WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Reynolds number: 1,000,000 Max Cl/Cd: 153.32 at α=2.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx62k131-il-1000000-n5.txt Download as CSV file: xf-fx62k131-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.500 -0.1072 0.09452 0.09218 -0.0916 0.8289 0.0025
-11.250 -0.1084 0.09010 0.08774 -0.0927 0.8264 0.0024
-10.750 -0.2158 0.09656 0.09415 -0.0878 0.8386 0.0021
-10.500 -0.2143 0.09196 0.08955 -0.0900 0.8349 0.0021
-10.250 -0.2130 0.08736 0.08495 -0.0924 0.8311 0.0021
-10.000 -0.2123 0.08265 0.08024 -0.0951 0.8274 0.0021
-9.500 -0.2123 0.07264 0.07023 -0.1018 0.8207 0.0021
-9.250 -0.2152 0.06636 0.06397 -0.1068 0.8169 0.0022
-9.000 -0.2311 0.05465 0.05224 -0.1198 0.8121 0.0021
-8.750 -0.2477 0.04690 0.04434 -0.1278 0.8077 0.0021
-8.500 -0.2467 0.04077 0.03800 -0.1339 0.8041 0.0022
-8.250 -0.2368 0.03613 0.03313 -0.1369 0.8009 0.0023
-8.000 -0.2229 0.03156 0.02828 -0.1391 0.7980 0.0024
-7.750 -0.2072 0.02580 0.02209 -0.1411 0.7954 0.0027
-7.500 -0.1895 0.01811 0.01362 -0.1428 0.7931 0.0030
-7.250 -0.1636 0.01588 0.01104 -0.1436 0.7909 0.0031
-7.000 -0.1365 0.01449 0.00943 -0.1442 0.7886 0.0032
-6.750 -0.1088 0.01362 0.00841 -0.1448 0.7863 0.0034
-6.500 -0.0806 0.01298 0.00765 -0.1454 0.7842 0.0036
-6.250 -0.0521 0.01251 0.00709 -0.1460 0.7822 0.0038
-6.000 -0.0233 0.01197 0.00646 -0.1466 0.7802 0.0039
-5.750 0.0067 0.01078 0.00513 -0.1479 0.7781 0.0041
-5.500 0.0373 0.01022 0.00449 -0.1491 0.7759 0.0045
-5.250 0.0678 0.00987 0.00410 -0.1501 0.7736 0.0049
-5.000 0.0985 0.00957 0.00375 -0.1511 0.7711 0.0055
-4.750 0.1292 0.00931 0.00342 -0.1521 0.7682 0.0061
-4.500 0.1599 0.00907 0.00315 -0.1531 0.7650 0.0065
-4.250 0.1920 0.00872 0.00275 -0.1544 0.7617 0.0077
-4.000 0.2228 0.00855 0.00256 -0.1554 0.7590 0.0093
-3.750 0.2537 0.00839 0.00237 -0.1563 0.7566 0.0105
-3.500 0.2850 0.00820 0.00215 -0.1573 0.7543 0.0143
-3.250 0.3160 0.00805 0.00200 -0.1583 0.7521 0.0207
-3.000 0.3484 0.00781 0.00186 -0.1597 0.7496 0.0509
-2.750 0.3826 0.00747 0.00172 -0.1617 0.7470 0.1205
-2.500 0.4280 0.00657 0.00151 -0.1670 0.7445 0.3516
-2.250 0.4729 0.00593 0.00139 -0.1718 0.7420 0.5373
-2.000 0.5069 0.00581 0.00139 -0.1735 0.7394 0.5974
-1.750 0.5391 0.00575 0.00142 -0.1747 0.7364 0.6395
-1.500 0.5693 0.00575 0.00143 -0.1753 0.7332 0.6540
-1.250 0.5991 0.00577 0.00142 -0.1759 0.7300 0.6613
-1.000 0.6286 0.00580 0.00144 -0.1764 0.7268 0.6677
-0.750 0.6584 0.00582 0.00144 -0.1770 0.7235 0.6732
-0.500 0.6880 0.00584 0.00147 -0.1775 0.7196 0.6777
-0.250 0.7172 0.00588 0.00149 -0.1780 0.7149 0.6825
0.000 0.7463 0.00592 0.00150 -0.1784 0.7089 0.6880
0.250 0.7750 0.00597 0.00155 -0.1788 0.7013 0.6928
0.500 0.8039 0.00602 0.00159 -0.1791 0.6949 0.6974
0.750 0.8328 0.00607 0.00162 -0.1796 0.6887 0.7023
1.000 0.8613 0.00613 0.00169 -0.1799 0.6824 0.7067
1.250 0.8897 0.00620 0.00176 -0.1802 0.6744 0.7110
1.500 0.9181 0.00628 0.00182 -0.1805 0.6658 0.7148
1.750 0.9461 0.00637 0.00189 -0.1807 0.6561 0.7178
2.000 0.9739 0.00647 0.00198 -0.1809 0.6455 0.7204
2.250 1.0015 0.00658 0.00209 -0.1810 0.6340 0.7232
2.500 1.0288 0.00671 0.00219 -0.1811 0.6209 0.7259
2.750 1.0554 0.00689 0.00231 -0.1810 0.6047 0.7287
3.000 1.0804 0.00716 0.00248 -0.1807 0.5780 0.7313
