WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il) Reynolds number: 1,000,000 Max Cl/Cd: 58.15 at α=3.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx3-il-1000000-n5.txt Download as CSV file: xf-fx3-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 3 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 -0.8174 0.08386 0.07972 -0.1217 0.7922 0.0058
-19.500 -0.8366 0.07733 0.07306 -0.1251 0.7922 0.0059
-19.250 -0.8498 0.07193 0.06753 -0.1279 0.7921 0.0059
-19.000 -0.8591 0.06731 0.06279 -0.1302 0.7921 0.0059
-18.750 -0.8652 0.06330 0.05868 -0.1320 0.7921 0.0060
-18.500 -0.8688 0.05976 0.05503 -0.1335 0.7920 0.0060
-18.250 -0.8697 0.05663 0.05181 -0.1347 0.7920 0.0061
-18.000 -0.8690 0.05381 0.04889 -0.1357 0.7920 0.0062
-17.750 -0.8667 0.05125 0.04624 -0.1366 0.7919 0.0062
-17.500 -0.8626 0.04895 0.04386 -0.1373 0.7919 0.0063
-17.250 -0.8570 0.04687 0.04170 -0.1378 0.7918 0.0064
-17.000 -0.8504 0.04495 0.03969 -0.1383 0.7918 0.0064
-16.750 -0.8466 0.04284 0.03750 -0.1385 0.7917 0.0066
-16.500 -0.8402 0.04104 0.03563 -0.1387 0.7917 0.0067
-16.250 -0.8316 0.03946 0.03400 -0.1388 0.7916 0.0069
-16.000 -0.8218 0.03804 0.03252 -0.1389 0.7916 0.0070
-15.750 -0.8107 0.03677 0.03119 -0.1389 0.7915 0.0072
-15.500 -0.7985 0.03559 0.02997 -0.1389 0.7915 0.0074
-15.250 -0.7858 0.03447 0.02880 -0.1390 0.7915 0.0076
-15.000 -0.7720 0.03346 0.02774 -0.1390 0.7915 0.0078
-14.750 -0.7577 0.03250 0.02672 -0.1389 0.7915 0.0080
-14.500 -0.7432 0.03157 0.02574 -0.1389 0.7914 0.0082
-14.250 -0.7281 0.03070 0.02482 -0.1388 0.7914 0.0084
-14.000 -0.7119 0.02991 0.02398 -0.1388 0.7914 0.0085
-13.750 -0.6971 0.02903 0.02306 -0.1386 0.7913 0.0088
-13.500 -0.6814 0.02822 0.02222 -0.1384 0.7913 0.0092
-13.250 -0.6650 0.02748 0.02145 -0.1383 0.7912 0.0095
-13.000 -0.6479 0.02680 0.02074 -0.1382 0.7912 0.0098
-12.750 -0.6299 0.02619 0.02010 -0.1381 0.7912 0.0102
-12.500 -0.6116 0.02561 0.01949 -0.1380 0.7911 0.0106
-12.250 -0.5929 0.02506 0.01891 -0.1380 0.7911 0.0110
-12.000 -0.5743 0.02451 0.01833 -0.1379 0.7911 0.0114
-11.750 -0.5564 0.02393 0.01775 -0.1377 0.7911 0.0121
-11.500 -0.5379 0.02340 0.01721 -0.1375 0.7910 0.0129
-11.250 -0.5188 0.02292 0.01671 -0.1374 0.7910 0.0136
-11.000 -0.4990 0.02249 0.01626 -0.1373 0.7910 0.0142
-10.750 -0.4796 0.02205 0.01580 -0.1372 0.7909 0.0151
-10.500 -0.4604 0.02159 0.01535 -0.1370 0.7909 0.0164
-10.250 -0.4407 0.02118 0.01494 -0.1368 0.7909 0.0176
-10.000 -0.4206 0.02080 0.01454 -0.1367 0.7908 0.0191
-9.750 -0.4013 0.02038 0.01415 -0.1365 0.7908 0.0217
-9.500 -0.3812 0.02001 0.01379 -0.1363 0.7908 0.0245
-9.250 -0.3612 0.01964 0.01346 -0.1362 0.7907 0.0283
-9.000 -0.3401 0.01933 0.01315 -0.1361 0.7907 0.0309
-8.750 -0.3193 0.01902 0.01288 -0.1360 0.7907 0.0343
-8.500 -0.2976 0.01876 0.01262 -0.1360 0.7906 0.0370
