WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 75-141 (fx75141-il) Reynolds number: 100,000 Max Cl/Cd: 53.45 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75141-il-100000-n5.txt Download as CSV file: xf-fx75141-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 75-141
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.250 -0.3944 0.09460 0.08963 -0.0668 0.9763 0.0360
-11.000 -0.4032 0.08508 0.08010 -0.0739 0.9660 0.0359
-10.750 -0.4254 0.07195 0.06689 -0.0858 0.9566 0.0355
-10.500 -0.4524 0.06025 0.05491 -0.0995 0.9465 0.0351
-10.250 -0.4702 0.05245 0.04671 -0.1093 0.9367 0.0352
-10.000 -0.4809 0.04723 0.04104 -0.1144 0.9264 0.0354
-9.750 -0.4843 0.04294 0.03621 -0.1168 0.9186 0.0358
-9.500 -0.4776 0.03973 0.03257 -0.1178 0.9127 0.0363
-9.250 -0.4592 0.03764 0.03031 -0.1190 0.9092 0.0372
-9.000 -0.4423 0.03611 0.02861 -0.1193 0.9051 0.0384
-8.750 -0.4266 0.03463 0.02689 -0.1191 0.9003 0.0402
-8.500 -0.4078 0.03271 0.02456 -0.1194 0.8963 0.0422
-8.250 -0.3853 0.03075 0.02221 -0.1198 0.8933 0.0438
-8.000 -0.3615 0.02944 0.02084 -0.1203 0.8907 0.0454
-7.750 -0.3433 0.02861 0.01992 -0.1194 0.8865 0.0476
-7.500 -0.3215 0.02761 0.01870 -0.1191 0.8828 0.0507
-7.250 -0.2974 0.02649 0.01742 -0.1190 0.8799 0.0534
-7.000 -0.2717 0.02560 0.01652 -0.1194 0.8773 0.0563
-6.750 -0.2462 0.02487 0.01564 -0.1195 0.8746 0.0608
-6.500 -0.2289 0.02422 0.01495 -0.1180 0.8702 0.0643
-6.250 -0.2075 0.02362 0.01436 -0.1174 0.8665 0.0685
-6.000 -0.1824 0.02305 0.01368 -0.1173 0.8633 0.0748
-5.750 -0.1568 0.02239 0.01306 -0.1175 0.8607 0.0816
-5.500 -0.1349 0.02193 0.01256 -0.1169 0.8572 0.0900
-5.250 -0.1164 0.02159 0.01221 -0.1156 0.8527 0.0994
-5.000 -0.0934 0.02112 0.01178 -0.1153 0.8490 0.1131
-4.750 -0.0671 0.02061 0.01131 -0.1155 0.8459 0.1328
-4.500 -0.0392 0.02004 0.01087 -0.1161 0.8434 0.1650
-4.250 -0.0226 0.01970 0.01073 -0.1147 0.8383 0.2068
-4.000 -0.0011 0.01918 0.01050 -0.1143 0.8341 0.2748
-3.750 0.0233 0.01857 0.01038 -0.1143 0.8307 0.3813
-3.500 0.0505 0.01835 0.01046 -0.1141 0.8280 0.4775
-3.250 0.0694 0.01852 0.01075 -0.1123 0.8232 0.5284
-3.000 0.0904 0.01876 0.01105 -0.1107 0.8184 0.5670
-2.750 0.1162 0.01900 0.01129 -0.1098 0.8149 0.5982
-2.500 0.1449 0.01922 0.01145 -0.1094 0.8122 0.6231
-2.250 0.1641 0.01961 0.01179 -0.1076 0.8070 0.6424
-2.000 0.1858 0.01993 0.01206 -0.1062 0.8019 0.6606
-1.750 0.2127 0.02015 0.01220 -0.1056 0.7984 0.6767
-1.500 0.2421 0.02028 0.01225 -0.1055 0.7958 0.6904
-1.250 0.2570 0.02065 0.01261 -0.1031 0.7889 0.7031
-1.000 0.2814 0.02082 0.01272 -0.1023 0.7844 0.7165
-0.750 0.3093 0.02086 0.01272 -0.1019 0.7812 0.7261
-0.500 0.3310 0.02102 0.01283 -0.1009 0.7759 0.7345
-0.250 0.3511 0.02117 0.01297 -0.0995 0.7698 0.7420
0.000 0.3805 0.02114 0.01287 -0.0998 0.7662 0.7496
0.250 0.4114 0.02105 0.01274 -0.1001 0.7636 0.7560
0.500 0.4239 0.02141 0.01312 -0.0978 0.7548 0.7639
0.750 0.4507 0.02137 0.01307 -0.0974 0.7507 0.7698
1.000 0.4834 0.02126 0.01291 -0.0982 0.7480 0.7769
1.250 0.4937 0.02161 0.01332 -0.0954 0.7389 0.7830
1.500 0.5216 0.02156 0.01326 -0.0953 0.7347 0.7896
1.750 0.5541 0.02140 0.01309 -0.0960 0.7319 0.7958
2.000 0.5634 0.02179 0.01355 -0.0930 0.7221 0.8022
2.250 0.5938 0.02169 0.01345 -0.0934 0.7183 0.8089
2.750 0.6344 0.02193 0.01377 -0.0909 0.7050 0.8212
3.000 0.6665 0.02172 0.01360 -0.0915 0.7017 0.8271
3.250 0.6783 0.02209 0.01404 -0.0890 0.6923 0.8337
