WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il) Reynolds number: 500,000 Max Cl/Cd: 44.62 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx3-il-500000-n5.txt Download as CSV file: xf-fx3-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.5765 0.11820 0.11417 -0.1095 0.8049 0.0087
-19.000 -0.6167 0.10610 0.10187 -0.1155 0.8049 0.0086
-18.750 -0.6448 0.09680 0.09239 -0.1204 0.8050 0.0086
-18.500 -0.6668 0.08892 0.08436 -0.1248 0.8050 0.0086
-18.250 -0.6851 0.08208 0.07738 -0.1286 0.8050 0.0086
-18.000 -0.6999 0.07614 0.07130 -0.1317 0.8050 0.0087
-17.750 -0.7119 0.07090 0.06594 -0.1344 0.8051 0.0087
-17.500 -0.7205 0.06639 0.06131 -0.1366 0.8051 0.0088
-17.250 -0.7261 0.06249 0.05730 -0.1384 0.8051 0.0089
-17.000 -0.7291 0.05905 0.05376 -0.1398 0.8051 0.0091
-16.750 -0.7295 0.05606 0.05067 -0.1409 0.8050 0.0092
-16.500 -0.7283 0.05339 0.04790 -0.1418 0.8050 0.0093
-16.250 -0.7254 0.05097 0.04538 -0.1425 0.8049 0.0095
-16.000 -0.7212 0.04875 0.04307 -0.1430 0.8048 0.0096
-15.750 -0.7158 0.04675 0.04098 -0.1434 0.8048 0.0098
-15.500 -0.7093 0.04493 0.03906 -0.1436 0.8048 0.0100
-15.250 -0.7018 0.04324 0.03727 -0.1438 0.8048 0.0103
-15.000 -0.6932 0.04170 0.03564 -0.1439 0.8048 0.0105
-14.750 -0.6837 0.04027 0.03413 -0.1439 0.8047 0.0107
-14.500 -0.6728 0.03900 0.03277 -0.1438 0.8047 0.0110
-14.250 -0.6612 0.03782 0.03150 -0.1438 0.8047 0.0112
-14.000 -0.6521 0.03646 0.03009 -0.1435 0.8047 0.0116
-13.750 -0.6401 0.03536 0.02895 -0.1434 0.8047 0.0120
-13.500 -0.6266 0.03440 0.02793 -0.1432 0.8047 0.0124
-13.250 -0.6119 0.03354 0.02701 -0.1431 0.8046 0.0129
-13.000 -0.5967 0.03273 0.02615 -0.1429 0.8046 0.0135
-12.750 -0.5812 0.03197 0.02532 -0.1427 0.8046 0.0140
-12.500 -0.5652 0.03126 0.02454 -0.1425 0.8046 0.0144
-12.250 -0.5511 0.03043 0.02369 -0.1422 0.8046 0.0151
-12.000 -0.5352 0.02975 0.02299 -0.1419 0.8045 0.0159
-11.750 -0.5184 0.02915 0.02235 -0.1416 0.8045 0.0167
-11.500 -0.5011 0.02860 0.02176 -0.1414 0.8045 0.0177
-11.250 -0.4835 0.02809 0.02120 -0.1411 0.8045 0.0186
-11.000 -0.4670 0.02754 0.02066 -0.1407 0.8045 0.0202
-10.750 -0.4495 0.02707 0.02019 -0.1404 0.8044 0.0220
-10.500 -0.4316 0.02664 0.01973 -0.1400 0.8044 0.0237
-10.250 -0.4138 0.02623 0.01934 -0.1397 0.8044 0.0261
-10.000 -0.3950 0.02589 0.01899 -0.1394 0.8044 0.0290
-9.750 -0.3763 0.02557 0.01867 -0.1391 0.8043 0.0317
-9.500 -0.3572 0.02529 0.01841 -0.1388 0.8043 0.0349
-9.250 -0.3377 0.02505 0.01815 -0.1385 0.8042 0.0376
-9.000 -0.3194 0.02479 0.01788 -0.1380 0.8042 0.0398
-8.750 -0.3012 0.02455 0.01766 -0.1375 0.8041 0.0425
-8.500 -0.2827 0.02437 0.01747 -0.1370 0.8041 0.0449
-8.250 -0.2645 0.02421 0.01729 -0.1364 0.8038 0.0467
