AS5045 (15%) (as5045-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: AS5045 (15%) (as5045-il) Reynolds number: 200,000 Max Cl/Cd: 59.55 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-as5045-il-200000.txt Download as CSV file: xf-as5045-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: AS5045 (15%)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.500 -0.4649 0.09252 0.08951 -0.0415 1.0000 0.0663
-11.250 -0.4963 0.08413 0.08107 -0.0465 1.0000 0.0663
-11.000 -0.5253 0.07710 0.07398 -0.0500 1.0000 0.0662
-10.750 -0.5521 0.07103 0.06784 -0.0525 1.0000 0.0662
-7.750 -0.6004 0.03157 0.02412 -0.0511 0.8488 0.0364
-7.500 -0.5747 0.02867 0.02101 -0.0506 0.8454 0.0338
-7.250 -0.5476 0.02693 0.01879 -0.0497 0.8418 0.0313
-7.000 -0.5208 0.02594 0.01764 -0.0494 0.8384 0.0309
-6.750 -0.4940 0.02458 0.01620 -0.0490 0.8355 0.0308
-6.500 -0.4681 0.02321 0.01482 -0.0484 0.8330 0.0310
-6.250 -0.4443 0.02189 0.01355 -0.0476 0.8306 0.0315
-6.000 -0.4214 0.02081 0.01255 -0.0471 0.8276 0.0324
-5.750 -0.3984 0.01994 0.01170 -0.0469 0.8244 0.0337
-5.500 -0.3745 0.01923 0.01098 -0.0468 0.8215 0.0361
-5.250 -0.3511 0.01836 0.01008 -0.0469 0.8190 0.0393
-5.000 -0.3263 0.01765 0.00932 -0.0472 0.8166 0.0435
-4.750 -0.3007 0.01688 0.00848 -0.0475 0.8142 0.0527
-4.500 -0.2862 0.01327 0.00764 -0.0489 0.8112 0.5589
-4.250 -0.2578 0.01447 0.00880 -0.0479 0.8086 0.6187
-4.000 -0.2328 0.01597 0.01035 -0.0454 0.8060 0.6422
-3.750 -0.2112 0.01795 0.01240 -0.0412 0.8032 0.6666
-3.500 -0.1870 0.01882 0.01324 -0.0389 0.8007 0.6762
-3.250 -0.1597 0.01895 0.01325 -0.0388 0.7984 0.6829
-3.000 -0.1336 0.01922 0.01350 -0.0380 0.7955 0.6876
-2.750 -0.1038 0.01912 0.01329 -0.0392 0.7923 0.6968
-2.500 -0.0790 0.01933 0.01348 -0.0379 0.7893 0.7000
-2.250 -0.0525 0.01944 0.01352 -0.0375 0.7863 0.7047
-2.000 -0.0216 0.01929 0.01322 -0.0391 0.7835 0.7123
-1.750 0.0036 0.01936 0.01330 -0.0383 0.7801 0.7149
-1.500 0.0299 0.01942 0.01336 -0.0380 0.7762 0.7184
-1.250 0.0585 0.01937 0.01325 -0.0386 0.7725 0.7234
-1.000 0.0887 0.01924 0.01302 -0.0397 0.7691 0.7285
-0.750 0.1140 0.01930 0.01308 -0.0391 0.7655 0.7310
-0.500 0.1407 0.01931 0.01311 -0.0391 0.7606 0.7341
-0.250 0.1691 0.01927 0.01303 -0.0395 0.7562 0.7379
0.000 0.2007 0.01918 0.01284 -0.0409 0.7524 0.7426
0.250 0.2271 0.01916 0.01285 -0.0408 0.7472 0.7452
0.500 0.2532 0.01914 0.01285 -0.0405 0.7417 0.7477
0.750 0.2808 0.01908 0.01276 -0.0404 0.7372 0.7505
1.000 0.3091 0.01908 0.01277 -0.0409 0.7315 0.7536
1.250 0.3394 0.01897 0.01265 -0.0418 0.7253 0.7567
1.500 0.3707 0.01883 0.01243 -0.0427 0.7206 0.7595
1.750 0.3964 0.01878 0.01246 -0.0425 0.7134 0.7615
2.000 0.4240 0.01862 0.01231 -0.0423 0.7073 0.7635
2.250 0.4523 0.01850 0.01218 -0.0423 0.7014 0.7655
2.500 0.4807 0.01834 0.01206 -0.0425 0.6932 0.7680
2.750 0.5112 0.01809 0.01176 -0.0428 0.6880 0.7707
3.000 0.5408 0.01794 0.01168 -0.0436 0.6784 0.7732
3.250 0.5725 0.01760 0.01129 -0.0442 0.6725 0.7751
3.500 0.5991 0.01738 0.01118 -0.0440 0.6627 0.7769
3.750 0.6281 0.01700 0.01079 -0.0438 0.6563 0.7790
