WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il) Reynolds number: 100,000 Max Cl/Cd: 23.45 at α=10.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx3-il-100000-n5.txt Download as CSV file: xf-fx3-il-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.750 -0.3202 0.09341 0.08726 -0.1596 0.8762 0.0306
-14.500 -0.3508 0.08602 0.07976 -0.1632 0.8765 0.0305
-14.250 -0.3797 0.08014 0.07371 -0.1652 0.8767 0.0303
-14.000 -0.4076 0.07537 0.06875 -0.1658 0.8770 0.0303
-13.750 -0.4340 0.07149 0.06466 -0.1651 0.8773 0.0304
-13.500 -0.4594 0.06826 0.06120 -0.1634 0.8776 0.0306
-13.250 -0.4789 0.06600 0.05878 -0.1610 0.8778 0.0309
-13.000 -0.4933 0.06493 0.05766 -0.1577 0.8775 0.0312
-12.750 -0.5086 0.06410 0.05678 -0.1538 0.8777 0.0316
-12.500 -0.5264 0.06348 0.05611 -0.1492 0.8780 0.0319
-12.250 -0.5470 0.06296 0.05553 -0.1438 0.8784 0.0322
-12.000 -0.5687 0.06248 0.05498 -0.1380 0.8788 0.0325
-11.750 -0.6047 0.06251 0.05499 -0.1288 0.8794 0.0324
-11.500 -0.6245 0.06190 0.05429 -0.1230 0.8791 0.0327
-11.250 -0.6649 0.06191 0.05429 -0.1127 0.8799 0.0325
-11.000 -0.7000 0.06162 0.05397 -0.1036 0.8810 0.0324
-10.750 -0.7225 0.06097 0.05325 -0.0969 0.8816 0.0327
-10.500 -0.7372 0.06011 0.05229 -0.0917 0.8814 0.0332
-10.250 -0.7601 0.05941 0.05151 -0.0848 0.8824 0.0335
-10.000 -0.7736 0.05839 0.05036 -0.0795 0.8834 0.0342
-9.750 -0.7761 0.05696 0.04870 -0.0761 0.8835 0.0353
-9.500 -0.7698 0.05524 0.04667 -0.0736 0.8829 0.0367
-9.250 -0.7652 0.05373 0.04478 -0.0705 0.8833 0.0384
-9.000 -0.7616 0.05293 0.04402 -0.0677 0.8838 0.0397
-8.750 -0.7578 0.05225 0.04330 -0.0650 0.8844 0.0411
-8.500 -0.7458 0.05141 0.04233 -0.0634 0.8837 0.0434
-8.250 -0.7276 0.05042 0.04107 -0.0620 0.8829 0.0464
-8.000 -0.7146 0.04966 0.04028 -0.0602 0.8827 0.0488
-7.750 -0.7048 0.04909 0.03970 -0.0582 0.8828 0.0514
-7.500 -0.6902 0.04850 0.03896 -0.0566 0.8826 0.0550
-7.250 -0.6689 0.04793 0.03827 -0.0558 0.8815 0.0589
-7.000 -0.6463 0.04754 0.03790 -0.0557 0.8803 0.0632
-6.500 -0.6175 0.04673 0.03689 -0.0520 0.8778 0.0713
-6.250 -0.6131 0.04597 0.03621 -0.0485 0.8749 0.0745
-6.000 -0.6005 0.04552 0.03573 -0.0467 0.8731 0.0790
-5.750 -0.5843 0.04518 0.03529 -0.0453 0.8710 0.0837
-5.500 -0.5663 0.04473 0.03487 -0.0441 0.8688 0.0883
-5.250 -0.5453 0.04442 0.03455 -0.0438 0.8669 0.0939
-5.000 -0.5211 0.04430 0.03434 -0.0438 0.8654 0.0996
-4.750 -0.5048 0.04390 0.03394 -0.0426 0.8615 0.1045
