WORTMANN FX 63-137 AIRFOIL (fx63137-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 63-137 AIRFOIL (fx63137-il) Reynolds number: 1,000,000 Max Cl/Cd: 105.72 at α=1.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx63137-il-1000000-n5.txt Download as CSV file: xf-fx63137-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 63-137 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
------ -------- --------- --------- -------- -------- --------
-13.250 -0.2896 0.10874 0.10679 -0.0759 0.9863 0.0052
-13.000 -0.2960 0.10151 0.09952 -0.0806 0.9841 0.0052
-12.500 -0.5628 0.03603 0.03306 -0.1335 0.9435 0.0044
-12.250 -0.5364 0.02909 0.02582 -0.1494 0.9252 0.0045
-12.000 -0.4896 0.02429 0.02071 -0.1647 0.9093 0.0046
-11.750 -0.4500 0.02138 0.01754 -0.1746 0.8912 0.0047
-11.500 -0.4199 0.01949 0.01543 -0.1801 0.8744 0.0047
-11.250 -0.3950 0.01823 0.01398 -0.1825 0.8590 0.0048
-11.000 -0.3706 0.01736 0.01295 -0.1837 0.8453 0.0048
-10.750 -0.3458 0.01654 0.01198 -0.1847 0.8335 0.0049
-10.500 -0.3203 0.01579 0.01109 -0.1856 0.8237 0.0049
-10.000 -0.2673 0.01457 0.00963 -0.1869 0.8045 0.0051
-9.500 -0.2120 0.01351 0.00835 -0.1883 0.7902 0.0053
-9.250 -0.1838 0.01307 0.00781 -0.1889 0.7838 0.0054
-9.000 -0.1552 0.01265 0.00730 -0.1895 0.7781 0.0055
-8.750 -0.1258 0.01223 0.00681 -0.1903 0.7727 0.0056
-8.500 -0.0967 0.01187 0.00637 -0.1909 0.7666 0.0058
-8.250 -0.0675 0.01155 0.00597 -0.1915 0.7604 0.0059
-8.000 -0.0380 0.01124 0.00560 -0.1921 0.7532 0.0061
-7.500 0.0214 0.01066 0.00491 -0.1933 0.7411 0.0071
-7.250 0.0512 0.01040 0.00464 -0.1939 0.7352 0.0077
-7.000 0.0799 0.01031 0.00455 -0.1941 0.7298 0.0119
-6.750 0.1098 0.01014 0.00434 -0.1946 0.7244 0.0131
-6.500 0.1390 0.01002 0.00417 -0.1949 0.7172 0.0140
-6.250 0.1681 0.00992 0.00402 -0.1952 0.7101 0.0147
-6.000 0.1974 0.00983 0.00388 -0.1955 0.7019 0.0150
-5.750 0.2269 0.00968 0.00369 -0.1959 0.6948 0.0154
-5.500 0.2570 0.00952 0.00349 -0.1965 0.6875 0.0159
-5.250 0.2859 0.00943 0.00335 -0.1967 0.6789 0.0168
-5.000 0.3153 0.00933 0.00321 -0.1971 0.6694 0.0174
-4.750 0.3445 0.00926 0.00306 -0.1974 0.6602 0.0178
-4.500 0.3736 0.00919 0.00293 -0.1977 0.6477 0.0180
-4.250 0.4029 0.00912 0.00280 -0.1980 0.6340 0.0182
-4.000 0.4322 0.00905 0.00265 -0.1983 0.6211 0.0185
-3.750 0.4616 0.00898 0.00252 -0.1986 0.6105 0.0188
-3.500 0.4915 0.00891 0.00240 -0.1991 0.6024 0.0193
-3.250 0.5211 0.00885 0.00229 -0.1994 0.5954 0.0201
-3.000 0.5510 0.00879 0.00220 -0.1999 0.5868 0.0208
-2.750 0.5800 0.00879 0.00214 -0.2001 0.5753 0.0212
-2.500 0.6087 0.00881 0.00210 -0.2002 0.5612 0.0215
-2.250 0.6375 0.00883 0.00207 -0.2004 0.5508 0.0219
-2.000 0.6665 0.00885 0.00205 -0.2006 0.5425 0.0232
-1.750 0.6959 0.00884 0.00204 -0.2010 0.5341 0.0321
-1.500 0.7247 0.00887 0.00205 -0.2011 0.5269 0.0367
-1.250 0.7535 0.00890 0.00206 -0.2013 0.5170 0.0391
-1.000 0.7819 0.00896 0.00207 -0.2014 0.5043 0.0423
-0.750 0.8101 0.00904 0.00211 -0.2015 0.4910 0.0481
-0.500 0.8387 0.00910 0.00215 -0.2017 0.4809 0.0667
-0.250 0.8673 0.00915 0.00219 -0.2018 0.4727 0.0753
0.000 0.8962 0.00919 0.00225 -0.2022 0.4628 0.1088
0.250 0.9244 0.00931 0.00237 -0.2024 0.4315 0.1646
0.500 0.9529 0.00944 0.00254 -0.2030 0.4005 0.2627
0.750 0.9829 0.00948 0.00272 -0.2039 0.3735 0.3733
1.000 1.0094 0.00972 0.00291 -0.2037 0.3514 0.4087
1.250 1.0364 0.00990 0.00306 -0.2036 0.3383 0.4277
1.500 1.0635 0.01006 0.00320 -0.2035 0.3283 0.4412
1.750 1.0881 0.01041 0.00342 -0.2030 0.2988 0.4541
2.000 1.1138 0.01068 0.00363 -0.2026 0.2840 0.4707