4.000 0.6555 0.01674 0.01064 -0.0438 0.6453 0.7812
4.250 0.6848 0.01638 0.01033 -0.0439 0.6358 0.7833
4.500 0.7149 0.01593 0.00990 -0.0441 0.6255 0.7854
4.750 0.7445 0.01554 0.00958 -0.0445 0.6112 0.7877
5.000 0.7748 0.01516 0.00924 -0.0449 0.5948 0.7902
5.250 0.8021 0.01485 0.00902 -0.0447 0.5723 0.7922
5.500 0.8290 0.01460 0.00874 -0.0443 0.5458 0.7941
5.750 0.8548 0.01454 0.00858 -0.0439 0.5093 0.7961
6.000 0.8789 0.01476 0.00859 -0.0433 0.4664 0.7983
6.250 0.9016 0.01523 0.00883 -0.0427 0.4220 0.8007
6.500 0.9235 0.01583 0.00922 -0.0422 0.3781 0.8035
6.750 0.9459 0.01648 0.00968 -0.0419 0.3371 0.8060
7.000 0.9660 0.01712 0.01017 -0.0411 0.3017 0.8080
7.250 0.9858 0.01777 0.01072 -0.0403 0.2707 0.8102
7.500 1.0057 0.01845 0.01131 -0.0396 0.2433 0.8125
7.750 1.0248 0.01921 0.01195 -0.0388 0.2195 0.8153
8.000 1.0450 0.01991 0.01261 -0.0382 0.1976 0.8184
8.250 1.0643 0.02072 0.01334 -0.0376 0.1786 0.8215
8.500 1.0813 0.02152 0.01409 -0.0366 0.1623 0.8241
8.750 1.0975 0.02233 0.01488 -0.0354 0.1478 0.8268
9.000 1.1137 0.02316 0.01572 -0.0343 0.1349 0.8299
9.250 1.1292 0.02406 0.01665 -0.0332 0.1236 0.8333
9.500 1.1416 0.02510 0.01765 -0.0318 0.1143 0.8369
9.750 1.1527 0.02603 0.01861 -0.0300 0.1063 0.8406
10.000 1.1651 0.02711 0.01977 -0.0287 0.0990 0.8449
10.250 1.1772 0.02831 0.02096 -0.0276 0.0927 0.8495
10.500 1.1909 0.02957 0.02232 -0.0267 0.0873 0.8541
10.750 1.2030 0.03072 0.02355 -0.0257 0.0825 0.8588
11.000 1.2145 0.03223 0.02503 -0.0246 0.0781 0.8643
11.250 1.2278 0.03344 0.02642 -0.0239 0.0743 0.8705
11.500 1.2391 0.03470 0.02777 -0.0229 0.0710 0.8777
11.750 1.2531 0.03627 0.02925 -0.0216 0.0673 0.8857
12.000 1.2616 0.03755 0.03082 -0.0204 0.0650 0.8982
12.250 1.2676 0.03879 0.03226 -0.0185 0.0626 0.9216
12.500 1.2745 0.04006 0.03364 -0.0172 0.0603 1.0000
12.750 1.2907 0.04178 0.03530 -0.0171 0.0577 1.0000
13.000 1.3030 0.04385 0.03752 -0.0169 0.0556 1.0000
13.250 1.3110 0.04590 0.03976 -0.0168 0.0536 1.0000
13.500 1.3188 0.04797 0.04195 -0.0166 0.0517 1.0000
13.750 1.3272 0.04992 0.04395 -0.0165 0.0500 1.0000
14.000 1.3402 0.05212 0.04611 -0.0158 0.0479 1.0000
14.250 1.3385 0.05499 0.04922 -0.0155 0.0468 1.0000
14.500 1.3357 0.05794 0.05241 -0.0154 0.0456 1.0000
14.750 1.3330 0.06099 0.05565 -0.0153 0.0444 1.0000
15.000 1.3299 0.06409 0.05891 -0.0154 0.0432 1.0000
15.250 1.3284 0.06699 0.06190 -0.0157 0.0420 1.0000
15.500 1.3315 0.06947 0.06438 -0.0158 0.0408 1.0000
15.750 1.3281 0.07348 0.06846 -0.0156 0.0395 1.0000
16.000 1.3121 0.07818 0.07343 -0.0168 0.0391 1.0000
16.250 1.2946 0.08350 0.07901 -0.0186 0.0387 1.0000
16.500 1.2759 0.08950 0.08527 -0.0210 0.0383 1.0000
16.750 1.2552 0.09626 0.09227 -0.0241 0.0380 1.0000
17.000 1.2315 0.10401 0.10028 -0.0281 0.0378 1.0000
17.250 1.2039 0.11310 0.10961 -0.0334 0.0378 1.0000
17.500 1.1699 0.12414 0.12090 -0.0403 0.0381 1.0000
17.750 1.1277 0.13794 0.13493 -0.0494 0.0388 1.0000
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Polar data table (+)
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