WORTMANN FX 74-080 (fx74080-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: WORTMANN FX 74-080 (fx74080-il) Reynolds number: 500,000 Max Cl/Cd: 134.44 at α=3.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx74080-il-500000.txt Download as CSV file: xf-fx74080-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 74-080
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.250 -0.1192 0.08704 0.08462 -0.0859 0.9261 0.0075
-10.000 -0.1103 0.08317 0.08072 -0.0883 0.9216 0.0078
-9.750 -0.1023 0.07951 0.07704 -0.0905 0.9168 0.0081
-9.500 -0.0938 0.07582 0.07331 -0.0928 0.9126 0.0084
-9.250 -0.0861 0.07215 0.06961 -0.0949 0.9088 0.0085
-9.000 -0.0799 0.06862 0.06607 -0.0966 0.9043 0.0089
-8.750 -0.0726 0.06510 0.06253 -0.0986 0.9003 0.0091
-8.500 -0.0649 0.06137 0.05877 -0.1010 0.8971 0.0096
-8.250 -0.0596 0.05801 0.05541 -0.1025 0.8933 0.0101
-8.000 -0.0538 0.05463 0.05203 -0.1045 0.8895 0.0109
-7.750 -0.0471 0.05132 0.04870 -0.1067 0.8859 0.0113
-5.250 0.0397 0.03355 0.02997 -0.1406 0.8590 0.0139
-5.000 0.0585 0.03100 0.02727 -0.1409 0.8564 0.0145
-4.750 0.0765 0.02994 0.02617 -0.1409 0.8535 0.0181
-4.500 0.0990 0.02756 0.02357 -0.1406 0.8507 0.0204
-4.250 0.1283 0.02693 0.02267 -0.1399 0.8483 0.0232
-4.000 0.1526 0.02513 0.02055 -0.1396 0.8460 0.0234
-3.000 0.2432 0.01464 0.00887 -0.1369 0.8363 0.0186
-2.750 0.2697 0.01244 0.00628 -0.1358 0.8341 0.0142
-2.500 0.2954 0.01128 0.00498 -0.1352 0.8321 0.0152
-2.250 0.3214 0.01072 0.00434 -0.1349 0.8301 0.0176
-2.000 0.3460 0.01046 0.00404 -0.1344 0.8275 0.0218
-1.750 0.3705 0.00998 0.00349 -0.1337 0.8248 0.0228
-1.500 0.3954 0.00940 0.00286 -0.1330 0.8222 0.0488
-1.250 0.4176 0.00853 0.00279 -0.1326 0.8199 0.3263
-1.000 0.4277 0.00735 0.00303 -0.1290 0.8176 0.8213
-0.750 0.4448 0.00726 0.00311 -0.1262 0.8146 0.9038
-0.500 0.4687 0.00721 0.00308 -0.1252 0.8117 0.9332
-0.250 0.5193 0.00711 0.00294 -0.1302 0.8099 0.9782
0.000 0.5832 0.00708 0.00283 -0.1383 0.8086 1.0000
0.250 0.6060 0.00713 0.00283 -0.1375 0.8060 1.0000
0.500 0.6295 0.00722 0.00288 -0.1369 0.8036 1.0000
0.750 0.6490 0.00728 0.00297 -0.1354 0.7998 1.0000
1.000 0.6723 0.00733 0.00302 -0.1347 0.7964 1.0000
1.250 0.6979 0.00738 0.00305 -0.1344 0.7936 1.0000
1.500 0.7254 0.00746 0.00310 -0.1345 0.7912 1.0000
1.750 0.7486 0.00753 0.00321 -0.1338 0.7873 1.0000
2.000 0.7737 0.00758 0.00329 -0.1333 0.7834 1.0000
2.250 0.8005 0.00762 0.00339 -0.1333 0.7803 1.0000
2.500 0.8290 0.00769 0.00347 -0.1336 0.7776 1.0000
2.750 0.8518 0.00771 0.00358 -0.1326 0.7719 1.0000
3.000 0.8757 0.00736 0.00322 -0.1314 0.7575 1.0000
3.250 0.8980 0.00705 0.00290 -0.1298 0.7396 1.0000
3.500 0.9142 0.00680 0.00258 -0.1269 0.6976 1.0000
3.750 0.9111 0.00760 0.00268 -0.1199 0.5525 1.0000
4.000 0.8888 0.01001 0.00373 -0.1105 0.2874 1.0000
4.250 0.8719 0.01261 0.00504 -0.1025 0.0239 1.0000
4.500 0.8849 0.01350 0.00608 -0.0995 0.0153 1.0000
4.750 0.8985 0.01428 0.00697 -0.0968 0.0142 1.0000
5.000 0.9167 0.01469 0.00739 -0.0951 0.0118 1.0000
5.250 0.9281 0.01550 0.00829 -0.0920 0.0104 1.0000
5.500 0.9386 0.01646 0.00931 -0.0888 0.0093 1.0000
5.750 0.9478 0.01770 0.01063 -0.0854 0.0086 1.0000
6.000 0.9628 0.01905 0.01207 -0.0831 0.0093 1.0000
7.000 1.1139 0.03781 0.03186 -0.0887 0.0146 1.0000
7.250 1.1280 0.04051 0.03483 -0.0862 0.0146 1.0000
7.500 1.1395 0.04303 0.03764 -0.0834 0.0145 1.0000
7.750 1.1495 0.04534 0.04022 -0.0805 0.0144 1.0000
8.000 1.1671 0.04442 0.03951 -0.0778 0.0133 1.0000
8.250 1.1844 0.04524 0.04054 -0.0755 0.0109 1.0000
8.500 1.1911 0.04765 0.04317 -0.0726 0.0097 1.0000
8.750 1.1944 0.05020 0.04592 -0.0695 0.0091 1.0000
9.000 1.1945 0.05287 0.04878 -0.0662 0.0086 1.0000
9.250 1.1917 0.05538 0.05142 -0.0630 0.0082 1.0000
9.500 1.1863 0.05826 0.05448 -0.0593 0.0080 1.0000
9.750 1.1730 0.06095 0.05730 -0.0548 0.0077 1.0000
10.000 1.1598 0.06363 0.06014 -0.0504 0.0077 1.0000
10.250 1.1409 0.06685 0.06351 -0.0465 0.0075 1.0000
10.500 1.1138 0.07136 0.06817 -0.0430 0.0073 1.0000
10.750 1.0989 0.07454 0.07150 -0.0407 0.0073 1.0000
11.000 1.0817 0.07823 0.07533 -0.0390 0.0073 1.0000
11.250 1.0614 0.08269 0.07992 -0.0380 0.0073 1.0000
11.500 1.0484 0.08640 0.08376 -0.0377 0.0074 1.0000
|
Polar data table (+)
Polar graphs
<< Back to WORTMANN FX 74-080 (fx74080-il)