-4.500 -0.4929 0.04341 0.03346 -0.0407 0.8575 0.1113
-4.250 -0.4736 0.04317 0.03325 -0.0400 0.8550 0.1216
-4.000 -0.4500 0.04296 0.03315 -0.0401 0.8525 0.1406
-3.750 -0.4232 0.04211 0.03300 -0.0419 0.8505 0.2436
-3.250 -0.4188 0.04650 0.03945 -0.0240 0.8411 0.6065
-2.750 -0.3396 0.04779 0.04017 -0.0338 0.8358 0.6804
-2.500 -0.3103 0.04898 0.04121 -0.0333 0.8341 0.6932
-2.250 -0.3131 0.04918 0.04141 -0.0268 0.8265 0.6985
-2.000 -0.2906 0.04977 0.04188 -0.0256 0.8232 0.7094
-1.750 -0.2645 0.05048 0.04248 -0.0249 0.8209 0.7219
-1.500 -0.2563 0.05103 0.04300 -0.0196 0.8163 0.7290
-1.250 -0.2406 0.05112 0.04301 -0.0179 0.8112 0.7387
-1.000 -0.2193 0.05134 0.04316 -0.0162 0.8082 0.7437
-0.750 -0.1885 0.05140 0.04309 -0.0178 0.8062 0.7476
-0.500 -0.1691 0.05115 0.04274 -0.0185 0.8005 0.7511
-0.250 -0.1458 0.05102 0.04253 -0.0188 0.7963 0.7533
0.000 -0.1191 0.05100 0.04243 -0.0192 0.7937 0.7548
0.250 -0.0876 0.05105 0.04240 -0.0206 0.7919 0.7562
0.500 -0.0780 0.05084 0.04216 -0.0186 0.7846 0.7581
0.750 -0.0497 0.05083 0.04209 -0.0197 0.7816 0.7600
1.000 -0.0166 0.05087 0.04206 -0.0217 0.7796 0.7616
1.250 -0.0009 0.05077 0.04193 -0.0212 0.7728 0.7631
1.500 0.0300 0.05078 0.04189 -0.0232 0.7697 0.7647
1.750 0.0660 0.05083 0.04189 -0.0260 0.7676 0.7663
2.000 0.0850 0.05084 0.04189 -0.0264 0.7606 0.7676
2.250 0.1173 0.05084 0.04186 -0.0285 0.7576 0.7684
2.500 0.1492 0.05077 0.04177 -0.0298 0.7556 0.7692
2.750 0.1611 0.05074 0.04178 -0.0283 0.7476 0.7702
3.000 0.1928 0.05066 0.04170 -0.0298 0.7450 0.7710
3.250 0.2109 0.05072 0.04178 -0.0295 0.7380 0.7716
3.500 0.2414 0.05064 0.04171 -0.0309 0.7344 0.7722
3.750 0.2754 0.05053 0.04162 -0.0328 0.7322 0.7731
4.000 0.2907 0.05066 0.04180 -0.0321 0.7237 0.7739
4.250 0.3246 0.05054 0.04171 -0.0340 0.7209 0.7745
4.500 0.3440 0.05070 0.04192 -0.0341 0.7131 0.7750
4.750 0.3748 0.05059 0.04187 -0.0355 0.7091 0.7757
5.000 0.4101 0.05035 0.04169 -0.0375 0.7066 0.7764
5.250 0.4267 0.05068 0.04209 -0.0373 0.6970 0.7766
5.500 0.4611 0.05045 0.04192 -0.0393 0.6937 0.7767
5.750 0.4818 0.05073 0.04229 -0.0395 0.6853 0.7770
6.000 0.5125 0.05059 0.04224 -0.0409 0.6805 0.7776
6.250 0.5485 0.05020 0.04195 -0.0429 0.6776 0.7781
6.500 0.5664 0.05065 0.04250 -0.0429 0.6673 0.7782
6.750 0.6015 0.05024 0.04220 -0.0447 0.6634 0.7782
7.250 0.6569 0.05008 0.04229 -0.0466 0.6490 0.7782
7.500 0.6946 0.04932 0.04167 -0.0485 0.6458 0.7782