-8.250 -0.2755 0.01852 0.01237 -0.1360 0.7906 0.0384
-8.000 -0.2546 0.01823 0.01209 -0.1358 0.7905 0.0408
-7.750 -0.2335 0.01796 0.01185 -0.1356 0.7905 0.0431
-7.500 -0.2119 0.01773 0.01162 -0.1355 0.7905 0.0451
-7.250 -0.1904 0.01751 0.01140 -0.1354 0.7904 0.0465
-7.000 -0.1701 0.01732 0.01121 -0.1350 0.7904 0.0480
-6.750 -0.1523 0.01711 0.01103 -0.1342 0.7903 0.0507
-6.500 -0.1355 0.01696 0.01090 -0.1331 0.7902 0.0531
-6.250 -0.1202 0.01685 0.01081 -0.1317 0.7901 0.0555
-6.000 -0.1028 0.01675 0.01071 -0.1307 0.7900 0.0573
-5.750 -0.0845 0.01660 0.01058 -0.1300 0.7899 0.0601
-5.500 -0.0659 0.01644 0.01045 -0.1293 0.7897 0.0635
-5.250 -0.0462 0.01631 0.01034 -0.1289 0.7896 0.0668
-5.000 -0.0253 0.01619 0.01024 -0.1287 0.7893 0.0697
-4.750 -0.0043 0.01604 0.01011 -0.1285 0.7889 0.0757
-4.500 0.0170 0.01591 0.01002 -0.1285 0.7886 0.0830
-4.250 0.0384 0.01573 0.00992 -0.1287 0.7883 0.0985
-4.000 0.0615 0.01528 0.00966 -0.1299 0.7879 0.1464
-3.750 0.0965 0.01416 0.00900 -0.1351 0.7875 0.2669
-3.500 0.1729 0.01211 0.00832 -0.1504 0.7879 0.6137
-3.000 0.2266 0.01291 0.00903 -0.1511 0.7872 0.6538
-2.750 0.2465 0.01353 0.00970 -0.1498 0.7865 0.6558
-2.500 0.2665 0.01409 0.01028 -0.1487 0.7858 0.6575
-2.250 0.2849 0.01474 0.01095 -0.1472 0.7851 0.6600
-2.000 0.3060 0.01526 0.01146 -0.1465 0.7844 0.6629
-1.750 0.3343 0.01551 0.01165 -0.1473 0.7838 0.6659
-1.500 0.3513 0.01607 0.01226 -0.1455 0.7831 0.6674
-1.250 0.3689 0.01661 0.01285 -0.1437 0.7825 0.6687
-1.000 0.3924 0.01690 0.01314 -0.1434 0.7821 0.6692
-0.750 0.3391 0.02021 0.01651 -0.1308 0.7736 0.6702
-0.500 0.3663 0.02029 0.01658 -0.1312 0.7724 0.6707
-0.250 0.3963 0.02025 0.01654 -0.1321 0.7717 0.6712
0.000 0.4265 0.02022 0.01650 -0.1331 0.7711 0.6715
0.250 0.4563 0.02023 0.01650 -0.1340 0.7706 0.6720
0.500 0.4864 0.02022 0.01649 -0.1349 0.7702 0.6726
0.750 0.5177 0.02015 0.01642 -0.1361 0.7698 0.6731
1.000 0.5499 0.02002 0.01629 -0.1374 0.7695 0.6733
1.250 0.5822 0.01988 0.01615 -0.1387 0.7692 0.6736
1.500 0.6149 0.01972 0.01599 -0.1401 0.7689 0.6740
1.750 0.6499 0.01941 0.01568 -0.1419 0.7686 0.6741
2.000 0.6873 0.01893 0.01522 -0.1440 0.7684 0.6743
2.250 0.7249 0.01843 0.01473 -0.1461 0.7683 0.6744
2.500 0.7614 0.01801 0.01431 -0.1480 0.7681 0.6746
2.750 0.7971 0.01763 0.01395 -0.1499 0.7679 0.6747
3.000 0.8328 0.01724 0.01358 -0.1517 0.7678 0.6748
3.250 0.8727 0.01654 0.01291 -0.1541 0.7678 0.6749
3.500 0.9118 0.01568 0.01207 -0.1564 0.7660 0.6751
4.750 0.9699 0.01708 0.01264 -0.1453 0.5866 0.6760
5.000 0.9611 0.01866 0.01402 -0.1398 0.5492 0.6761
5.250 0.9615 0.01993 0.01513 -0.1359 0.5164 0.6762
5.500 0.9670 0.02100 0.01603 -0.1329 0.4820 0.6763
5.750 0.9719 0.02209 0.01690 -0.1298 0.4380 0.6764
6.000 0.9758 0.02323 0.01775 -0.1266 0.3849 0.6766
