WORTMANN FX 2 AIRFOIL (fx2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 2 AIRFOIL (fx2-il) Reynolds number: 1,000,000 Max Cl/Cd: 110.99 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx2-il-1000000-n5.txt Download as CSV file: xf-fx2-il-1000000-n5.csv |
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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7032 0.06904 0.06431 -0.1623 0.8053 0.0065
-19.500 -0.7044 0.06563 0.06081 -0.1642 0.8050 0.0066
-19.250 -0.7050 0.06236 0.05745 -0.1661 0.8047 0.0067
-19.000 -0.7074 0.05897 0.05396 -0.1678 0.8045 0.0067
-18.750 -0.7058 0.05614 0.05105 -0.1692 0.8042 0.0068
-18.500 -0.7054 0.05330 0.04812 -0.1705 0.8039 0.0069
-18.250 -0.7041 0.05065 0.04539 -0.1716 0.8036 0.0070
-18.000 -0.7013 0.04822 0.04289 -0.1726 0.8033 0.0071
-17.750 -0.6957 0.04616 0.04076 -0.1734 0.8030 0.0072
-17.500 -0.6896 0.04420 0.03875 -0.1741 0.8026 0.0074
-17.250 -0.6816 0.04247 0.03696 -0.1747 0.8023 0.0075
-17.000 -0.6719 0.04092 0.03536 -0.1752 0.8020 0.0077
-16.750 -0.6627 0.03937 0.03376 -0.1756 0.8017 0.0079
-16.500 -0.6520 0.03798 0.03231 -0.1760 0.8014 0.0081
-16.250 -0.6418 0.03661 0.03087 -0.1763 0.8010 0.0082
-16.000 -0.6294 0.03542 0.02964 -0.1765 0.8007 0.0085
-15.750 -0.6183 0.03417 0.02833 -0.1767 0.8004 0.0086
-15.500 -0.6043 0.03317 0.02728 -0.1769 0.8001 0.0089
-15.250 -0.5931 0.03199 0.02606 -0.1768 0.7998 0.0091
-15.000 -0.5809 0.03093 0.02496 -0.1767 0.7995 0.0094
-14.750 -0.5680 0.02994 0.02393 -0.1767 0.7991 0.0097
-14.500 -0.5542 0.02904 0.02299 -0.1765 0.7988 0.0100
-14.250 -0.5403 0.02816 0.02208 -0.1764 0.7985 0.0103
-14.000 -0.5258 0.02736 0.02124 -0.1762 0.7982 0.0107
-13.750 -0.5108 0.02660 0.02044 -0.1760 0.7978 0.0111
-13.500 -0.4951 0.02590 0.01971 -0.1757 0.7975 0.0113
-13.250 -0.4797 0.02520 0.01898 -0.1755 0.7971 0.0117
-13.000 -0.4659 0.02444 0.01820 -0.1750 0.7967 0.0124
-12.750 -0.4505 0.02379 0.01752 -0.1745 0.7962 0.0130
-12.500 -0.4348 0.02318 0.01689 -0.1741 0.7957 0.0138
-12.250 -0.4188 0.02259 0.01628 -0.1737 0.7953 0.0144
-12.000 -0.4024 0.02205 0.01571 -0.1733 0.7948 0.0148
-11.750 -0.3871 0.02149 0.01513 -0.1727 0.7944 0.0160
-11.500 -0.3721 0.02093 0.01458 -0.1719 0.7940 0.0175
-11.250 -0.3566 0.02043 0.01407 -0.1712 0.7939 0.0185
-11.000 -0.3420 0.01990 0.01353 -0.1703 0.7937 0.0203
-10.750 -0.3272 0.01940 0.01305 -0.1694 0.7934 0.0226
-10.500 -0.3120 0.01893 0.01259 -0.1684 0.7932 0.0252
-10.250 -0.2973 0.01845 0.01214 -0.1674 0.7930 0.0296
-10.000 -0.2825 0.01799 0.01172 -0.1664 0.7927 0.0337
-9.750 -0.2660 0.01760 0.01134 -0.1655 0.7924 0.0366
-9.500 -0.2498 0.01722 0.01096 -0.1646 0.7921 0.0392
-9.250 -0.2336 0.01684 0.01060 -0.1636 0.7918 0.0418
-9.000 -0.2168 0.01650 0.01026 -0.1627 0.7915 0.0445
-8.750 -0.2001 0.01616 0.00991 -0.1617 0.7911 0.0457