-8.000 -0.2489 0.02401 0.01710 -0.1354 0.8035 0.0488
-7.750 -0.2340 0.02388 0.01700 -0.1343 0.8033 0.0512
-7.500 -0.2199 0.02383 0.01697 -0.1329 0.8030 0.0534
-7.250 -0.2082 0.02389 0.01703 -0.1311 0.8026 0.0553
-7.000 -0.2021 0.02410 0.01724 -0.1282 0.8020 0.0567
-6.750 -0.2135 0.02475 0.01792 -0.1222 0.8007 0.0573
-6.500 -0.3446 0.02694 0.02019 -0.0944 0.7952 0.0537
-6.250 -0.3530 0.02695 0.02017 -0.0889 0.7942 0.0548
-6.000 -0.3428 0.02682 0.02001 -0.0869 0.7936 0.0564
-5.750 -0.3233 0.02655 0.01972 -0.0865 0.7932 0.0587
-5.500 -0.3010 0.02618 0.01937 -0.0867 0.7928 0.0628
-5.250 -0.2784 0.02596 0.01914 -0.0870 0.7926 0.0661
-5.000 -0.2880 0.02659 0.01976 -0.0822 0.7900 0.0673
-4.750 -0.2500 0.02621 0.01934 -0.0849 0.7906 0.0702
-4.500 -0.2141 0.02581 0.01896 -0.0875 0.7909 0.0768
-4.250 -0.1786 0.02549 0.01864 -0.0899 0.7912 0.0842
-4.000 -0.1426 0.02512 0.01834 -0.0927 0.7915 0.1007
-3.500 -0.0578 0.02336 0.01867 -0.1123 0.7846 0.5631
-3.250 -0.0737 0.02537 0.02106 -0.1004 0.7825 0.5978
-2.750 -0.0037 0.02582 0.02129 -0.1054 0.7817 0.6559
-2.500 0.0200 0.02624 0.02170 -0.1045 0.7812 0.6589
-2.250 0.0574 0.02635 0.02169 -0.1073 0.7808 0.6661
-2.000 0.0807 0.02667 0.02203 -0.1059 0.7803 0.6677
-1.750 0.1043 0.02700 0.02237 -0.1046 0.7799 0.6698
-1.500 0.0991 0.02795 0.02334 -0.0996 0.7727 0.6717
-1.250 0.1248 0.02820 0.02356 -0.0996 0.7714 0.6747
-1.000 0.1572 0.02836 0.02366 -0.1012 0.7706 0.6798
-0.750 0.1783 0.02862 0.02395 -0.0995 0.7697 0.6812
-0.500 0.2080 0.02861 0.02392 -0.1003 0.7692 0.6818
-0.250 0.2389 0.02858 0.02386 -0.1014 0.7687 0.6822
0.000 0.2698 0.02853 0.02381 -0.1025 0.7682 0.6828
0.250 0.3012 0.02849 0.02375 -0.1036 0.7679 0.6834
0.500 0.3336 0.02841 0.02366 -0.1050 0.7675 0.6839
0.750 0.3663 0.02833 0.02356 -0.1065 0.7672 0.6845
1.250 0.3962 0.02900 0.02424 -0.1040 0.7576 0.6862
1.500 0.4285 0.02889 0.02414 -0.1054 0.7570 0.6872
1.750 0.4617 0.02876 0.02400 -0.1070 0.7565 0.6881
2.000 0.4957 0.02858 0.02382 -0.1087 0.7560 0.6889
2.250 0.5297 0.02838 0.02362 -0.1105 0.7554 0.6894
2.750 0.5694 0.02867 0.02393 -0.1097 0.7452 0.6901
3.000 0.6035 0.02840 0.02367 -0.1114 0.7445 0.6903
3.500 0.6450 0.02874 0.02406 -0.1108 0.7338 0.6908
3.750 0.6781 0.02849 0.02383 -0.1123 0.7326 0.6911
4.250 0.7220 0.02888 0.02427 -0.1119 0.7211 0.6917
4.750 0.7695 0.02914 0.02461 -0.1121 0.7083 0.6919
5.250 0.8243 0.02889 0.02441 -0.1130 0.6901 0.6921
5.500 0.8705 0.02744 0.02294 -0.1160 0.6744 0.6922
5.750 0.9648 0.02266 0.01788 -0.1255 0.6344 0.6922
6.000 0.9927 0.02225 0.01725 -0.1256 0.6003 0.6923
6.250 1.0056 0.02282 0.01765 -0.1237 0.5677 0.6924
6.500 1.0096 0.02390 0.01850 -0.1204 0.5258 0.6924
