WORTMANN FX 60-126 AIRFOIL (fx60126-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 60-126 AIRFOIL (fx60126-il) Reynolds number: 200,000 Max Cl/Cd: 75.22 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx60126-il-200000-n5.txt Download as CSV file: xf-fx60126-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 60-126 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.750 -0.5348 0.07369 0.06966 -0.0576 1.0000 0.0122
-11.500 -0.5795 0.06183 0.05755 -0.0660 1.0000 0.0118
-11.250 -0.6037 0.05515 0.05069 -0.0705 1.0000 0.0117
-11.000 -0.6227 0.05014 0.04556 -0.0733 1.0000 0.0117
-10.750 -0.6399 0.04628 0.04159 -0.0746 1.0000 0.0116
-10.500 -0.6616 0.04349 0.03873 -0.0736 1.0000 0.0116
-10.250 -0.6853 0.04118 0.03636 -0.0718 1.0000 0.0116
-10.000 -0.6707 0.03713 0.03201 -0.0787 0.9944 0.0117
-9.750 -0.6474 0.03393 0.02853 -0.0838 0.9877 0.0119
-9.500 -0.6196 0.03133 0.02566 -0.0880 0.9831 0.0121
-9.250 -0.5943 0.02923 0.02334 -0.0905 0.9772 0.0124
-9.000 -0.5652 0.02729 0.02117 -0.0931 0.9728 0.0127
-8.750 -0.5331 0.02556 0.01925 -0.0959 0.9698 0.0131
-8.500 -0.5060 0.02410 0.01761 -0.0973 0.9639 0.0135
-8.250 -0.4741 0.02274 0.01609 -0.0995 0.9595 0.0139
-8.000 -0.4404 0.02143 0.01466 -0.1020 0.9562 0.0147
-7.750 -0.4113 0.02043 0.01359 -0.1034 0.9505 0.0156
-7.500 -0.3801 0.01949 0.01254 -0.1049 0.9451 0.0167
-7.250 -0.3458 0.01854 0.01143 -0.1069 0.9410 0.0179
-7.000 -0.3168 0.01760 0.01043 -0.1079 0.9342 0.0191
-6.750 -0.2854 0.01682 0.00956 -0.1092 0.9286 0.0210
-6.500 -0.2523 0.01604 0.00871 -0.1107 0.9246 0.0244
-6.250 -0.2245 0.01541 0.00804 -0.1111 0.9172 0.0319
-6.000 -0.1933 0.01472 0.00736 -0.1121 0.9114 0.0462
-5.750 -0.1637 0.01418 0.00685 -0.1127 0.9046 0.0662
-5.500 -0.1345 0.01361 0.00638 -0.1134 0.8974 0.0908
-5.250 -0.1043 0.01295 0.00591 -0.1143 0.8916 0.1375
-5.000 -0.0760 0.01244 0.00555 -0.1148 0.8841 0.1804
-4.750 -0.0457 0.01206 0.00520 -0.1153 0.8785 0.2139
-4.500 -0.0174 0.01179 0.00498 -0.1155 0.8711 0.2474
-4.250 0.0119 0.01156 0.00476 -0.1157 0.8642 0.2755
-4.000 0.0405 0.01140 0.00458 -0.1157 0.8560 0.3033
-3.750 0.0694 0.01125 0.00444 -0.1158 0.8480 0.3290
-3.500 0.0977 0.01116 0.00435 -0.1157 0.8392 0.3539
-3.250 0.1267 0.01108 0.00423 -0.1157 0.8316 0.3754
-3.000 0.1549 0.01104 0.00416 -0.1155 0.8226 0.3909
-2.750 0.1838 0.01099 0.00404 -0.1155 0.8151 0.4035
-2.500 0.2120 0.01096 0.00397 -0.1153 0.8056 0.4160
-2.250 0.2404 0.01093 0.00390 -0.1152 0.7962 0.4308
-2.000 0.2687 0.01092 0.00382 -0.1150 0.7855 0.4446
-1.750 0.2966 0.01089 0.00378 -0.1148 0.7741 0.4556
-1.500 0.3248 0.01088 0.00372 -0.1146 0.7633 0.4650
-1.250 0.3532 0.01088 0.00365 -0.1145 0.7527 0.4751
-1.000 0.3811 0.01087 0.00364 -0.1143 0.7415 0.4842
-0.750 0.4093 0.01089 0.00360 -0.1141 0.7298 0.4936
-0.500 0.4372 0.01090 0.00358 -0.1139 0.7173 0.5021
-0.250 0.4650 0.01093 0.00355 -0.1136 0.7035 0.5103
0.000 0.4928 0.01096 0.00354 -0.1134 0.6896 0.5184
0.250 0.5205 0.01101 0.00354 -0.1132 0.6757 0.5264
0.500 0.5481 0.01107 0.00357 -0.1129 0.6621 0.5351
0.750 0.5757 0.01114 0.00362 -0.1127 0.6485 0.5438
1.000 0.6032 0.01123 0.00366 -0.1125 0.6346 0.5533
1.250 0.6305 0.01132 0.00374 -0.1122 0.6212 0.5619
1.500 0.6578 0.01144 0.00380 -0.1120 0.6067 0.5711
1.750 0.6845 0.01155 0.00389 -0.1116 0.5898 0.5789
