WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il) Reynolds number: 200,000 Max Cl/Cd: 57.91 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05191-il-200000-n5.txt Download as CSV file: xf-fx05191-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-191 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
------ -------- --------- --------- -------- -------- --------
-15.500 -0.4523 0.09241 0.08819 -0.1078 0.9495 0.0234
-15.250 -0.5065 0.07675 0.07216 -0.1194 0.9461 0.0230
-15.000 -0.5334 0.06787 0.06295 -0.1263 0.9417 0.0230
-14.750 -0.5490 0.06138 0.05614 -0.1314 0.9373 0.0231
-14.500 -0.5582 0.05613 0.05058 -0.1355 0.9332 0.0233
-14.250 -0.5644 0.05203 0.04619 -0.1380 0.9284 0.0235
-14.000 -0.5688 0.04847 0.04233 -0.1397 0.9234 0.0239
-13.750 -0.5698 0.04526 0.03877 -0.1411 0.9192 0.0242
-13.500 -0.5684 0.04275 0.03597 -0.1416 0.9148 0.0246
-13.250 -0.5636 0.04069 0.03367 -0.1416 0.9101 0.0249
-13.000 -0.5493 0.03904 0.03194 -0.1420 0.9066 0.0252
-12.750 -0.5343 0.03759 0.03038 -0.1424 0.9038 0.0256
-12.500 -0.5207 0.03629 0.02897 -0.1423 0.9009 0.0260
-12.250 -0.5072 0.03508 0.02764 -0.1418 0.8979 0.0263
-12.000 -0.4929 0.03396 0.02641 -0.1414 0.8950 0.0268
-11.750 -0.4765 0.03290 0.02523 -0.1410 0.8924 0.0272
-11.500 -0.4585 0.03188 0.02409 -0.1407 0.8902 0.0279
-11.250 -0.4395 0.03096 0.02304 -0.1406 0.8881 0.0286
-11.000 -0.4208 0.03013 0.02209 -0.1400 0.8856 0.0291
-10.750 -0.4043 0.02939 0.02124 -0.1392 0.8829 0.0299
-10.500 -0.3865 0.02863 0.02049 -0.1386 0.8807 0.0306
-10.250 -0.3694 0.02791 0.01977 -0.1379 0.8784 0.0314
-10.000 -0.3519 0.02723 0.01905 -0.1373 0.8762 0.0319
-9.750 -0.3345 0.02655 0.01832 -0.1366 0.8739 0.0328
-9.500 -0.3169 0.02590 0.01759 -0.1360 0.8715 0.0338
-9.250 -0.3047 0.02532 0.01698 -0.1343 0.8676 0.0345
-9.000 -0.2914 0.02471 0.01631 -0.1328 0.8634 0.0354
-8.750 -0.2790 0.02399 0.01557 -0.1314 0.8599 0.0366
-8.500 -0.2647 0.02337 0.01493 -0.1303 0.8573 0.0381
-8.250 -0.2510 0.02282 0.01434 -0.1289 0.8547 0.0398
-8.000 -0.2413 0.02235 0.01385 -0.1268 0.8511 0.0414
-7.750 -0.2313 0.02181 0.01328 -0.1247 0.8476 0.0432
-7.500 -0.2208 0.02122 0.01268 -0.1228 0.8444 0.0454
-7.250 -0.2069 0.02070 0.01211 -0.1213 0.8416 0.0484
-7.000 -0.1934 0.02017 0.01154 -0.1197 0.8390 0.0521
-6.750 -0.1890 0.01981 0.01122 -0.1164 0.8347 0.0568
-6.500 -0.1819 0.01942 0.01084 -0.1135 0.8305 0.0634
-6.250 -0.1738 0.01902 0.01043 -0.1107 0.8270 0.0730
-6.000 -0.1658 0.01854 0.01000 -0.1080 0.8241 0.0882
-5.750 -0.1631 0.01815 0.00973 -0.1044 0.8197 0.1110
-5.500 -0.1615 0.01764 0.00943 -0.1007 0.8147 0.1524