3.500 0.7084 0.02194 0.01393 -0.0893 0.6879 0.8402
3.750 0.7269 0.02208 0.01414 -0.0877 0.6806 0.8464
4.000 0.7512 0.02205 0.01418 -0.0871 0.6742 0.8532
4.250 0.7856 0.02166 0.01385 -0.0878 0.6707 0.8593
4.500 0.7972 0.02198 0.01426 -0.0852 0.6601 0.8673
4.750 0.8333 0.02144 0.01379 -0.0861 0.6557 0.8739
5.000 0.8485 0.02149 0.01393 -0.0839 0.6440 0.8829
5.250 0.8719 0.02119 0.01371 -0.0827 0.6329 0.8918
5.500 0.9050 0.02060 0.01319 -0.0829 0.6232 0.9013
5.750 0.9293 0.02044 0.01313 -0.0821 0.6120 0.9135
6.000 0.9555 0.02038 0.01319 -0.0818 0.6005 0.9303
6.250 0.9877 0.02013 0.01304 -0.0824 0.5890 1.0000
6.500 1.0204 0.02002 0.01297 -0.0832 0.5767 1.0000
6.750 1.0488 0.02004 0.01303 -0.0832 0.5622 1.0000
7.000 1.0720 0.02023 0.01324 -0.0826 0.5455 1.0000
7.250 1.0907 0.02052 0.01356 -0.0812 0.5255 1.0000
7.500 1.1102 0.02077 0.01376 -0.0798 0.5006 1.0000
7.750 1.1232 0.02126 0.01418 -0.0775 0.4714 1.0000
8.000 1.1350 0.02185 0.01466 -0.0752 0.4385 1.0000
8.250 1.1440 0.02264 0.01531 -0.0727 0.4018 1.0000
8.500 1.1502 0.02364 0.01611 -0.0701 0.3617 1.0000
8.750 1.1539 0.02489 0.01712 -0.0674 0.3224 1.0000
9.000 1.1565 0.02633 0.01833 -0.0648 0.2866 1.0000
9.250 1.1594 0.02787 0.01968 -0.0625 0.2550 1.0000
9.500 1.1631 0.02944 0.02111 -0.0604 0.2277 1.0000
9.750 1.1668 0.03109 0.02264 -0.0585 0.2035 1.0000
10.000 1.1721 0.03269 0.02415 -0.0568 0.1813 1.0000
10.250 1.1771 0.03436 0.02575 -0.0551 0.1614 1.0000
10.500 1.1815 0.03613 0.02744 -0.0536 0.1429 1.0000
10.750 1.1873 0.03785 0.02912 -0.0522 0.1258 1.0000
11.000 1.1923 0.03967 0.03090 -0.0508 0.1115 1.0000
11.250 1.1966 0.04160 0.03280 -0.0495 0.0996 1.0000
11.500 1.2010 0.04358 0.03476 -0.0483 0.0900 1.0000
11.750 1.2065 0.04551 0.03673 -0.0472 0.0823 1.0000
12.000 1.2091 0.04772 0.03891 -0.0461 0.0768 1.0000
12.250 1.2156 0.04966 0.04095 -0.0452 0.0714 1.0000
12.500 1.2193 0.05189 0.04321 -0.0443 0.0669 1.0000
12.750 1.2235 0.05415 0.04553 -0.0435 0.0633 1.0000
13.000 1.2299 0.05625 0.04775 -0.0428 0.0598 1.0000
13.250 1.2343 0.05858 0.05014 -0.0422 0.0568 1.0000
13.500 1.2377 0.06107 0.05262 -0.0417 0.0543 1.0000
13.750 1.2452 0.06323 0.05496 -0.0412 0.0518 1.0000
14.000 1.2508 0.06562 0.05746 -0.0408 0.0492 1.0000
14.250 1.2554 0.06813 0.06004 -0.0406 0.0473 1.0000
14.500 1.2600 0.07067 0.06257 -0.0403 0.0455 1.0000
14.750 1.2665 0.07316 0.06529 -0.0400 0.0438 1.0000
15.000 1.2718 0.07582 0.06813 -0.0399 0.0421 1.0000
15.250 1.2758 0.07863 0.07108 -0.0400 0.0406 1.0000
15.500 1.2787 0.08158 0.07410 -0.0402 0.0392 1.0000
15.750 1.2825 0.08439 0.07693 -0.0405 0.0379 1.0000
16.000 1.2839 0.08774 0.08047 -0.0409 0.0368 1.0000
16.250 1.2827 0.09157 0.08457 -0.0415 0.0358 1.0000
16.500 1.2803 0.09560 0.08885 -0.0425 0.0349 1.0000
16.750 1.2763 0.09992 0.09338 -0.0437 0.0340 1.0000
17.000 1.2715 0.10438 0.09803 -0.0453 0.0332 1.0000
17.250 1.2668 0.10885 0.10265 -0.0470 0.0325 1.0000
17.500 1.2628 0.11326 0.10718 -0.0489 0.0318 1.0000
17.750 1.2609 0.11731 0.11130 -0.0506 0.0311 1.0000
18.000 1.2538 0.12249 0.11661 -0.0531 0.0306 1.0000
18.250 1.2365 0.12991 0.12431 -0.0573 0.0304 1.0000
18.500 1.2171 0.13813 0.13281 -0.0623 0.0302 1.0000
18.750 1.1944 0.14757 0.14250 -0.0684 0.0301 1.0000
19.000 1.1663 0.15903 0.15420 -0.0762 0.0302 1.0000
19.250 1.1265 0.17497 0.17033 -0.0871 0.0305 1.0000
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