2.000 0.7111 0.01170 0.00396 -0.1112 0.5710 0.5876
2.250 0.7373 0.01185 0.00407 -0.1108 0.5529 0.5961
2.500 0.7637 0.01202 0.00420 -0.1104 0.5360 0.6057
2.750 0.7902 0.01217 0.00434 -0.1100 0.5213 0.6162
3.000 0.8167 0.01231 0.00451 -0.1097 0.5081 0.6268
3.250 0.8431 0.01246 0.00469 -0.1094 0.4955 0.6384
3.500 0.8694 0.01264 0.00487 -0.1090 0.4825 0.6506
3.750 0.8952 0.01282 0.00506 -0.1086 0.4683 0.6625
4.000 0.9207 0.01301 0.00527 -0.1081 0.4513 0.6755
4.250 0.9458 0.01321 0.00550 -0.1075 0.4326 0.6900
4.500 0.9703 0.01344 0.00573 -0.1069 0.4139 0.7059
4.750 0.9945 0.01369 0.00598 -0.1062 0.3957 0.7238
5.000 1.0187 0.01392 0.00625 -0.1055 0.3787 0.7451
5.250 1.0420 0.01415 0.00653 -0.1046 0.3620 0.7726
5.500 1.0635 0.01435 0.00680 -0.1034 0.3464 0.8137
5.750 1.0816 0.01438 0.00700 -0.1012 0.3298 1.0000
6.000 1.1057 0.01481 0.00735 -0.1007 0.3082 1.0000
6.250 1.1285 0.01531 0.00775 -0.1001 0.2873 1.0000
6.500 1.1515 0.01580 0.00818 -0.0994 0.2669 1.0000
6.750 1.1739 0.01632 0.00863 -0.0987 0.2454 1.0000
7.000 1.1951 0.01692 0.00914 -0.0978 0.2268 1.0000
7.250 1.2166 0.01749 0.00967 -0.0970 0.2081 1.0000
7.500 1.2373 0.01810 0.01023 -0.0961 0.1900 1.0000
7.750 1.2568 0.01879 0.01085 -0.0950 0.1741 1.0000
8.000 1.2758 0.01948 0.01149 -0.0938 0.1575 1.0000
8.250 1.2936 0.02024 0.01218 -0.0925 0.1420 1.0000
8.500 1.3109 0.02099 0.01290 -0.0912 0.1308 1.0000
8.750 1.3275 0.02174 0.01365 -0.0897 0.1220 1.0000
9.000 1.3437 0.02244 0.01438 -0.0882 0.1128 1.0000
9.250 1.3583 0.02317 0.01514 -0.0864 0.1050 1.0000
9.500 1.3706 0.02404 0.01599 -0.0844 0.0979 1.0000
9.750 1.3835 0.02489 0.01690 -0.0825 0.0921 1.0000
10.000 1.3933 0.02594 0.01795 -0.0804 0.0870 1.0000
10.250 1.4058 0.02686 0.01896 -0.0787 0.0827 1.0000
10.500 1.4176 0.02785 0.02005 -0.0770 0.0779 1.0000
10.750 1.4262 0.02909 0.02132 -0.0752 0.0739 1.0000
11.000 1.4373 0.03021 0.02254 -0.0736 0.0704 1.0000
11.250 1.4466 0.03149 0.02391 -0.0721 0.0669 1.0000
11.500 1.4536 0.03299 0.02545 -0.0705 0.0640 1.0000
11.750 1.4604 0.03458 0.02711 -0.0691 0.0616 1.0000
12.000 1.4675 0.03621 0.02885 -0.0678 0.0593 1.0000
12.250 1.4728 0.03805 0.03078 -0.0666 0.0571 1.0000
12.500 1.4763 0.04013 0.03292 -0.0655 0.0552 1.0000
12.750 1.4771 0.04256 0.03541 -0.0644 0.0535 1.0000
13.000 1.4789 0.04500 0.03794 -0.0636 0.0521 1.0000
13.250 1.4843 0.04716 0.04028 -0.0629 0.0509 1.0000
13.500 1.4882 0.04952 0.04279 -0.0624 0.0494 1.0000
13.750 1.4913 0.05205 0.04546 -0.0621 0.0478 1.0000
14.000 1.4933 0.05478 0.04831 -0.0620 0.0463 1.0000
14.250 1.4935 0.05781 0.05144 -0.0621 0.0447 1.0000
14.500 1.4910 0.06127 0.05497 -0.0624 0.0434 1.0000
14.750 1.4919 0.06444 0.05827 -0.0628 0.0420 1.0000
15.000 1.4945 0.06751 0.06152 -0.0634 0.0403 1.0000
15.250 1.4952 0.07091 0.06507 -0.0642 0.0387 1.0000
15.500 1.4943 0.07464 0.06893 -0.0653 0.0372 1.0000
15.750 1.4910 0.07883 0.07322 -0.0666 0.0360 1.0000
16.000 1.4854 0.08348 0.07796 -0.0683 0.0350 1.0000
16.250 1.4834 0.08766 0.08231 -0.0697 0.0340 1.0000
16.500 1.4806 0.09206 0.08688 -0.0713 0.0328 1.0000
16.750 1.4765 0.09681 0.09179 -0.0733 0.0317 1.0000
17.000 1.4709 0.10192 0.09704 -0.0756 0.0307 1.0000
17.250 1.4637 0.10743 0.10266 -0.0782 0.0297 1.0000
17.500 1.4552 0.11325 0.10859 -0.0811 0.0289 1.0000
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