6.750 1.0092 0.02527 0.01959 -0.1166 0.4753 0.6925
7.000 1.0096 0.02668 0.02071 -0.1131 0.4232 0.6926
7.250 1.0114 0.02807 0.02178 -0.1098 0.3682 0.6926
7.500 1.0181 0.02923 0.02267 -0.1073 0.3174 0.6927
7.750 1.0253 0.03039 0.02354 -0.1049 0.2631 0.6927
8.000 1.0326 0.03158 0.02441 -0.1026 0.2072 0.6927
8.250 1.0426 0.03264 0.02522 -0.1007 0.1617 0.6928
8.500 1.0562 0.03355 0.02597 -0.0994 0.1320 0.6928
8.750 1.0708 0.03441 0.02672 -0.0982 0.1091 0.6929
9.000 1.0859 0.03526 0.02749 -0.0971 0.0920 0.6931
9.250 1.1018 0.03607 0.02825 -0.0961 0.0792 0.6933
9.500 1.1186 0.03684 0.02900 -0.0953 0.0699 0.6933
9.750 1.1348 0.03766 0.02979 -0.0944 0.0608 0.6933
10.000 1.1504 0.03852 0.03061 -0.0935 0.0499 0.6933
10.500 1.1772 0.04059 0.03252 -0.0911 0.0256 0.6934
10.750 1.1910 0.04162 0.03355 -0.0899 0.0217 0.6934
11.000 1.2059 0.04259 0.03457 -0.0890 0.0195 0.6934
11.250 1.2204 0.04359 0.03561 -0.0880 0.0179 0.6934
11.500 1.2337 0.04469 0.03673 -0.0869 0.0163 0.6935
11.750 1.2481 0.04572 0.03782 -0.0859 0.0154 0.6935
12.000 1.2621 0.04680 0.03896 -0.0850 0.0146 0.6935
12.250 1.2752 0.04796 0.04018 -0.0840 0.0139 0.6935
12.500 1.2876 0.04919 0.04145 -0.0829 0.0132 0.6936
12.750 1.2987 0.05053 0.04285 -0.0817 0.0125 0.6936
13.000 1.3091 0.05194 0.04432 -0.0805 0.0120 0.6936
13.250 1.3209 0.05327 0.04573 -0.0796 0.0116 0.6936
13.500 1.3322 0.05465 0.04717 -0.0786 0.0111 0.6937
13.750 1.3429 0.05611 0.04870 -0.0776 0.0106 0.6937
14.000 1.3525 0.05768 0.05034 -0.0765 0.0103 0.6937
14.250 1.3615 0.05933 0.05205 -0.0755 0.0099 0.6938
14.500 1.3684 0.06121 0.05401 -0.0744 0.0096 0.6938
14.750 1.3730 0.06332 0.05619 -0.0731 0.0093 0.6938
15.000 1.3804 0.06521 0.05817 -0.0722 0.0091 0.6938
15.250 1.3873 0.06717 0.06023 -0.0713 0.0089 0.6939
15.500 1.3931 0.06929 0.06244 -0.0704 0.0087 0.6939
15.750 1.3989 0.07144 0.06468 -0.0696 0.0085 0.6940
16.000 1.4041 0.07370 0.06703 -0.0689 0.0082 0.6940
16.250 1.4090 0.07601 0.06943 -0.0682 0.0080 0.6940
16.500 1.4127 0.07849 0.07201 -0.0677 0.0078 0.6941
16.750 1.4163 0.08101 0.07462 -0.0672 0.0076 0.6941
17.000 1.4185 0.08372 0.07742 -0.0668 0.0075 0.6942
17.250 1.4187 0.08672 0.08051 -0.0664 0.0073 0.6942
17.500 1.4171 0.08999 0.08387 -0.0662 0.0072 0.6942
17.750 1.4147 0.09342 0.08740 -0.0660 0.0070 0.6943
18.000 1.4145 0.09662 0.09072 -0.0661 0.0069 0.6943
18.250 1.4136 0.09996 0.09418 -0.0663 0.0069 0.6944
18.500 1.4120 0.10344 0.09778 -0.0667 0.0068 0.6944
18.750 1.4097 0.10706 0.10153 -0.0673 0.0067 0.6944
19.000 1.4069 0.11080 0.10539 -0.0680 0.0066 0.6945
19.250 1.4034 0.11471 0.10943 -0.0689 0.0065 0.6945
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