00751 0.00248 -0.1689 0.7684 0.6549
-2.000 0.4881 0.00757 0.00253 -0.1693 0.7657 0.6758
-1.750 0.5172 0.00760 0.00255 -0.1697 0.7626 0.6828
-1.500 0.5471 0.00763 0.00252 -0.1703 0.7595 0.6892
-1.250 0.5759 0.00767 0.00254 -0.1706 0.7565 0.6936
-1.000 0.6055 0.00772 0.00253 -0.1711 0.7538 0.6986
-0.750 0.6351 0.00775 0.00255 -0.1717 0.7503 0.7037
-0.500 0.6636 0.00780 0.00260 -0.1720 0.7467 0.7081
-0.250 0.6928 0.00784 0.00262 -0.1724 0.7433 0.7129
0.000 0.7225 0.00790 0.00263 -0.1730 0.7401 0.7175
0.250 0.7504 0.00795 0.00272 -0.1731 0.7360 0.7214
0.500 0.7790 0.00800 0.00278 -0.1734 0.7315 0.7258
0.750 0.8082 0.00805 0.00279 -0.1739 0.7267 0.7300
1.000 0.8362 0.00808 0.00285 -0.1741 0.7198 0.7329
1.250 0.8638 0.00813 0.00291 -0.1741 0.7134 0.7355
1.500 0.8920 0.00819 0.00298 -0.1744 0.7074 0.7383
1.750 0.9204 0.00824 0.00305 -0.1747 0.7014 0.7414
2.000 0.9493 0.00830 0.00311 -0.1751 0.6949 0.7445
2.250 0.9769 0.00837 0.00321 -0.1752 0.6872 0.7467
2.500 1.0041 0.00844 0.00331 -0.1753 0.6791 0.7489
2.750 1.0312 0.00854 0.00341 -0.1753 0.6706 0.7512
3.000 1.0586 0.00863 0.00353 -0.1753 0.6606 0.7539
3.250 1.0860 0.00874 0.00367 -0.1754 0.6498 0.7567
3.500 1.1131 0.00887 0.00379 -0.1755 0.6360 0.7595
3.750 1.1365 0.00910 0.00395 -0.1747 0.6109 0.7613
4.000 1.1563 0.00952 0.00419 -0.1732 0.5699 0.7634
4.250 1.1758 0.01001 0.00452 -0.1718 0.5320 0.7657
4.500 1.1968 0.01045 0.00486 -0.1707 0.5004 0.7681
4.750 1.2150 0.01106 0.00527 -0.1691 0.4549 0.7707
5.000 1.2313 0.01181 0.00576 -0.1672 0.4029 0.7735
5.250 1.2424 0.01279 0.00641 -0.1645 0.3384 0.7754
5.500 1.2522 0.01385 0.00713 -0.1615 0.2730 0.7773
5.750 1.2585 0.01509 0.00797 -0.1580 0.1996 0.7795
6.000 1.2659 0.01608 0.00874 -0.1547 0.1514 0.7820
6.250 1.2718 0.01725 0.00962 -0.1512 0.1017 0.7847
6.500 1.2828 0.01820 0.01041 -0.1487 0.0699 0.7871
6.750 1.2924 0.01922 0.01128 -0.1460 0.0424 0.7889
7.000 1.3028 0.02019 0.01217 -0.1435 0.0234 0.7908
7.250 1.3159 0.02101 0.01299 -0.1414 0.0151 0.7928
7.500 1.3278 0.02196 0.01393 -0.1393 0.0067 0.7950
7.750 1.3403 0.02291 0.01491 -0.1373 0.0041 0.7972
8.000 1.3539 0.02383 0.01592 -0.1355 0.0034 0.7994
8.250 1.3667 0.02484 0.01702 -0.1337 0.0030 0.8016
8.500 1.3789 0.02584 0.01812 -0.1319 0.0029 0.8033
8.750 1.3909 0.02689 0.01928 -0.1300 0.0027 0.8051
9.000 1.4022 0.02799 0.02048 -0.1282 0.0025 0.8069
9.250 1.4132 0.02917 0.02177 -0.1265 0.0024 0.8089
9.500 1.4234 0.03041 0.02309 -0.1247 0.0021 0.8111
9.750 1.4326 0.03179 0.02457 -0.1229 0.0020 0.8132
10.000 1.4402 0.03331 0.02619 -0.1210 0.0019 0.8152
10.250 1.4466 0.03496 0.02795 -0.1190 0.0018 0.8168
10.500 1.4514 0.03673 0.02985 -0.1169 0.0017 0.8185
10.750 1.4534 0.03883 0.03211 -0.1146 0.0016 0.8203
11.000 1.4524 0.04126 0.03469 -0.1122 0.0015 0.8219
11.250 1.4572 0.04321 0.03675 -0.1105 0.0015 0.8237
11.500 1.4611 0.04524 0.03891 -0.1087 0.0015 0.8257
11.750 1.4661 0.04725 0.04103 -0.1073 0.0014 0.8276
12.000 1.4689 0.04954 0.04345 -0.1057 0.0014 0.8294
12.250 1.4706 0.05194 0.04599 -0.1041 0.0014 0.8307
12.500 1.4717 0.05447 0.04867 -0.1027 0.0013 0.8321
12.750 1.4720 0.05717 0.05152 -0.1013 0.0013 0.8337
13.000 1.4714 0.06004 0.05455 -0.1000 0.0012 0.8354
13.250 1.4702 0.06307 0.05773 -0.0989 0.0012 0.8372
13.500 1.4682 0.06627 0.06108 -0.0979 0.0012 0.8390
13.750 1.4652 0.06971 0.06469 -0.0971 0.0011 0.8406
14.000 1.4612 0.07337 0.06852 -0.0965 0.0011 0.8421
14.250 1.4563 0.07729 0.07261 -0.0961 0.0011 0.8435
14.500 1.4508 0.08132 0.07683 -0.0959 0.0011 0.8448
14.750 1.4439 0.08570 0.08138 -0.0959 0.0010 0.8463
15.000 1.4357 0.09047 0.08637 -0.0963 0.0010 0.8478
15.250 1.4266 0.09545 0.09155 -0.0970 0.0010 0.8494
15.500 1.4168 0.10080 0.09708 -0.0982 0.0010 0.8511
15.750 1.4060 0.10647 0.10294 -0.0997 0.0010 0.8526
16.000 1.3943 0.11244 0.10910 -0.1017 0.0010 0.8541
16.250 1.3820 0.11881 0.11565 -0.1041 0.0010 0.8555
16.500 1.3686 0.12567 0.12270 -0.1072 0.0010 0.8569
16.750 1.3557 0.13262 0.12984 -0.1106 0.0010 0.8581
17.000 1.3413 0.14030 0.13771 -0.1148 0.0010 0.8593
17.250 1.3274 0.14810 0.14568 -0.1193 0.0010 0.8606
17.500 1.3134 0.15641 0.15416 -0.1244 0.0010 0.8620
17.750 1.2982 0.16548 0.16341 -0.1302 0.0010 0.8634
18.000 1.2841 0.17482 0.17290 -0.1363 0.0010 0.8649
18.250 1.2697 0.18486 0.18309 -0.1430 0.0010 0.8663
18.500 1.2519 0.19715 0.19552 -0.1511 0.0011 0.8674
18.750 1.2320 0.21153 0.21003 -0.1601 0.0011 0.8682
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