7.750 0.7141 0.04972 0.04220 -0.0484 0.6345 0.7782
8.000 0.7512 0.04879 0.04143 -0.0500 0.6303 0.7784
8.250 0.7779 0.04812 0.04088 -0.0500 0.6162 0.7788
8.500 0.8104 0.04683 0.03970 -0.0504 0.5990 0.7792
8.750 0.8426 0.04589 0.03885 -0.0510 0.5812 0.7794
9.000 0.8733 0.04536 0.03844 -0.0517 0.5644 0.7793
9.250 0.9015 0.04506 0.03826 -0.0522 0.5443 0.7793
9.500 0.9331 0.04447 0.03774 -0.0529 0.5198 0.7793
9.750 0.9668 0.04368 0.03693 -0.0538 0.4874 0.7793
10.000 0.9977 0.04311 0.03622 -0.0542 0.4431 0.7793
10.250 1.0169 0.04337 0.03616 -0.0533 0.3801 0.7792
10.500 1.0227 0.04474 0.03710 -0.0513 0.3100 0.7791
10.750 1.0230 0.04670 0.03862 -0.0490 0.2449 0.7790
11.000 1.0244 0.04874 0.04028 -0.0471 0.1914 0.7789
11.250 1.0301 0.05055 0.04185 -0.0457 0.1550 0.7788
11.750 1.0485 0.05380 0.04495 -0.0439 0.1128 0.7787
12.000 1.0584 0.05542 0.04656 -0.0432 0.0966 0.7787
12.250 1.0675 0.05714 0.04831 -0.0424 0.0824 0.7788
12.500 1.0756 0.05897 0.05014 -0.0416 0.0697 0.7790
12.750 1.0828 0.06093 0.05210 -0.0407 0.0591 0.7792
13.000 1.0893 0.06300 0.05419 -0.0399 0.0516 0.7793
13.250 1.0974 0.06497 0.05626 -0.0392 0.0456 0.7794
13.500 1.1033 0.06716 0.05847 -0.0385 0.0416 0.7794
13.750 1.1110 0.06922 0.06067 -0.0379 0.0381 0.7793
14.000 1.1171 0.07147 0.06300 -0.0374 0.0360 0.7793
14.250 1.1222 0.07385 0.06547 -0.0369 0.0342 0.7792
14.500 1.1301 0.07598 0.06777 -0.0365 0.0323 0.7791
14.750 1.1374 0.07819 0.07011 -0.0362 0.0305 0.7791
15.000 1.1436 0.08054 0.07256 -0.0360 0.0290 0.7791
15.250 1.1488 0.08300 0.07510 -0.0358 0.0279 0.7791
15.500 1.1552 0.08532 0.07747 -0.0354 0.0270 0.7790
15.750 1.1642 0.08747 0.07984 -0.0352 0.0263 0.7790
16.000 1.1719 0.08981 0.08239 -0.0351 0.0254 0.7791
16.250 1.1778 0.09241 0.08521 -0.0351 0.0244 0.7791
16.500 1.1820 0.09521 0.08820 -0.0354 0.0236 0.7791
16.750 1.1847 0.09822 0.09138 -0.0358 0.0228 0.7791
17.000 1.1867 0.10136 0.09467 -0.0363 0.0222 0.7791
17.250 1.1882 0.10461 0.09807 -0.0370 0.0218 0.7791
17.500 1.1889 0.10801 0.10162 -0.0378 0.0214 0.7791
17.750 1.1884 0.11165 0.10543 -0.0387 0.0210 0.7791
18.250 1.1783 0.12068 0.11490 -0.0418 0.0206 0.7790
18.500 1.1678 0.12634 0.12085 -0.0445 0.0205 0.7789
18.750 1.1551 0.13265 0.12745 -0.0478 0.0204 0.7788
19.000 1.1404 0.13965 0.13473 -0.0520 0.0203 0.7787
19.250 1.1237 0.14753 0.14287 -0.0571 0.0203 0.7786
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