WORTMANN FX 63-137 AIRFOIL (fx63137-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 63-137 AIRFOIL (fx63137-il) Reynolds number: 1,000,000 Max Cl/Cd: 132.52 at α=2.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx63137-il-1000000.txt Download as CSV file: xf-fx63137-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.5605 0.07422 0.07208 -0.0847 0.9955 0.0071
-13.250 -0.6564 0.04706 0.04445 -0.1106 0.9887 0.0068
-13.000 -0.6591 0.03837 0.03554 -0.1235 0.9843 0.0068
-12.750 -0.6590 0.03317 0.03018 -0.1304 0.9748 0.0068
-12.500 -0.6470 0.02858 0.02542 -0.1380 0.9652 0.0069
-12.250 -0.6190 0.02474 0.02141 -0.1469 0.9595 0.0069
-12.000 -0.5901 0.02191 0.01840 -0.1539 0.9504 0.0069
-11.750 -0.5501 0.01978 0.01609 -0.1608 0.9466 0.0070
-11.500 -0.5101 0.01826 0.01442 -0.1660 0.9427 0.0071
-11.250 -0.4712 0.01692 0.01293 -0.1704 0.9357 0.0072
-11.000 -0.4255 0.01580 0.01167 -0.1758 0.9309 0.0074
-10.750 -0.3785 0.01483 0.01056 -0.1811 0.9249 0.0075
-10.500 -0.3340 0.01402 0.00961 -0.1856 0.9158 0.0077
-10.250 -0.2950 0.01339 0.00885 -0.1887 0.9037 0.0078
-10.000 -0.2599 0.01289 0.00822 -0.1908 0.8908 0.0079
-9.750 -0.2278 0.01250 0.00772 -0.1921 0.8788 0.0082
-9.500 -0.1988 0.01214 0.00730 -0.1928 0.8668 0.0087
-9.250 -0.1699 0.01188 0.00702 -0.1933 0.8563 0.0093
-9.000 -0.1417 0.01189 0.00704 -0.1933 0.8464 0.0104
-8.750 -0.1131 0.01164 0.00671 -0.1937 0.8378 0.0126
-8.500 -0.0847 0.01156 0.00654 -0.1938 0.8295 0.0140
-8.250 -0.0568 0.01152 0.00644 -0.1937 0.8212 0.0149
-7.750 0.0003 0.01118 0.00600 -0.1943 0.8059 0.0162
-7.500 0.0290 0.01104 0.00580 -0.1946 0.7991 0.0169
-7.250 0.0580 0.01087 0.00557 -0.1949 0.7928 0.0174
-7.000 0.0869 0.01072 0.00537 -0.1952 0.7866 0.0178
-6.750 0.1154 0.01067 0.00525 -0.1954 0.7803 0.0182
-6.500 0.1462 0.01023 0.00475 -0.1963 0.7740 0.0189
-6.250 0.1761 0.00994 0.00443 -0.1970 0.7671 0.0195
-6.000 0.2058 0.00975 0.00418 -0.1975 0.7608 0.0201
-5.750 0.2358 0.00954 0.00395 -0.1981 0.7549 0.0208
-5.500 0.2655 0.00939 0.00373 -0.1985 0.7487 0.0213
-5.250 0.2957 0.00918 0.00347 -0.1991 0.7424 0.0221
-5.000 0.3261 0.00896 0.00321 -0.1997 0.7352 0.0231
-4.750 0.3558 0.00882 0.00301 -0.2002 0.7282 0.0238
-4.500 0.3859 0.00867 0.00283 -0.2006 0.7205 0.0243
-4.250 0.4153 0.00858 0.00267 -0.2010 0.7130 0.0247
-4.000 0.4456 0.00845 0.00253 -0.2014 0.7064 0.0252
-3.750 0.4755 0.00835 0.00239 -0.2018 0.6993 0.0261
-3.500 0.5053 0.00827 0.00230 -0.2022 0.6933 0.0274
-3.250 0.5352 0.00820 0.00223 -0.2026 0.6871 0.0300
-3.000 0.5642 0.00817 0.00217 -0.2028 0.6804 0.0340
-2.750 0.5941 0.00811 0.00209 -0.2032 0.6742 0.0378
-2.500 0.6235 0.00808 0.00203 -0.2034 0.6675 0.0409
-2.250 0.6529 0.00805 0.00197 -0.2037 0.6617 0.0444
-2.000 0.6832 0.00797 0.00193 -0.2042 0.6555 0.0530
-1.750 0.7125 0.00795 0.00190 -0.2045 0.6485 0.0687
-1.500 0.7430 0.00785 0.00187 -0.2051 0.6420 0.0971
-1.250 0.7738 0.00774 0.00184 -0.2058 0.6338 0.1424
-1.000 0.8061 0.00751 0.00182 -0.2070 0.6257 0.2327
-0.750 0.8372 0.00738 0.00182 -0.2079 0.6173 0.3054
-0.500 0.8675 0.00731 0.00187 -0.2085 0.6098 0.3678
-0.250 0.8970 0.00730 0.00193 -0.2089 0.6016 0.4063
0.000 0.9255 0.00736 0.00200 -0.2090 0.5921 0.4363
0.250 0.9531 0.00746 0.00208 -0.2090 0.5740 0.4573
0.500 0.9799 0.00762 0.00218 -0.2087 0.5532 0.4818
0.750 1.0070 0.00776 0.00229 -0.2085 0.5396 0.5006
