WORTMANN FX 63-137 AIRFOIL (fx63137-il) Xfoil prediction polar at RE=500,000 Ncrit=5
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Airfoil: WORTMANN FX 63-137 AIRFOIL (fx63137-il) Reynolds number: 500,000 Max Cl/Cd: 103.57 at α=1.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx63137-il-500000-n5.txt Download as CSV file: xf-fx63137-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.000 -0.5402 0.04129 0.03799 -0.1209 0.9491 0.0065
-11.750 -0.5411 0.03471 0.03116 -0.1304 0.9350 0.0064
-11.500 -0.5168 0.02925 0.02542 -0.1423 0.9248 0.0065
-11.250 -0.4778 0.02514 0.02102 -0.1542 0.9161 0.0067
-11.000 -0.4311 0.02252 0.01814 -0.1639 0.9091 0.0068
-10.750 -0.3891 0.02067 0.01606 -0.1705 0.9000 0.0069
-10.500 -0.3505 0.01927 0.01444 -0.1752 0.8901 0.0072
-10.000 -0.2838 0.01734 0.01219 -0.1807 0.8690 0.0076
-9.750 -0.2533 0.01667 0.01140 -0.1823 0.8594 0.0080
-9.500 -0.2240 0.01637 0.01108 -0.1832 0.8500 0.0088
-9.250 -0.1950 0.01637 0.01111 -0.1836 0.8417 0.0094
-9.000 -0.1663 0.01577 0.01034 -0.1845 0.8333 0.0118
-8.750 -0.1376 0.01522 0.00962 -0.1854 0.8259 0.0132
-8.500 -0.1091 0.01483 0.00909 -0.1859 0.8181 0.0144
-8.250 -0.0804 0.01457 0.00869 -0.1864 0.8112 0.0151
-8.000 -0.0517 0.01418 0.00824 -0.1870 0.8043 0.0156
-7.750 -0.0227 0.01386 0.00782 -0.1877 0.7978 0.0161
-7.500 0.0064 0.01355 0.00743 -0.1882 0.7917 0.0167
-7.250 0.0354 0.01326 0.00705 -0.1888 0.7851 0.0172
-7.000 0.0647 0.01301 0.00670 -0.1893 0.7787 0.0177
-6.750 0.0935 0.01281 0.00642 -0.1896 0.7723 0.0183
-6.500 0.1238 0.01237 0.00593 -0.1906 0.7665 0.0191
-6.250 0.1539 0.01209 0.00559 -0.1913 0.7617 0.0199
-6.000 0.1839 0.01182 0.00529 -0.1920 0.7566 0.0206
-5.750 0.2138 0.01159 0.00499 -0.1926 0.7510 0.0212
-5.500 0.2438 0.01139 0.00470 -0.1932 0.7455 0.0215
-5.250 0.2741 0.01115 0.00442 -0.1938 0.7397 0.0218
-5.000 0.3044 0.01093 0.00416 -0.1944 0.7337 0.0223
-4.750 0.3346 0.01076 0.00392 -0.1950 0.7284 0.0227
-4.500 0.3649 0.01058 0.00372 -0.1956 0.7230 0.0235
-4.250 0.3949 0.01044 0.00354 -0.1961 0.7168 0.0246
-4.000 0.4248 0.01032 0.00338 -0.1966 0.7104 0.0259
-3.750 0.4546 0.01019 0.00325 -0.1970 0.7028 0.0271
-3.500 0.4840 0.01011 0.00312 -0.1974 0.6952 0.0285
-3.250 0.5136 0.01002 0.00301 -0.1977 0.6873 0.0323
-3.000 0.5425 0.00998 0.00290 -0.1979 0.6791 0.0362
-2.750 0.5717 0.00993 0.00280 -0.1981 0.6703 0.0397
-2.500 0.6008 0.00989 0.00270 -0.1984 0.6616 0.0438
-2.250 0.6300 0.00984 0.00264 -0.1986 0.6510 0.0483
-2.000 0.6592 0.00979 0.00258 -0.1989 0.6402 0.0618
-1.750 0.6875 0.00981 0.00254 -0.1990 0.6286 0.0703
-1.500 0.7173 0.00973 0.00250 -0.1995 0.6189 0.0944
-1.250 0.7476 0.00964 0.00247 -0.2002 0.6109 0.1418
-1.000 0.7787 0.00950 0.00246 -0.2010 0.6032 0.2010
-0.750 0.8098 0.00937 0.00247 -0.2020 0.5955 0.2733
-0.500 0.8413 0.00923 0.00253 -0.2030 0.5867 0.3539
-0.250 0.8709 0.00922 0.00263 -0.2034 0.5780 0.4114
0.000 0.8997 0.00926 0.00272 -0.2036 0.5680 0.4475
0.250 0.9275 0.00936 0.00281 -0.2036 0.5586 0.4673
0.500 0.9549 0.00948 0.00291 -0.2034 0.5494 0.4816
0.750 0.9823 0.00961 0.00301 -0.2033 0.5407 0.4940
1.000 1.0087 0.00979 0.00313 -0.2030 0.5285 0.5053
1.250 1.0347 0.00999 0.00327 -0.2026 0.5079 0.5150
1.500 1.0590 0.01029 0.00344 -0.2019 0.4833 0.5258