2.250 1.1395 0.01094 0.00385 -0.2023 0.2682 0.4881
2.500 1.1626 0.01140 0.00417 -0.2015 0.2346 0.5026
2.750 1.1878 0.01169 0.00440 -0.2010 0.2229 0.5155
3.000 1.2125 0.01198 0.00464 -0.2005 0.2068 0.5245
3.250 1.2347 0.01249 0.00500 -0.1996 0.1785 0.5317
3.500 1.2593 0.01277 0.00525 -0.1990 0.1697 0.5425
3.750 1.2848 0.01299 0.00548 -0.1986 0.1637 0.5542
4.000 1.3067 0.01347 0.00585 -0.1976 0.1384 0.5625
4.250 1.3305 0.01378 0.00613 -0.1970 0.1316 0.5697
4.500 1.3546 0.01406 0.00640 -0.1963 0.1260 0.5760
4.750 1.3790 0.01431 0.00665 -0.1958 0.1206 0.5817
5.000 1.4007 0.01472 0.00702 -0.1947 0.1049 0.5874
5.250 1.4212 0.01520 0.00742 -0.1935 0.0939 0.5930
5.500 1.4435 0.01554 0.00775 -0.1926 0.0884 0.5987
5.750 1.4652 0.01588 0.00810 -0.1915 0.0840 0.6052
6.000 1.4846 0.01626 0.00848 -0.1901 0.0796 0.6115
6.250 1.5052 0.01654 0.00880 -0.1888 0.0772 0.6180
6.750 1.5375 0.01759 0.00978 -0.1848 0.0580 0.6336
7.000 1.5557 0.01802 0.01024 -0.1832 0.0565 0.6431
7.250 1.5733 0.01848 0.01074 -0.1816 0.0549 0.6527
7.500 1.5900 0.01901 0.01128 -0.1798 0.0525 0.6628
7.750 1.6067 0.01954 0.01186 -0.1781 0.0505 0.6722
8.000 1.6244 0.02002 0.01239 -0.1766 0.0500 0.6826
8.250 1.6419 0.02052 0.01296 -0.1751 0.0495 0.6943
8.500 1.6586 0.02108 0.01358 -0.1735 0.0490 0.7064
8.750 1.6748 0.02168 0.01425 -0.1719 0.0481 0.7196
9.000 1.6903 0.02234 0.01497 -0.1702 0.0473 0.7344
9.500 1.7173 0.02399 0.01673 -0.1666 0.0440 0.7679
9.750 1.7302 0.02490 0.01772 -0.1648 0.0425 0.7906
10.000 1.7445 0.02571 0.01863 -0.1633 0.0415 0.8217
10.250 1.7570 0.02638 0.01949 -0.1614 0.0408 0.9000
10.500 1.7658 0.02721 0.02040 -0.1590 0.0399 1.0000
10.750 1.7781 0.02826 0.02148 -0.1575 0.0379 1.0000
11.000 1.7881 0.02955 0.02277 -0.1558 0.0352 1.0000
11.250 1.7985 0.03084 0.02407 -0.1542 0.0320 1.0000
11.500 1.7987 0.03306 0.02619 -0.1519 0.0211 1.0000
11.750 1.7946 0.03582 0.02894 -0.1494 0.0114 1.0000
12.000 1.7882 0.03897 0.03212 -0.1470 0.0036 1.0000
12.250 1.7942 0.04097 0.03418 -0.1457 0.0030 1.0000
12.500 1.8003 0.04302 0.03630 -0.1444 0.0027 1.0000
12.750 1.8058 0.04519 0.03854 -0.1433 0.0025 1.0000
13.000 1.8116 0.04739 0.04081 -0.1423 0.0023 1.0000
13.250 1.8173 0.04965 0.04314 -0.1414 0.0022 1.0000
13.500 1.8224 0.05204 0.04561 -0.1405 0.0021 1.0000
13.750 1.8260 0.05468 0.04833 -0.1398 0.0019 1.0000
14.000 1.8291 0.05745 0.05117 -0.1391 0.0019 1.0000
14.250 1.8320 0.06031 0.05411 -0.1386 0.0018 1.0000
14.500 1.8339 0.06340 0.05729 -0.1381 0.0017 1.0000
14.750 1.8343 0.06674 0.06073 -0.1378 0.0016 1.0000
15.000 1.8350 0.07013 0.06421 -0.1376 0.0016 1.0000
15.250 1.8354 0.07364 0.06780 -0.1375 0.0015 1.0000
15.500 1.8362 0.07716 0.07141 -0.1376 0.0015 1.0000
15.750 1.8363 0.08085 0.07519 -0.1378 0.0015 1.0000
16.000 1.8358 0.08468 0.07911 -0.1381 0.0015 1.0000
16.250 1.8345 0.08871 0.08324 -0.1385 0.0014 1.0000
16.500 1.8326 0.09289 0.08752 -0.1392 0.0014 1.0000
16.750 1.8298 0.09729 0.09202 -0.1399 0.0014 1.0000
17.000 1.8272 0.10167 0.09650 -0.1408 0.0013 1.0000
17.250 1.8231 0.10636 0.10129 -0.1419 0.0013 1.0000
17.500 1.8198 0.11095 0.10599 -0.1431 0.0013 1.0000
17.750 1.8163 0.11559 0.11072 -0.1445 0.0012 1.0000
18.000 1.8118 0.12045 0.11568 -0.1460 0.0012 1.0000
18.250 1.8072 0.12535 0.12069 -0.1477 0.0012 1.0000
18.500 1.8036 0.13006 0.12549 -0.1495 0.0012 1.0000
18.750 1.7979 0.13517 0.13071 -0.1516 0.0012 1.0000
19.000 1.7928 0.14017 0.13582 -0.1538 0.0012 1.0000
19.250 1.7880 0.14515 0.14089 -0.1560 0.0011 1.0000
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