1.000 1.0340 0.00792 0.00240 -0.2083 0.5271 0.5107
1.250 1.0611 0.00807 0.00251 -0.2082 0.5127 0.5199
1.500 1.0878 0.00825 0.00262 -0.2079 0.4960 0.5273
1.750 1.1142 0.00845 0.00276 -0.2076 0.4813 0.5361
2.000 1.1408 0.00863 0.00289 -0.2074 0.4683 0.5452
2.250 1.1675 0.00881 0.00304 -0.2071 0.4542 0.5553
2.750 1.2175 0.00939 0.00342 -0.2061 0.4131 0.5741
3.000 1.2430 0.00964 0.00362 -0.2057 0.3984 0.5805
3.250 1.2687 0.00987 0.00381 -0.2053 0.3812 0.5889
3.500 1.2932 0.01018 0.00403 -0.2047 0.3606 0.5983
3.750 1.3179 0.01048 0.00427 -0.2042 0.3463 0.6078
4.000 1.3425 0.01077 0.00451 -0.2036 0.3325 0.6154
4.250 1.3666 0.01110 0.00476 -0.2030 0.3090 0.6228
4.500 1.3889 0.01155 0.00508 -0.2021 0.2879 0.6297
4.750 1.4124 0.01189 0.00538 -0.2014 0.2715 0.6368
5.000 1.4331 0.01243 0.00577 -0.2002 0.2408 0.6441
5.250 1.4548 0.01288 0.00614 -0.1991 0.2260 0.6514
5.500 1.4779 0.01321 0.00645 -0.1984 0.2128 0.6598
5.750 1.4967 0.01382 0.00693 -0.1969 0.1863 0.6680
6.000 1.5176 0.01427 0.00733 -0.1957 0.1737 0.6776
6.250 1.5386 0.01467 0.00772 -0.1946 0.1629 0.6873
6.500 1.5531 0.01542 0.00831 -0.1923 0.1353 0.6982
6.750 1.5701 0.01589 0.00877 -0.1904 0.1265 0.7108
7.000 1.5890 0.01627 0.00919 -0.1889 0.1183 0.7250
7.250 1.6002 0.01705 0.00988 -0.1861 0.0977 0.7403
7.500 1.6144 0.01770 0.01051 -0.1838 0.0869 0.7571
7.750 1.6284 0.01835 0.01118 -0.1816 0.0792 0.7756
8.000 1.6449 0.01888 0.01176 -0.1798 0.0690 0.7981
8.250 1.6575 0.01962 0.01250 -0.1775 0.0638 0.8261
8.500 1.6708 0.02021 0.01319 -0.1752 0.0597 0.8750
8.750 1.6781 0.02069 0.01380 -0.1718 0.0584 1.0000
9.000 1.6921 0.02146 0.01459 -0.1699 0.0570 1.0000
9.250 1.7040 0.02237 0.01551 -0.1678 0.0550 1.0000
9.500 1.7158 0.02333 0.01648 -0.1658 0.0529 1.0000
9.750 1.7277 0.02431 0.01750 -0.1638 0.0513 1.0000
10.000 1.7406 0.02523 0.01847 -0.1621 0.0503 1.0000
10.250 1.7550 0.02608 0.01936 -0.1607 0.0498 1.0000
10.500 1.7687 0.02701 0.02034 -0.1592 0.0491 1.0000
10.750 1.7816 0.02801 0.02139 -0.1577 0.0480 1.0000
11.000 1.7935 0.02913 0.02256 -0.1562 0.0468 1.0000
11.250 1.8035 0.03044 0.02389 -0.1545 0.0450 1.0000
11.500 1.8118 0.03194 0.02542 -0.1529 0.0431 1.0000
11.750 1.8225 0.03328 0.02680 -0.1515 0.0415 1.0000
12.000 1.8368 0.03430 0.02786 -0.1505 0.0399 1.0000
12.250 1.8462 0.03581 0.02935 -0.1492 0.0360 1.0000
12.500 1.8523 0.03768 0.03118 -0.1477 0.0294 1.0000
12.750 1.8444 0.04104 0.03443 -0.1455 0.0177 1.0000
13.000 1.8282 0.04551 0.03891 -0.1431 0.0055 1.0000
13.250 1.8274 0.04848 0.04196 -0.1418 0.0041 1.0000
13.500 1.8301 0.05113 0.04469 -0.1408 0.0038 1.0000
13.750 1.8311 0.05406 0.04771 -0.1399 0.0034 1.0000
14.000 1.8340 0.05685 0.05059 -0.1391 0.0032 1.0000
14.250 1.8373 0.05964 0.05347 -0.1386 0.0031 1.0000
14.500 1.8392 0.06270 0.05662 -0.1381 0.0030 1.0000
14.750 1.8400 0.06597 0.05999 -0.1377 0.0029 1.0000
15.000 1.8407 0.06934 0.06345 -0.1375 0.0029 1.0000
15.250 1.8399 0.07302 0.06722 -0.1374 0.0028 1.0000
15.500 1.8376 0.07699 0.07130 -0.1374 0.0027 1.0000
15.750 1.8350 0.08110 0.07552 -0.1377 0.0026 1.0000
16.000 1.8323 0.08530 0.07982 -0.1380 0.0026 1.0000
16.250 1.8275 0.08992 0.08456 -0.1386 0.0025 1.0000
16.500 1.8224 0.09468 0.08944 -0.1394 0.0025 1.0000
16.750 1.8142 0.10005 0.09494 -0.1404 0.0024 1.0000
17.000 1.8063 0.10543 0.10044 -0.1417 0.0024 1.0000
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