WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=1,000,000 Ncrit=0
| Details | Polar file |
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Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Reynolds number: 1,000,000 Max Cl/Cd: 162.4 at α=3.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx62k131-il-1000000.txt Download as CSV file: xf-fx62k131-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 62-K-131 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.250 -0.1606 0.13427 0.13265 -0.0721 0.9763 0.0051
-14.000 -0.1530 0.13115 0.12952 -0.0746 0.9702 0.0053
-13.750 -0.1435 0.12763 0.12599 -0.0776 0.9640 0.0054
-13.500 -0.1337 0.12397 0.12231 -0.0807 0.9578 0.0056
-13.250 -0.1236 0.12008 0.11838 -0.0840 0.9496 0.0059
-13.000 -0.1144 0.11615 0.11441 -0.0870 0.9371 0.0061
-12.750 -0.1089 0.11255 0.11072 -0.0890 0.9209 0.0063
-12.500 -0.1058 0.10919 0.10727 -0.0904 0.9069 0.0064
-12.250 -0.1025 0.10587 0.10390 -0.0914 0.8973 0.0065
-12.000 -0.0993 0.10259 0.10058 -0.0924 0.8898 0.0065
-11.750 -0.0964 0.09912 0.09708 -0.0933 0.8834 0.0065
-11.500 -0.0938 0.09562 0.09354 -0.0943 0.8782 0.0065
-11.250 -0.0916 0.09199 0.08990 -0.0952 0.8736 0.0065
-11.000 -0.0887 0.08820 0.08609 -0.0964 0.8693 0.0065
-10.750 -0.0874 0.08439 0.08225 -0.0974 0.8653 0.0066
-10.500 -0.0854 0.08042 0.07828 -0.0987 0.8617 0.0066
-10.250 -0.0843 0.07628 0.07413 -0.0999 0.8581 0.0066
-10.000 -0.0837 0.07212 0.06996 -0.1012 0.8548 0.0066
-9.750 -0.0835 0.06772 0.06553 -0.1027 0.8516 0.0066
-9.500 -0.0834 0.06323 0.06105 -0.1044 0.8487 0.0066
-9.250 -0.1614 0.07721 0.07500 -0.1027 0.8604 0.0066
-9.000 -0.1578 0.07260 0.07038 -0.1059 0.8556 0.0066
-8.750 -0.1544 0.06752 0.06527 -0.1099 0.8511 0.0066
-8.500 -0.1511 0.06035 0.05811 -0.1175 0.8467 0.0066
-8.250 -0.1527 0.05380 0.05147 -0.1246 0.8417 0.0066
-8.000 -0.1555 0.04883 0.04636 -0.1296 0.8368 0.0066
-7.750 -0.1500 0.04374 0.04112 -0.1352 0.8328 0.0066
-7.500 -0.1410 0.03899 0.03616 -0.1385 0.8293 0.0066
-7.250 -0.1403 0.02983 0.02646 -0.1432 0.8254 0.0069
-7.000 -0.1196 0.02725 0.02367 -0.1452 0.8226 0.0073
-6.750 -0.0955 0.02571 0.02201 -0.1467 0.8201 0.0077
-6.500 -0.0697 0.02386 0.01997 -0.1479 0.8176 0.0086
-6.250 -0.0385 0.02456 0.02052 -0.1477 0.8152 0.0105
-6.000 -0.0111 0.02217 0.01780 -0.1491 0.8128 0.0106
-5.750 0.0151 0.01509 0.01011 -0.1507 0.8104 0.0081
-5.500 0.0439 0.01431 0.00923 -0.1514 0.8082 0.0088
-5.250 0.0715 0.01254 0.00727 -0.1513 0.8059 0.0084
-5.000 0.1000 0.01113 0.00572 -0.1517 0.8031 0.0081
-4.750 0.1304 0.01037 0.00488 -0.1526 0.8002 0.0085
-4.500 0.1616 0.00989 0.00432 -0.1537 0.7973 0.0096
-4.250 0.1924 0.00965 0.00402 -0.1546 0.7946 0.0105
-4.000 0.2274 0.00886 0.00314 -0.1568 0.7923 0.0125
-3.750 0.2586 0.00862 0.00289 -0.1579 0.7899 0.0152
-3.500 0.2910 0.00832 0.00252 -0.1591 0.7875 0.0193
-3.250 0.3263 0.00785 0.00221 -0.1613 0.7853 0.0766
-3.000 0.3787 0.00647 0.00187 -0.1688 0.7834 0.4123
-2.750 0.4218 0.00596 0.00179 -0.1730 0.7812 0.5771
-2.500 0.4548 0.00585 0.00181 -0.1744 0.7789 0.6324
-2.250 0.4856 0.00585 0.00183 -0.1752 0.7762 0.6603
-2.000 0.5157 0.00587 0.00184 -0.1757 0.7735 0.6759
-1.750 0.5451 0.00593 0.00191 -0.1761 0.7709 0.6926
-1.500 0.5747 0.00601 0.00193 -0.1766 0.7682 0.7007
-1.250 0.6041 0.00603 0.00195 -0.1771 0.7655 0.7055
-1.000 0.6332 0.00606 0.00198 -0.1775 0.7626 0.7100
-0.750 0.6629 0.00609 0.00199 -0.1780 0.7595 0.7144
-0.500 0.6924 0.00612 0.00199 -0.1786 0.7565 0.7182