-5.250 -0.1575 0.01673 0.00888 -0.0978 0.8107 0.2312
-5.000 -0.1522 0.01541 0.00819 -0.0955 0.8076 0.3714
-4.750 -0.1395 0.01491 0.00808 -0.0936 0.8033 0.4617
-4.500 -0.1221 0.01474 0.00809 -0.0920 0.7986 0.5137
-4.250 -0.0973 0.01459 0.00805 -0.0917 0.7953 0.5559
-4.000 -0.0699 0.01454 0.00809 -0.0916 0.7928 0.5923
-3.750 -0.0400 0.01456 0.00814 -0.0918 0.7907 0.6207
-3.500 -0.0208 0.01475 0.00837 -0.0901 0.7857 0.6355
-3.250 0.0016 0.01486 0.00847 -0.0890 0.7811 0.6443
-3.000 0.0300 0.01479 0.00834 -0.0893 0.7779 0.6516
-2.750 0.0606 0.01470 0.00816 -0.0899 0.7754 0.6572
-2.500 0.0877 0.01472 0.00815 -0.0898 0.7722 0.6620
-2.250 0.1062 0.01477 0.00818 -0.0883 0.7658 0.6688
-2.000 0.1333 0.01474 0.00811 -0.0883 0.7622 0.6737
-1.750 0.1633 0.01471 0.00804 -0.0887 0.7594 0.6782
-1.500 0.1870 0.01470 0.00800 -0.0882 0.7544 0.6846
-1.250 0.2086 0.01475 0.00803 -0.0871 0.7486 0.6895
-1.000 0.2366 0.01474 0.00800 -0.0871 0.7451 0.6935
-0.750 0.2690 0.01464 0.00783 -0.0881 0.7425 0.6991
-0.500 0.2851 0.01475 0.00796 -0.0863 0.7346 0.7048
-0.250 0.3117 0.01475 0.00795 -0.0860 0.7302 0.7082
0.000 0.3435 0.01467 0.00782 -0.0868 0.7272 0.7128
0.250 0.3628 0.01475 0.00789 -0.0857 0.7195 0.7197
0.500 0.3887 0.01477 0.00791 -0.0853 0.7148 0.7225
0.750 0.4172 0.01475 0.00787 -0.0854 0.7105 0.7259
1.000 0.4377 0.01484 0.00797 -0.0843 0.7033 0.7312
1.250 0.4698 0.01475 0.00783 -0.0855 0.6989 0.7364
1.500 0.4942 0.01482 0.00791 -0.0848 0.6937 0.7391
1.750 0.5168 0.01490 0.00800 -0.0839 0.6874 0.7425
2.000 0.5488 0.01484 0.00790 -0.0849 0.6829 0.7467
2.250 0.5772 0.01486 0.00790 -0.0855 0.6771 0.7522
2.500 0.6004 0.01496 0.00802 -0.0847 0.6715 0.7546
2.750 0.6305 0.01497 0.00801 -0.0852 0.6670 0.7574
3.000 0.6540 0.01508 0.00814 -0.0846 0.6609 0.7611
3.250 0.6831 0.01513 0.00818 -0.0853 0.6553 0.7659
3.500 0.7155 0.01515 0.00818 -0.0864 0.6510 0.7692
3.750 0.7360 0.01532 0.00839 -0.0852 0.6452 0.7718
4.000 0.7590 0.01545 0.00855 -0.0845 0.6394 0.7747
4.250 0.7906 0.01553 0.00862 -0.0854 0.6349 0.7780
4.500 0.8163 0.01567 0.00879 -0.0856 0.6293 0.7825
4.750 0.8386 0.01582 0.00898 -0.0849 0.6234 0.7857
5.000 0.8669 0.01593 0.00911 -0.0851 0.6182 0.7879
5.250 0.8823 0.01611 0.00936 -0.0830 0.6109 0.7910
5.500 0.9060 0.01623 0.00948 -0.0825 0.6028 0.7944
5.750 0.9265 0.01641 0.00969 -0.0816 0.5943 0.7987
6.000 0.9493 0.01655 0.00986 -0.0810 0.5866 0.8017
6.250 0.9662 0.01676 0.01014 -0.0792 0.5796 0.8043
6.500 0.9833 0.01698 0.01039 -0.0775 0.5705 0.8073
6.750 0.9973 0.01726 0.01071 -0.0754 0.5582 0.8109
