WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 75-141 (fx75141-il) Reynolds number: 200,000 Max Cl/Cd: 83.77 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx75141-il-200000.txt Download as CSV file: xf-fx75141-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.750 -0.1815 0.10521 0.10182 -0.0746 0.9620 0.0683
-11.500 -0.1774 0.10081 0.09741 -0.0780 0.9599 0.0714
-11.250 -0.3327 0.10966 0.10623 -0.0629 0.9781 0.0645
-11.000 -0.3123 0.10727 0.10381 -0.0640 0.9731 0.0668
-10.750 -0.3004 0.10310 0.09962 -0.0679 0.9689 0.0693
-10.500 -0.3241 0.09214 0.08871 -0.0856 0.9619 0.0743
-10.250 -0.3136 0.08641 0.08297 -0.0876 0.9593 0.0756
-10.000 -0.2882 0.08459 0.08111 -0.0873 0.9572 0.0770
-9.750 -0.4269 0.04414 0.03934 -0.1288 0.9394 0.0432
-9.500 -0.4244 0.04011 0.03501 -0.1297 0.9329 0.0429
-9.250 -0.4161 0.03642 0.03089 -0.1308 0.9281 0.0429
-9.000 -0.4009 0.03343 0.02741 -0.1319 0.9245 0.0432
-8.750 -0.3924 0.03058 0.02425 -0.1310 0.9198 0.0443
-8.500 -0.3729 0.02932 0.02298 -0.1308 0.9159 0.0461
-8.250 -0.3512 0.02790 0.02139 -0.1309 0.9128 0.0476
-8.000 -0.3272 0.02621 0.01941 -0.1312 0.9099 0.0490
-7.750 -0.3019 0.02481 0.01768 -0.1315 0.9072 0.0509
-7.500 -0.2863 0.02391 0.01655 -0.1298 0.9032 0.0528
-7.250 -0.2653 0.02274 0.01543 -0.1292 0.8996 0.0558
-7.000 -0.2404 0.02195 0.01455 -0.1291 0.8965 0.0586
-6.750 -0.2133 0.02123 0.01365 -0.1291 0.8939 0.0618
-6.500 -0.1864 0.02016 0.01258 -0.1294 0.8915 0.0663
-6.250 -0.1702 0.01984 0.01227 -0.1277 0.8874 0.0705
-6.000 -0.1485 0.01941 0.01174 -0.1267 0.8836 0.0750
-5.750 -0.1252 0.01872 0.01114 -0.1264 0.8802 0.0820
-5.500 -0.0985 0.01813 0.01052 -0.1265 0.8774 0.0902
-5.250 -0.0731 0.01779 0.01017 -0.1264 0.8745 0.1005
-5.000 -0.0572 0.01743 0.00991 -0.1247 0.8697 0.1125
-4.750 -0.0341 0.01699 0.00953 -0.1243 0.8658 0.1327
-4.500 -0.0084 0.01632 0.00910 -0.1245 0.8625 0.1729
-4.250 0.0184 0.01547 0.00871 -0.1253 0.8598 0.2697
-4.000 0.0333 0.01497 0.00879 -0.1238 0.8548 0.3986
-3.750 0.0552 0.01484 0.00897 -0.1228 0.8504 0.4954
-3.500 0.0825 0.01485 0.00909 -0.1225 0.8471 0.5501
-3.250 0.1118 0.01499 0.00925 -0.1223 0.8443 0.5874
-3.000 0.1319 0.01538 0.00968 -0.1206 0.8396 0.6118
-2.750 0.1547 0.01571 0.00997 -0.1195 0.8345 0.6344
-2.500 0.1830 0.01601 0.01024 -0.1190 0.8311 0.6526
-2.250 0.2130 0.01629 0.01046 -0.1188 0.8282 0.6686
-2.000 0.2316 0.01674 0.01091 -0.1169 0.8224 0.6815
-1.750 0.2549 0.01704 0.01121 -0.1156 0.8174 0.6916
-1.500 0.2842 0.01722 0.01134 -0.1153 0.8141 0.7040
-1.250 0.3147 0.01739 0.01145 -0.1153 0.8114 0.7167
-1.000 0.3276 0.01780 0.01192 -0.1125 0.8037 0.7249
-0.750 0.3551 0.01787 0.01196 -0.1120 0.7997 0.7350
-0.500 0.3860 0.01792 0.01195 -0.1122 0.7968 0.7472
-0.250 0.4013 0.01821 0.01230 -0.1095 0.7899 0.7548
0.000 0.4278 0.01823 0.01229 -0.1093 0.7849 0.7640
0.250 0.4574 0.01812 0.01216 -0.1091 0.7817 0.7702
0.500 0.4834 0.01820 0.01221 -0.1089 0.7768 0.7787
0.750 0.5026 0.01828 0.01233 -0.1072 0.7699 0.7844
1.000 0.5339 0.01813 0.01215 -0.1076 0.7664 0.7920
1.250 0.5658 0.01795 0.01195 -0.1080 0.7638 0.7978
1.500 0.5798 0.01820 0.01226 -0.1057 0.7547 0.8049
1.750 0.6105 0.01801 0.01206 -0.1060 0.7508 0.8116
2.000 0.6423 0.01777 0.01181 -0.1063 0.7481 0.8171
2.250 0.6594 0.01800 0.01209 -0.1047 0.7393 0.8245
2.500 0.6876 0.01776 0.01187 -0.1044 0.7351 0.8300
2.750 0.7206 0.01748 0.01159 -0.1051 0.7323 0.8361
3.000 0.7380 0.01762 0.01180 -0.1034 0.7234 0.8424