1.750 1.0835 0.01059 0.00364 -0.2013 0.4634 0.5377
2.000 1.1091 0.01083 0.00383 -0.2009 0.4430 0.5496
2.250 1.1339 0.01111 0.00403 -0.2003 0.4242 0.5596
2.500 1.1591 0.01137 0.00423 -0.1998 0.4119 0.5674
2.750 1.1846 0.01160 0.00443 -0.1994 0.4003 0.5743
3.000 1.2100 0.01184 0.00463 -0.1990 0.3866 0.5804
3.250 1.2341 0.01216 0.00489 -0.1983 0.3668 0.5873
3.500 1.2578 0.01250 0.00514 -0.1976 0.3521 0.5939
3.750 1.2820 0.01280 0.00540 -0.1970 0.3390 0.5996
4.000 1.3057 0.01312 0.00569 -0.1963 0.3214 0.6058
4.250 1.3265 0.01364 0.00606 -0.1952 0.2946 0.6119
4.500 1.3485 0.01407 0.00641 -0.1942 0.2777 0.6179
4.750 1.3692 0.01456 0.00682 -0.1930 0.2514 0.6245
5.000 1.3887 0.01513 0.00726 -0.1916 0.2319 0.6310
5.250 1.4100 0.01554 0.00765 -0.1906 0.2214 0.6381
5.500 1.4308 0.01596 0.00806 -0.1894 0.2060 0.6462
5.750 1.4469 0.01657 0.00858 -0.1875 0.1850 0.6547
6.250 1.4818 0.01755 0.00954 -0.1839 0.1662 0.6746
6.500 1.4999 0.01800 0.01001 -0.1823 0.1515 0.6845
6.750 1.5123 0.01880 0.01071 -0.1799 0.1342 0.6942
7.000 1.5271 0.01945 0.01135 -0.1778 0.1256 0.7044
7.500 1.5575 0.02074 0.01269 -0.1740 0.1009 0.7303
7.750 1.5695 0.02161 0.01353 -0.1717 0.0933 0.7449
8.000 1.5842 0.02232 0.01429 -0.1699 0.0880 0.7607
8.250 1.5982 0.02308 0.01513 -0.1680 0.0831 0.7786
8.500 1.6116 0.02391 0.01602 -0.1661 0.0788 0.8004
8.750 1.6252 0.02470 0.01690 -0.1643 0.0687 0.8295
9.000 1.6261 0.02552 0.01784 -0.1602 0.0645 0.9308
9.250 1.6343 0.02673 0.01904 -0.1580 0.0593 1.0000
9.500 1.6457 0.02788 0.02022 -0.1563 0.0573 1.0000
9.750 1.6564 0.02912 0.02149 -0.1546 0.0555 1.0000
10.000 1.6668 0.03042 0.02282 -0.1529 0.0541 1.0000
10.250 1.6765 0.03182 0.02427 -0.1513 0.0526 1.0000
10.500 1.6853 0.03334 0.02584 -0.1497 0.0509 1.0000
10.750 1.6968 0.03466 0.02722 -0.1485 0.0498 1.0000
11.000 1.7079 0.03605 0.02869 -0.1473 0.0489 1.0000
11.250 1.7181 0.03755 0.03026 -0.1461 0.0478 1.0000
11.500 1.7275 0.03917 0.03195 -0.1449 0.0466 1.0000
11.750 1.7354 0.04097 0.03381 -0.1437 0.0451 1.0000
12.000 1.7421 0.04295 0.03585 -0.1425 0.0438 1.0000
12.250 1.7462 0.04526 0.03821 -0.1413 0.0420 1.0000
12.500 1.7565 0.04695 0.03997 -0.1405 0.0409 1.0000
12.750 1.7656 0.04880 0.04190 -0.1397 0.0397 1.0000
13.000 1.7734 0.05084 0.04400 -0.1389 0.0377 1.0000
13.250 1.7790 0.05318 0.04637 -0.1382 0.0350 1.0000
13.500 1.7849 0.05553 0.04878 -0.1375 0.0326 1.0000
13.750 1.7832 0.05889 0.05205 -0.1368 0.0227 1.0000
14.000 1.7730 0.06351 0.05665 -0.1361 0.0139 1.0000
14.250 1.7582 0.06895 0.06213 -0.1357 0.0054 1.0000
14.500 1.7536 0.07318 0.06646 -0.1356 0.0041 1.0000
14.750 1.7525 0.07699 0.07037 -0.1357 0.0037 1.0000
15.000 1.7523 0.08074 0.07423 -0.1359 0.0035 1.0000
15.250 1.7507 0.08476 0.07837 -0.1362 0.0033 1.0000
15.500 1.7500 0.08871 0.08244 -0.1366 0.0031 1.0000
15.750 1.7488 0.09282 0.08667 -0.1372 0.0030 1.0000
16.000 1.7476 0.09695 0.09092 -0.1380 0.0029 1.0000
16.250 1.7455 0.10129 0.09538 -0.1388 0.0028 1.0000
16.500 1.7431 0.10572 0.09992 -0.1399 0.0028 1.0000
16.750 1.7393 0.11042 0.10475 -0.1411 0.0026 1.0000
17.000 1.7355 0.11515 0.10960 -0.1424 0.0025 1.0000
17.250 1.7319 0.11989 0.11448 -0.1440 0.0025 1.0000
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