3.250 1.1025 0.00762 0.00276 -0.1798 0.5359 0.7335
3.500 1.1232 0.00817 0.00309 -0.1786 0.4871 0.7358
3.750 1.1453 0.00865 0.00339 -0.1778 0.4470 0.7383
4.000 1.1661 0.00921 0.00373 -0.1767 0.4002 0.7408
4.250 1.1849 0.00990 0.00417 -0.1753 0.3474 0.7433
4.500 1.2045 0.01053 0.00459 -0.1741 0.3025 0.7455
4.750 1.2169 0.01161 0.00525 -0.1716 0.2235 0.7476
5.000 1.2289 0.01268 0.00594 -0.1690 0.1522 0.7497
5.250 1.2424 0.01361 0.00660 -0.1667 0.0988 0.7518
5.500 1.2579 0.01438 0.00718 -0.1647 0.0628 0.7542
5.750 1.2747 0.01503 0.00772 -0.1630 0.0391 0.7565
6.000 1.2895 0.01567 0.00826 -0.1608 0.0217 0.7586
6.250 1.3044 0.01620 0.00877 -0.1586 0.0129 0.7605
6.500 1.3188 0.01684 0.00938 -0.1564 0.0045 0.7624
6.750 1.3346 0.01742 0.00999 -0.1545 0.0026 0.7644
7.000 1.3510 0.01796 0.01059 -0.1527 0.0022 0.7664
7.250 1.3664 0.01858 0.01126 -0.1508 0.0018 0.7683
7.500 1.3814 0.01924 0.01198 -0.1489 0.0015 0.7702
7.750 1.3977 0.01984 0.01265 -0.1473 0.0015 0.7721
8.000 1.4131 0.02051 0.01337 -0.1456 0.0014 0.7740
8.250 1.4276 0.02125 0.01419 -0.1438 0.0013 0.7757
8.500 1.4417 0.02204 0.01504 -0.1421 0.0013 0.7774
8.750 1.4549 0.02291 0.01598 -0.1402 0.0012 0.7791
9.000 1.4678 0.02382 0.01696 -0.1384 0.0011 0.7810
9.250 1.4800 0.02482 0.01804 -0.1365 0.0011 0.7829
9.500 1.4919 0.02585 0.01913 -0.1348 0.0010 0.7847
9.750 1.5027 0.02701 0.02036 -0.1329 0.0010 0.7864
10.000 1.5134 0.02818 0.02161 -0.1311 0.0009 0.7880
10.250 1.5237 0.02942 0.02295 -0.1293 0.0009 0.7896
10.500 1.5335 0.03068 0.02430 -0.1275 0.0008 0.7912
10.750 1.5420 0.03211 0.02581 -0.1257 0.0008 0.7928
11.000 1.5491 0.03366 0.02745 -0.1237 0.0007 0.7945
11.250 1.5552 0.03532 0.02921 -0.1218 0.0007 0.7962
11.500 1.5588 0.03722 0.03121 -0.1196 0.0007 0.7979
11.750 1.5485 0.04045 0.03462 -0.1162 0.0006 0.7993
12.000 1.5538 0.04226 0.03653 -0.1145 0.0006 0.8008
12.250 1.5576 0.04425 0.03862 -0.1128 0.0006 0.8023
12.500 1.5626 0.04618 0.04066 -0.1113 0.0005 0.8037
12.750 1.5658 0.04835 0.04294 -0.1098 0.0005 0.8051
13.000 1.5674 0.05073 0.04544 -0.1082 0.0005 0.8064
13.250 1.5680 0.05326 0.04809 -0.1068 0.0005 0.8078
13.500 1.5679 0.05595 0.05092 -0.1054 0.0005 0.8094
13.750 1.5678 0.05874 0.05383 -0.1042 0.0005 0.8109
14.000 1.5657 0.06182 0.05704 -0.1031 0.0005 0.8124
14.250 1.5627 0.06512 0.06048 -0.1022 0.0005 0.8138
14.500 1.5588 0.06859 0.06408 -0.1014 0.0005 0.8150
14.750 1.5537 0.07237 0.06800 -0.1008 0.0005 0.8161
15.000 1.5473 0.07646 0.07225 -0.1005 0.0004 0.8172
15.250 1.5397 0.08080 0.07675 -0.1004 0.0004 0.8185
15.500 1.5306 0.08549 0.08159 -0.1005 0.0004 0.8198
15.750 1.5208 0.09044 0.08671 -0.1010 0.0004 0.8211
16.000 1.5110 0.09556 0.09197 -0.1018 0.0004 0.8224
16.250 1.4992 0.10116 0.09774 -0.1030 0.0004 0.8237
16.500 1.4859 0.10719 0.10393 -0.1046 0.0004 0.8248
16.750 1.4738 0.11313 0.11002 -0.1065 0.0004 0.8260
17.000 1.4582 0.11995 0.11700 -0.1091 0.0004 0.8270
17.250 1.4441 0.12672 0.12392 -0.1119 0.0004 0.8280
17.500 1.4300 0.13375 0.13111 -0.1153 0.0004 0.8290
18.000 1.4003 0.14893 0.14659 -0.1234 0.0004 0.8308
18.250 1.3854 0.15691 0.15472 -0.1281 0.0004 0.8319
18.500 1.3678 0.16600 0.16396 -0.1337 0.0004 0.8328
18.750 1.3530 0.17485 0.17295 -0.1394 0.0004 0.8338
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