3.250 0.7675 0.01730 0.01151 -0.1033 0.7191 0.8479
3.500 0.8032 0.01688 0.01109 -0.1043 0.7161 0.8540
3.750 0.8198 0.01683 0.01113 -0.1022 0.7060 0.8599
4.000 0.8569 0.01602 0.01029 -0.1031 0.7011 0.8652
4.250 0.8790 0.01573 0.01007 -0.1018 0.6902 0.8717
4.500 0.9104 0.01518 0.00953 -0.1019 0.6846 0.8769
4.750 0.9311 0.01506 0.00950 -0.1005 0.6749 0.8834
5.000 0.9598 0.01475 0.00923 -0.1004 0.6680 0.8892
5.250 0.9827 0.01455 0.00910 -0.0992 0.6588 0.8958
5.500 1.0074 0.01437 0.00898 -0.0985 0.6488 0.9027
5.750 1.0368 0.01405 0.00867 -0.0984 0.6400 0.9093
6.000 1.0593 0.01396 0.00864 -0.0973 0.6272 0.9176
6.250 1.0831 0.01377 0.00847 -0.0962 0.6117 0.9266
6.500 1.1071 0.01366 0.00833 -0.0952 0.5926 0.9376
6.750 1.1321 0.01371 0.00843 -0.0948 0.5709 0.9543
7.000 1.1611 0.01386 0.00855 -0.0952 0.5486 1.0000
7.250 1.1820 0.01417 0.00883 -0.0943 0.5253 1.0000
7.500 1.2009 0.01455 0.00913 -0.0929 0.4993 1.0000
7.750 1.2156 0.01501 0.00953 -0.0909 0.4692 1.0000
8.000 1.2247 0.01558 0.00996 -0.0879 0.4358 1.0000
8.250 1.2288 0.01632 0.01054 -0.0842 0.3958 1.0000
8.500 1.2285 0.01733 0.01132 -0.0801 0.3538 1.0000
8.750 1.2253 0.01862 0.01234 -0.0759 0.3123 1.0000
9.000 1.2230 0.02006 0.01357 -0.0723 0.2752 1.0000
9.250 1.2226 0.02158 0.01489 -0.0693 0.2424 1.0000
9.500 1.2235 0.02316 0.01630 -0.0666 0.2133 1.0000
9.750 1.2248 0.02482 0.01779 -0.0642 0.1865 1.0000
10.000 1.2268 0.02651 0.01934 -0.0620 0.1602 1.0000
10.250 1.2286 0.02830 0.02098 -0.0598 0.1347 1.0000
10.500 1.2284 0.03030 0.02281 -0.0576 0.1143 1.0000
10.750 1.2310 0.03218 0.02460 -0.0557 0.0998 1.0000
11.000 1.2336 0.03408 0.02644 -0.0540 0.0896 1.0000
11.250 1.2398 0.03578 0.02816 -0.0525 0.0815 1.0000
11.500 1.2416 0.03786 0.03017 -0.0507 0.0757 1.0000
11.750 1.2499 0.03945 0.03185 -0.0495 0.0706 1.0000
12.000 1.2544 0.04140 0.03376 -0.0482 0.0664 1.0000
12.250 1.2621 0.04316 0.03559 -0.0469 0.0629 1.0000
12.500 1.2708 0.04485 0.03735 -0.0459 0.0593 1.0000
12.750 1.2782 0.04670 0.03917 -0.0449 0.0562 1.0000
13.000 1.2895 0.04839 0.04089 -0.0438 0.0536 1.0000
13.250 1.2988 0.05011 0.04274 -0.0430 0.0510 1.0000
13.500 1.3087 0.05184 0.04452 -0.0422 0.0487 1.0000
13.750 1.3211 0.05353 0.04617 -0.0414 0.0464 1.0000
14.000 1.3344 0.05535 0.04810 -0.0406 0.0443 1.0000
14.250 1.3424 0.05734 0.05025 -0.0399 0.0426 1.0000
14.500 1.3507 0.05937 0.05240 -0.0392 0.0410 1.0000
14.750 1.3605 0.06136 0.05445 -0.0387 0.0396 1.0000
15.000 1.3814 0.06311 0.05616 -0.0381 0.0378 1.0000
15.250 1.3845 0.06596 0.05923 -0.0375 0.0369 1.0000
15.500 1.3831 0.06895 0.06249 -0.0371 0.0360 1.0000
15.750 1.3822 0.07207 0.06582 -0.0368 0.0351 1.0000
16.000 1.3813 0.07522 0.06915 -0.0367 0.0341 1.0000
16.250 1.3806 0.07851 0.07260 -0.0368 0.0334 1.0000
16.500 1.3788 0.08196 0.07619 -0.0371 0.0327 1.0000
16.750 1.3782 0.08538 0.07973 -0.0374 0.0321 1.0000
17.000 1.3790 0.08888 0.08333 -0.0378 0.0315 1.0000
17.250 1.3748 0.09362 0.08824 -0.0384 0.0309 1.0000
17.500 1.3588 0.09944 0.09430 -0.0400 0.0307 1.0000
17.750 1.3399 0.10551 0.10064 -0.0423 0.0306 1.0000
18.000 1.3200 0.11208 0.10746 -0.0452 0.0305 1.0000
18.250 1.2991 0.11922 0.11484 -0.0488 0.0305 1.0000
18.500 1.2770 0.12699 0.12284 -0.0531 0.0305 1.0000
18.750 1.2533 0.13546 0.13153 -0.0582 0.0306 1.0000
19.000 1.2294 0.14453 0.14079 -0.0639 0.0307 1.0000
19.250 1.2021 0.15507 0.15156 -0.0714 0.0310 1.0000
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