WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 75-141 (fx75141-il) Reynolds number: 50,000 Max Cl/Cd: 26.74 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75141-il-50000-n5.txt Download as CSV file: xf-fx75141-il-50000-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 = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.750 -0.3949 0.10694 0.10005 -0.0579 1.0000 0.0625
-10.500 -0.4108 0.10448 0.09769 -0.0561 1.0000 0.0624
-10.250 -0.4273 0.10193 0.09524 -0.0543 1.0000 0.0623
-10.000 -0.4432 0.09912 0.09250 -0.0529 1.0000 0.0621
-9.750 -0.4571 0.09515 0.08860 -0.0533 0.9992 0.0618
-9.500 -0.4627 0.08814 0.08158 -0.0588 0.9935 0.0614
-9.250 -0.4773 0.08091 0.07432 -0.0652 0.9867 0.0609
-9.000 -0.4973 0.07488 0.06820 -0.0704 0.9787 0.0604
-8.750 -0.5186 0.06958 0.06275 -0.0743 0.9700 0.0601
-8.500 -0.5308 0.06447 0.05738 -0.0773 0.9627 0.0600
-8.250 -0.5359 0.05962 0.05216 -0.0798 0.9563 0.0604
-8.000 -0.5361 0.05522 0.04726 -0.0814 0.9507 0.0613
-7.750 -0.5322 0.05127 0.04271 -0.0823 0.9451 0.0629
-7.500 -0.5119 0.04912 0.04051 -0.0834 0.9416 0.0653
-7.250 -0.4921 0.04668 0.03777 -0.0844 0.9379 0.0677
-7.000 -0.4782 0.04429 0.03501 -0.0840 0.9331 0.0696
-6.750 -0.4567 0.04190 0.03204 -0.0847 0.9290 0.0733
-6.500 -0.4301 0.04003 0.02998 -0.0858 0.9258 0.0772
-6.250 -0.4034 0.03849 0.02823 -0.0865 0.9227 0.0812
-6.000 -0.3850 0.03725 0.02666 -0.0854 0.9179 0.0862
-5.750 -0.3608 0.03610 0.02547 -0.0854 0.9139 0.0918
-5.500 -0.3322 0.03505 0.02421 -0.0858 0.9106 0.0992
-5.250 -0.3011 0.03408 0.02322 -0.0868 0.9078 0.1081
-5.000 -0.2852 0.03348 0.02245 -0.0848 0.9023 0.1165
-4.750 -0.2621 0.03275 0.02175 -0.0845 0.8978 0.1283
-4.500 -0.2336 0.03197 0.02095 -0.0852 0.8941 0.1450
-4.250 -0.2054 0.03113 0.02024 -0.0860 0.8905 0.1685
-4.000 -0.1893 0.03048 0.01973 -0.0850 0.8846 0.1980
-3.750 -0.1630 0.02947 0.01909 -0.0860 0.8802 0.2600
-3.500 -0.1351 0.02850 0.01903 -0.0868 0.8767 0.3943
-3.250 -0.1215 0.02869 0.01961 -0.0838 0.8707 0.4987
-3.000 -0.1039 0.02921 0.02023 -0.0809 0.8649 0.5649
-2.750 -0.0783 0.02986 0.02079 -0.0794 0.8607 0.6171
-2.500 -0.0646 0.03049 0.02133 -0.0764 0.8541 0.6509
-2.250 -0.0459 0.03107 0.02177 -0.0739 0.8482 0.6810
-2.000 -0.0213 0.03156 0.02214 -0.0721 0.8441 0.7089
-1.750 -0.0109 0.03196 0.02244 -0.0690 0.8366 0.7317
-1.500 0.0081 0.03222 0.02260 -0.0667 0.8311 0.7518
-1.250 0.0348 0.03235 0.02260 -0.0657 0.8274 0.7726
-1.000 0.0408 0.03261 0.02280 -0.0620 0.8188 0.7898
-0.750 0.0649 0.03267 0.02274 -0.0611 0.8139 0.8072
-0.500 0.0847 0.03277 0.02275 -0.0598 0.8081 0.8211
-0.250 0.1018 0.03290 0.02279 -0.0583 0.8009 0.8332
0.000 0.1329 0.03290 0.02267 -0.0590 0.7967 0.8448
0.250 0.1459 0.03319 0.02289 -0.0572 0.7887 0.8568
0.500 0.1713 0.03326 0.02288 -0.0571 0.7830 0.8679
0.750 0.2052 0.03327 0.02281 -0.0582 0.7795 0.8785
1.000 0.2137 0.03368 0.02320 -0.0560 0.7698 0.8909
1.250 0.2461 0.03376 0.02323 -0.0571 0.7654 0.9026
1.500 0.2645 0.03414 0.02360 -0.0565 0.7575 0.9158
1.750 0.2956 0.03438 0.02383 -0.0578 0.7515 0.9287
2.000 0.3384 0.03450 0.02393 -0.0608 0.7479 0.9418