-8.500 -0.1850 0.01577 0.00955 -0.1605 0.7908 0.0490
-8.250 -0.1689 0.01543 0.00922 -0.1594 0.7904 0.0512
-8.000 -0.1524 0.01510 0.00889 -0.1583 0.7900 0.0530
-7.750 -0.1351 0.01481 0.00859 -0.1573 0.7896 0.0542
-7.500 -0.1197 0.01446 0.00824 -0.1560 0.7890 0.0565
-7.250 -0.1056 0.01407 0.00787 -0.1545 0.7885 0.0597
-7.000 -0.0909 0.01372 0.00753 -0.1530 0.7880 0.0628
-6.750 -0.0751 0.01340 0.00721 -0.1517 0.7876 0.0647
-6.500 -0.0593 0.01310 0.00690 -0.1504 0.7871 0.0660
-6.250 -0.0466 0.01275 0.00655 -0.1485 0.7866 0.0695
-6.000 -0.0382 0.01242 0.00623 -0.1458 0.7861 0.0736
-5.750 -0.0315 0.01213 0.00595 -0.1429 0.7855 0.0769
-5.500 -0.0154 0.01185 0.00567 -0.1417 0.7850 0.0824
-5.250 -0.0001 0.01153 0.00541 -0.1402 0.7846 0.0989
-5.000 0.0117 0.01101 0.00508 -0.1384 0.7841 0.1486
-4.750 0.0305 0.01066 0.00485 -0.1375 0.7836 0.1807
-4.500 0.0489 0.01021 0.00458 -0.1367 0.7832 0.2291
-4.250 0.0675 0.00966 0.00427 -0.1361 0.7828 0.2971
-4.000 0.0880 0.00907 0.00395 -0.1358 0.7824 0.3723
-3.500 0.1349 0.00798 0.00344 -0.1361 0.7815 0.5464
-3.250 0.1632 0.00791 0.00342 -0.1367 0.7811 0.5668
-3.000 0.1919 0.00790 0.00342 -0.1373 0.7808 0.5777
-2.750 0.2204 0.00790 0.00344 -0.1379 0.7804 0.5870
-2.500 0.2490 0.00792 0.00349 -0.1385 0.7800 0.5976
-2.000 0.3053 0.00803 0.00366 -0.1395 0.7793 0.6157
-1.500 0.3603 0.00816 0.00383 -0.1401 0.7787 0.6286
-1.250 0.3875 0.00824 0.00391 -0.1404 0.7783 0.6340
-1.000 0.4144 0.00829 0.00396 -0.1406 0.7777 0.6366
-0.750 0.4410 0.00836 0.00405 -0.1408 0.7771 0.6386
-0.500 0.4676 0.00843 0.00414 -0.1409 0.7765 0.6406
-0.250 0.4941 0.00851 0.00423 -0.1410 0.7759 0.6429
0.000 0.5205 0.00857 0.00430 -0.1411 0.7751 0.6452
0.250 0.5472 0.00859 0.00432 -0.1413 0.7740 0.6476
0.500 0.5745 0.00858 0.00431 -0.1416 0.7728 0.6498
0.750 0.6024 0.00856 0.00430 -0.1419 0.7718 0.6514
1.000 0.6308 0.00856 0.00432 -0.1424 0.7708 0.6528
1.250 0.6594 0.00856 0.00433 -0.1430 0.7700 0.6543
1.500 0.6883 0.00857 0.00436 -0.1435 0.7693 0.6559
1.750 0.7175 0.00858 0.00438 -0.1442 0.7687 0.6575
2.000 0.7489 0.00851 0.00432 -0.1453 0.7677 0.6592
2.250 0.7844 0.00831 0.00409 -0.1472 0.7659 0.6608
2.500 0.7959 0.00826 0.00410 -0.1440 0.7617 0.6626
2.750 0.8166 0.00814 0.00399 -0.1428 0.7578 0.6641
3.000 0.8425 0.00789 0.00373 -0.1425 0.7537 0.6654
3.250 0.8575 0.00783 0.00371 -0.1401 0.7503 0.6667
3.500 0.8591 0.00796 0.00390 -0.1348 0.7446 0.6681
3.750 0.8779 0.00791 0.00386 -0.1332 0.7392 0.6692
4.000 0.8782 0.00822 0.00421 -0.1279 0.7304 0.6705
4.250 0.8857 0.00843 0.00441 -0.1241 0.7186 0.6718
4.500 0.8900 0.00872 0.00463 -0.1198 0.6967 0.6731
4.750 0.8630 0.00987 0.00552 -0.1097 0.6516 0.6746
5.000 0.8411 0.01122 0.00670 -0.1010 0.6191 0.6760
5.250 0.8257 0.01253 0.00785 -0.0938 0.5879 0.6771
5.500 0.8164 0.01373 0.00892 -0.0879 0.5584 0.6781
5.750 0.8087 0.01496 0.00999 -0.0823 0.5259 0.6790