7.000 1.0137 0.01756 0.01101 -0.0740 0.5443 0.8148
7.250 1.0286 0.01787 0.01133 -0.0721 0.5313 0.8177
7.500 1.0411 0.01821 0.01168 -0.0698 0.5184 0.8202
7.750 1.0520 0.01866 0.01217 -0.0674 0.5044 0.8230
8.000 1.0647 0.01914 0.01269 -0.0655 0.4899 0.8262
8.250 1.0788 0.01967 0.01324 -0.0640 0.4741 0.8294
8.500 1.0916 0.02028 0.01384 -0.0624 0.4559 0.8322
8.750 1.0981 0.02098 0.01453 -0.0596 0.4342 0.8345
9.000 1.1010 0.02192 0.01539 -0.0566 0.4053 0.8371
9.250 1.0996 0.02320 0.01651 -0.0532 0.3664 0.8398
9.500 1.0922 0.02496 0.01802 -0.0495 0.3216 0.8427
9.750 1.0838 0.02702 0.01983 -0.0461 0.2757 0.8456
10.000 1.0746 0.02923 0.02179 -0.0428 0.2317 0.8478
10.250 1.0673 0.03136 0.02374 -0.0398 0.1942 0.8497
10.500 1.0644 0.03339 0.02563 -0.0374 0.1637 0.8518
10.750 1.0639 0.03539 0.02752 -0.0355 0.1377 0.8540
11.000 1.0671 0.03728 0.02933 -0.0341 0.1171 0.8560
11.250 1.0718 0.03915 0.03116 -0.0331 0.1032 0.8578
11.500 1.0786 0.04097 0.03296 -0.0323 0.0939 0.8598
11.750 1.0859 0.04283 0.03483 -0.0317 0.0870 0.8617
12.000 1.0933 0.04452 0.03657 -0.0309 0.0817 0.8634
12.250 1.1001 0.04629 0.03840 -0.0301 0.0769 0.8649
12.500 1.1053 0.04832 0.04046 -0.0293 0.0729 0.8664
12.750 1.1153 0.04997 0.04222 -0.0289 0.0690 0.8680
13.000 1.1230 0.05187 0.04419 -0.0285 0.0650 0.8697
13.250 1.1279 0.05412 0.04645 -0.0281 0.0617 0.8716
13.500 1.1386 0.05586 0.04832 -0.0280 0.0583 0.8735
13.750 1.1473 0.05788 0.05041 -0.0280 0.0550 0.8752
14.000 1.1531 0.06027 0.05282 -0.0280 0.0523 0.8766
14.250 1.1626 0.06228 0.05494 -0.0281 0.0496 0.8780
14.500 1.1704 0.06432 0.05708 -0.0280 0.0470 0.8793
14.750 1.1764 0.06662 0.05942 -0.0280 0.0447 0.8807
15.000 1.1819 0.06902 0.06187 -0.0280 0.0428 0.8822
15.250 1.1895 0.07121 0.06418 -0.0281 0.0408 0.8840
15.500 1.1965 0.07354 0.06660 -0.0283 0.0389 0.8859
15.750 1.2018 0.07613 0.06924 -0.0287 0.0374 0.8877
16.000 1.2070 0.07878 0.07195 -0.0291 0.0359 0.8893
16.250 1.2145 0.08122 0.07451 -0.0296 0.0344 0.8909
16.500 1.2209 0.08383 0.07721 -0.0302 0.0330 0.8924
17.000 1.2288 0.08958 0.08309 -0.0315 0.0308 0.8953
17.250 1.2336 0.09230 0.08594 -0.0320 0.0297 0.8969
17.500 1.2386 0.09504 0.08880 -0.0326 0.0287 0.8986
17.750 1.2428 0.09794 0.09182 -0.0334 0.0277 0.9004
18.000 1.2463 0.10102 0.09498 -0.0344 0.0268 0.9023
18.250 1.2487 0.10428 0.09832 -0.0355 0.0260 0.9043
18.500 1.2506 0.10763 0.10172 -0.0367 0.0253 0.9064
18.750 1.2545 0.11078 0.10504 -0.0379 0.0245 0.9086
19.000 1.2562 0.11399 0.10840 -0.0390 0.0237 0.9110
19.250 1.2576 0.11731 0.11184 -0.0402 0.0231 0.9136
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