2.250 0.3616 0.03520 0.02466 -0.0620 0.7382 0.9626
2.500 0.3997 0.03539 0.02483 -0.0645 0.7334 1.0000
2.750 0.4150 0.03613 0.02555 -0.0642 0.7243 1.0000
3.000 0.4462 0.03651 0.02591 -0.0656 0.7187 1.0000
3.250 0.4674 0.03719 0.02657 -0.0659 0.7107 1.0000
3.500 0.4949 0.03771 0.02710 -0.0668 0.7041 1.0000
4.000 0.5443 0.03893 0.02834 -0.0680 0.6893 1.0000
4.250 0.5817 0.03907 0.02852 -0.0696 0.6851 1.0000
4.500 0.5941 0.04012 0.02960 -0.0689 0.6741 1.0000
5.000 0.6450 0.04117 0.03075 -0.0696 0.6585 1.0000
5.250 0.6650 0.04190 0.03154 -0.0695 0.6490 1.0000
5.500 0.6976 0.04199 0.03171 -0.0702 0.6424 1.0000
5.750 0.7146 0.04281 0.03260 -0.0696 0.6314 1.0000
6.000 0.7532 0.04240 0.03231 -0.0705 0.6258 1.0000
6.250 0.7695 0.04312 0.03311 -0.0696 0.6133 1.0000
6.500 0.7916 0.04345 0.03354 -0.0691 0.6019 1.0000
6.750 0.8324 0.04238 0.03263 -0.0694 0.5950 1.0000
7.000 0.8505 0.04282 0.03317 -0.0684 0.5817 1.0000
7.250 0.8722 0.04293 0.03341 -0.0675 0.5691 1.0000
7.500 0.9165 0.04122 0.03190 -0.0675 0.5626 1.0000
7.750 0.9353 0.04150 0.03231 -0.0663 0.5484 1.0000
8.000 0.9562 0.04158 0.03255 -0.0652 0.5341 1.0000
8.250 0.9792 0.04144 0.03258 -0.0641 0.5193 1.0000
8.500 1.0038 0.04109 0.03238 -0.0629 0.5033 1.0000
8.750 1.0306 0.04044 0.03187 -0.0616 0.4853 1.0000
9.000 1.0470 0.04064 0.03219 -0.0599 0.4627 1.0000
9.250 1.0694 0.04021 0.03183 -0.0583 0.4364 1.0000
9.500 1.0837 0.04053 0.03214 -0.0563 0.4047 1.0000
9.750 1.0947 0.04124 0.03278 -0.0544 0.3697 1.0000
10.000 1.1045 0.04215 0.03352 -0.0525 0.3333 1.0000
10.250 1.1115 0.04347 0.03463 -0.0506 0.2988 1.0000
10.500 1.1149 0.04528 0.03625 -0.0488 0.2681 1.0000
10.750 1.1170 0.04736 0.03817 -0.0473 0.2413 1.0000
11.000 1.1182 0.04961 0.04026 -0.0459 0.2183 1.0000
11.250 1.1196 0.05202 0.04261 -0.0447 0.1963 1.0000
11.500 1.1207 0.05452 0.04502 -0.0437 0.1773 1.0000
11.750 1.1226 0.05704 0.04748 -0.0428 0.1607 1.0000
12.000 1.1254 0.05957 0.04999 -0.0420 0.1460 1.0000
12.250 1.1298 0.06206 0.05247 -0.0413 0.1331 1.0000
12.500 1.1350 0.06452 0.05495 -0.0407 0.1221 1.0000
12.750 1.1406 0.06695 0.05734 -0.0401 0.1132 1.0000
13.000 1.1487 0.06927 0.05977 -0.0396 0.1050 1.0000
13.250 1.1573 0.07159 0.06214 -0.0391 0.0982 1.0000
13.500 1.1657 0.07396 0.06465 -0.0388 0.0920 1.0000
13.750 1.1771 0.07609 0.06683 -0.0382 0.0869 1.0000
14.000 1.1841 0.07886 0.06985 -0.0380 0.0819 1.0000
14.250 1.1940 0.08111 0.07211 -0.0378 0.0779 1.0000
14.500 1.2027 0.08394 0.07514 -0.0375 0.0745 1.0000
14.750 1.2027 0.08777 0.07930 -0.0379 0.0717 1.0000
15.000 1.2023 0.09152 0.08326 -0.0384 0.0690 1.0000
15.250 1.2060 0.09465 0.08648 -0.0387 0.0666 1.0000
15.500 1.2089 0.09817 0.09009 -0.0392 0.0646 1.0000
15.750 1.1946 0.10423 0.09652 -0.0412 0.0637 1.0000
16.000 1.1763 0.11116 0.10378 -0.0441 0.0631 1.0000
16.250 1.1533 0.11927 0.11218 -0.0481 0.0627 1.0000
16.500 1.1256 0.12900 0.12215 -0.0536 0.0627 1.0000
16.750 1.0907 0.14140 0.13477 -0.0613 0.0631 1.0000
17.000 1.0500 0.15732 0.15080 -0.0715 0.0637 1.0000
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