-0.250 0.7213 0.00617 0.00203 -0.1789 0.7530 0.7214
0.000 0.7499 0.00618 0.00206 -0.1792 0.7484 0.7253
0.250 0.7789 0.00621 0.00207 -0.1796 0.7436 0.7296
0.500 0.8078 0.00627 0.00209 -0.1800 0.7395 0.7329
0.750 0.8362 0.00628 0.00215 -0.1802 0.7353 0.7360
1.000 0.8646 0.00633 0.00221 -0.1805 0.7309 0.7398
1.250 0.8934 0.00640 0.00226 -0.1808 0.7264 0.7435
1.500 0.9222 0.00642 0.00231 -0.1812 0.7213 0.7465
1.750 0.9502 0.00645 0.00236 -0.1814 0.7159 0.7490
2.000 0.9782 0.00651 0.00243 -0.1816 0.7108 0.7515
2.250 1.0065 0.00655 0.00252 -0.1818 0.7045 0.7542
2.500 1.0347 0.00663 0.00258 -0.1821 0.6984 0.7570
2.750 1.0633 0.00668 0.00265 -0.1824 0.6902 0.7594
3.000 1.0904 0.00674 0.00272 -0.1824 0.6783 0.7615
3.250 1.1157 0.00687 0.00281 -0.1820 0.6579 0.7637
3.500 1.1402 0.00708 0.00293 -0.1815 0.6304 0.7659
3.750 1.1650 0.00731 0.00309 -0.1810 0.6052 0.7683
4.000 1.1883 0.00766 0.00331 -0.1803 0.5742 0.7709
4.250 1.2117 0.00802 0.00356 -0.1797 0.5443 0.7733
4.500 1.2323 0.00852 0.00388 -0.1785 0.5019 0.7753
4.750 1.2500 0.00919 0.00429 -0.1768 0.4435 0.7773
5.000 1.2644 0.01009 0.00483 -0.1745 0.3724 0.7795
5.250 1.2766 0.01114 0.00548 -0.1719 0.2968 0.7819
5.500 1.2878 0.01223 0.00617 -0.1692 0.2233 0.7843
5.750 1.2972 0.01341 0.00696 -0.1662 0.1515 0.7866
6.000 1.3099 0.01431 0.00762 -0.1638 0.1062 0.7888
6.250 1.3187 0.01527 0.00834 -0.1606 0.0636 0.7908
6.500 1.3279 0.01606 0.00900 -0.1574 0.0366 0.7928
6.750 1.3357 0.01710 0.00989 -0.1540 0.0107 0.7950
7.000 1.3486 0.01790 0.01065 -0.1516 0.0044 0.7973
7.250 1.3641 0.01856 0.01135 -0.1497 0.0035 0.7996
7.500 1.3790 0.01927 0.01213 -0.1478 0.0031 0.8015
7.750 1.3930 0.02001 0.01297 -0.1458 0.0029 0.8033
8.000 1.4068 0.02076 0.01380 -0.1438 0.0028 0.8051
8.250 1.4197 0.02160 0.01472 -0.1417 0.0027 0.8071
8.500 1.4322 0.02249 0.01569 -0.1397 0.0026 0.8091
8.750 1.4436 0.02350 0.01678 -0.1376 0.0025 0.8112
9.000 1.4543 0.02459 0.01795 -0.1355 0.0024 0.8132
9.250 1.4644 0.02578 0.01922 -0.1334 0.0023 0.8150
9.500 1.4733 0.02703 0.02056 -0.1312 0.0021 0.8169
9.750 1.4810 0.02843 0.02206 -0.1290 0.0020 0.8187
10.000 1.4850 0.03013 0.02386 -0.1264 0.0018 0.8205
10.250 1.4846 0.03227 0.02613 -0.1234 0.0017 0.8222
10.500 1.4795 0.03490 0.02891 -0.1200 0.0016 0.8241
10.750 1.4752 0.03754 0.03172 -0.1168 0.0016 0.8258
11.000 1.4713 0.04027 0.03459 -0.1138 0.0016 0.8274
11.250 1.4727 0.04254 0.03698 -0.1114 0.0016 0.8288
11.500 1.4736 0.04490 0.03947 -0.1091 0.0016 0.8304
11.750 1.4730 0.04754 0.04227 -0.1066 0.0016 0.8319
12.000 1.4750 0.04990 0.04476 -0.1046 0.0016 0.8334
12.250 1.4771 0.05226 0.04725 -0.1028 0.0016 0.8349
12.500 1.4781 0.05483 0.04996 -0.1011 0.0016 0.8365
12.750 1.4790 0.05746 0.05273 -0.0996 0.0016 0.8381
13.000 1.4790 0.06020 0.05561 -0.0983 0.0016 0.8398
13.250 1.4781 0.06311 0.05866 -0.0971 0.0016 0.8413
13.500 1.4762 0.06624 0.06193 -0.0961 0.0017 0.8428
13.750 1.4730 0.06968 0.06554 -0.0952 0.0017 0.8442
14.000 1.2367 0.07593 0.07221 -0.0714 0.0016 0.8361
14.250 1.2216 0.07999 0.07642 -0.0705 0.0016 0.8369
14.500 1.1990 0.08351 0.08008 -0.0692 0.0017 0.8373
14.750 1.1806 0.08730 0.08403 -0.0688 0.0017 0.8381
15.000 1.1655 0.09124 0.08811 -0.0690 0.0017 0.8390
15.250 1.1516 0.09518 0.09219 -0.0696 0.0017 0.8400
15.500 1.1371 0.09940 0.09656 -0.0705 0.0017 0.8409
15.750 1.1206 0.10398 0.10129 -0.0718 0.0018 0.8416
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