6.250 0.9816 0.02428 0.01849 -0.1237 0.3278 0.6768
6.500 0.9911 0.02519 0.01914 -0.1214 0.2785 0.6769
6.750 1.0020 0.02607 0.01978 -0.1193 0.2328 0.6769
7.000 1.0138 0.02693 0.02042 -0.1174 0.1909 0.6770
7.250 1.0257 0.02780 0.02108 -0.1156 0.1507 0.6770
7.500 1.0394 0.02862 0.02172 -0.1141 0.1192 0.6771
7.750 1.0562 0.02930 0.02230 -0.1130 0.1000 0.6771
8.000 1.0738 0.02995 0.02288 -0.1121 0.0850 0.6771
8.250 1.0918 0.03058 0.02345 -0.1113 0.0735 0.6772
8.500 1.1106 0.03116 0.02400 -0.1106 0.0655 0.6772
8.750 1.1288 0.03179 0.02459 -0.1098 0.0565 0.6772
9.000 1.1461 0.03247 0.02521 -0.1089 0.0470 0.6773
9.250 1.1612 0.03329 0.02594 -0.1077 0.0328 0.6773
9.500 1.1763 0.03412 0.02671 -0.1064 0.0226 0.6773
9.750 1.1932 0.03487 0.02745 -0.1055 0.0190 0.6774
10.000 1.2095 0.03565 0.02824 -0.1046 0.0168 0.6774
10.250 1.2266 0.03639 0.02900 -0.1037 0.0154 0.6774
10.500 1.2438 0.03712 0.02977 -0.1029 0.0144 0.6775
10.750 1.2604 0.03791 0.03056 -0.1020 0.0133 0.6775
11.000 1.2762 0.03874 0.03141 -0.1010 0.0123 0.6775
11.250 1.2932 0.03952 0.03222 -0.1002 0.0117 0.6776
11.500 1.3096 0.04033 0.03306 -0.0993 0.0111 0.6776
11.750 1.3246 0.04126 0.03401 -0.0983 0.0105 0.6776
12.000 1.3389 0.04224 0.03501 -0.0973 0.0099 0.6777
12.250 1.3525 0.04326 0.03608 -0.0961 0.0093 0.6777
12.500 1.3677 0.04419 0.03705 -0.0952 0.0090 0.6777
12.750 1.3824 0.04516 0.03806 -0.0943 0.0087 0.6778
13.000 1.3961 0.04622 0.03916 -0.0932 0.0084 0.6778
13.250 1.4089 0.04737 0.04035 -0.0921 0.0081 0.6778
13.500 1.4216 0.04854 0.04155 -0.0911 0.0078 0.6779
13.750 1.4338 0.04975 0.04281 -0.0900 0.0075 0.6779
14.000 1.4441 0.05112 0.04423 -0.0887 0.0071 0.6779
14.250 1.4555 0.05243 0.04558 -0.0876 0.0069 0.6780
14.500 1.4669 0.05374 0.04695 -0.0866 0.0067 0.6780
14.750 1.4778 0.05511 0.04838 -0.0855 0.0066 0.6781
15.000 1.4875 0.05661 0.04994 -0.0844 0.0064 0.6781
15.250 1.4974 0.05813 0.05151 -0.0834 0.0062 0.6781
15.500 1.5064 0.05973 0.05317 -0.0823 0.0060 0.6782
15.750 1.5146 0.06144 0.05495 -0.0813 0.0059 0.6782
16.000 1.5227 0.06317 0.05673 -0.0803 0.0057 0.6783
16.250 1.5290 0.06510 0.05872 -0.0792 0.0056 0.6783
16.500 1.5348 0.06708 0.06077 -0.0782 0.0054 0.6783
16.750 1.5382 0.06937 0.06314 -0.0771 0.0053 0.6784
17.000 1.5427 0.07158 0.06542 -0.0762 0.0052 0.6784
17.250 1.5470 0.07386 0.06779 -0.0753 0.0051 0.6784
17.500 1.5513 0.07616 0.07017 -0.0746 0.0051 0.6785
17.750 1.5550 0.07857 0.07267 -0.0740 0.0050 0.6785
18.000 1.5573 0.08117 0.07535 -0.0734 0.0049 0.6785
18.250 1.5592 0.08383 0.07810 -0.0728 0.0048 0.6786
18.500 1.5604 0.08661 0.08097 -0.0724 0.0047 0.6786
18.750 1.5606 0.08957 0.08402 -0.0721 0.0047 0.6787
19.000 1.5603 0.09261 0.08715 -0.0719 0.0046 0.6787
19.250 1.5601 0.09569 0.09032 -0.0719 0.0045 0.6787
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