6.000 0.8095 0.01595 0.01084 -0.0783 0.4962 0.6797
6.250 0.8122 0.01690 0.01167 -0.0747 0.4685 0.6805
6.500 0.8110 0.01802 0.01259 -0.0705 0.4287 0.6815
6.750 0.8191 0.01881 0.01327 -0.0679 0.3988 0.6823
7.000 0.8297 0.01955 0.01391 -0.0657 0.3751 0.6831
7.250 0.8366 0.02045 0.01465 -0.0631 0.3397 0.6838
7.500 0.8412 0.02149 0.01545 -0.0601 0.2927 0.6845
7.750 0.8451 0.02259 0.01627 -0.0571 0.2394 0.6851
8.000 0.8530 0.02355 0.01702 -0.0548 0.1978 0.6858
8.250 0.8627 0.02447 0.01778 -0.0528 0.1650 0.6865
8.500 0.8758 0.02525 0.01844 -0.0512 0.1423 0.6872
8.750 0.8891 0.02603 0.01911 -0.0498 0.1163 0.6878
9.250 0.9167 0.02760 0.02048 -0.0471 0.0775 0.6894
9.500 0.9343 0.02820 0.02107 -0.0463 0.0713 0.6901
9.750 0.9513 0.02884 0.02170 -0.0455 0.0670 0.6909
10.000 0.9674 0.02955 0.02239 -0.0445 0.0609 0.6917
10.250 0.9858 0.03013 0.02300 -0.0439 0.0583 0.6923
10.500 1.0026 0.03081 0.02366 -0.0431 0.0532 0.6929
10.750 1.0192 0.03150 0.02434 -0.0423 0.0473 0.6933
11.000 1.0319 0.03244 0.02518 -0.0411 0.0336 0.6937
11.250 1.0439 0.03346 0.02614 -0.0398 0.0238 0.6941
11.500 1.0585 0.03433 0.02700 -0.0388 0.0201 0.6944
11.750 1.0733 0.03519 0.02788 -0.0379 0.0177 0.6947
12.000 1.0892 0.03601 0.02871 -0.0371 0.0161 0.6951
12.250 1.1040 0.03690 0.02962 -0.0363 0.0149 0.6954
12.500 1.1177 0.03787 0.03061 -0.0354 0.0137 0.6961
12.750 1.1324 0.03877 0.03155 -0.0345 0.0130 0.6969
13.000 1.1473 0.03967 0.03249 -0.0338 0.0124 0.6976
13.250 1.1617 0.04063 0.03349 -0.0331 0.0117 0.6982
13.500 1.1746 0.04173 0.03462 -0.0322 0.0111 0.6988
13.750 1.1872 0.04285 0.03578 -0.0313 0.0106 0.6993
14.000 1.2011 0.04389 0.03686 -0.0306 0.0101 0.6998
14.250 1.2138 0.04504 0.03806 -0.0299 0.0098 0.7003
14.500 1.2265 0.04622 0.03928 -0.0291 0.0093 0.7008
14.750 1.2385 0.04745 0.04055 -0.0284 0.0090 0.7013
15.000 1.2503 0.04873 0.04188 -0.0277 0.0087 0.7018
15.250 1.2608 0.05013 0.04332 -0.0270 0.0083 0.7023
15.500 1.2705 0.05164 0.04488 -0.0262 0.0080 0.7030
15.750 1.2815 0.05306 0.04636 -0.0256 0.0077 0.7035
16.000 1.2918 0.05456 0.04792 -0.0250 0.0075 0.7040
16.250 1.3024 0.05604 0.04945 -0.0245 0.0073 0.7045
16.500 1.3106 0.05779 0.05127 -0.0239 0.0072 0.7048
16.750 1.3198 0.05946 0.05299 -0.0234 0.0069 0.7051
17.000 1.3281 0.06124 0.05483 -0.0229 0.0067 0.7054
17.250 1.3352 0.06318 0.05682 -0.0225 0.0065 0.7058
17.500 1.3421 0.06517 0.05887 -0.0221 0.0063 0.7061
17.750 1.3477 0.06735 0.06112 -0.0217 0.0062 0.7064
18.000 1.3524 0.06966 0.06350 -0.0215 0.0060 0.7068
18.250 1.3585 0.07183 0.06574 -0.0213 0.0059 0.7071
18.500 1.3638 0.07413 0.06812 -0.0212 0.0058 0.7074
18.750 1.3673 0.07668 0.07076 -0.0212 0.0057 0.7077
19.000 1.3713 0.07923 0.07338 -0.0213 0.0056 0.7080
19.250 1.3756 0.08176 0.07598 -0.0215 0.0054 0.7083
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