Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il) Reynolds number: 200,000 Max Cl/Cd: 74.33 at α=2.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-eiffel385-il-200000-n5.txt Download as CSV file: xf-eiffel385-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Eiffel 385 (S.T. Ae)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.500 -0.6700 0.07464 0.06989 -0.0747 1.0000 0.0422
-16.250 -0.7030 0.06726 0.06240 -0.0793 1.0000 0.0423
-16.000 -0.7292 0.06134 0.05640 -0.0825 1.0000 0.0424
-15.750 -0.7550 0.05595 0.05093 -0.0852 1.0000 0.0425
-15.500 -0.7841 0.05084 0.04576 -0.0872 1.0000 0.0426
-15.250 -0.8201 0.04635 0.04126 -0.0875 1.0000 0.0425
-15.000 -0.8562 0.04112 0.03593 -0.0894 1.0000 0.0424
-14.750 -0.8654 0.03680 0.03139 -0.0921 0.9994 0.0427
-14.500 -0.8398 0.03423 0.02875 -0.0962 0.9945 0.0435
-14.250 -0.8141 0.03205 0.02645 -0.0994 0.9890 0.0444
-14.000 -0.7868 0.03017 0.02442 -0.1021 0.9841 0.0454
-13.750 -0.7615 0.02854 0.02265 -0.1037 0.9794 0.0464
-13.500 -0.7365 0.02711 0.02107 -0.1048 0.9743 0.0474
-13.250 -0.7070 0.02579 0.01957 -0.1065 0.9706 0.0485
-13.000 -0.6833 0.02461 0.01830 -0.1068 0.9646 0.0497
-12.750 -0.6552 0.02349 0.01711 -0.1078 0.9598 0.0512
-12.500 -0.6234 0.02246 0.01596 -0.1092 0.9566 0.0534
-12.250 -0.5998 0.02162 0.01499 -0.1088 0.9499 0.0554
-12.000 -0.5705 0.02070 0.01403 -0.1096 0.9454 0.0578
-11.750 -0.5375 0.01986 0.01311 -0.1109 0.9422 0.0613
-11.500 -0.5119 0.01918 0.01237 -0.1106 0.9353 0.0651
-11.250 -0.4805 0.01854 0.01168 -0.1113 0.9302 0.0709
-11.000 -0.4452 0.01801 0.01111 -0.1127 0.9266 0.0783
-10.750 -0.4167 0.01761 0.01065 -0.1126 0.9199 0.0854
-10.500 -0.3850 0.01722 0.01013 -0.1131 0.9138 0.0923
-10.250 -0.3491 0.01680 0.00965 -0.1144 0.9092 0.0985
-10.000 -0.3212 0.01650 0.00917 -0.1141 0.9003 0.1033
-9.750 -0.2880 0.01603 0.00870 -0.1149 0.8938 0.1080
-9.500 -0.2580 0.01570 0.00829 -0.1151 0.8854 0.1129
-9.250 -0.2258 0.01537 0.00782 -0.1156 0.8768 0.1173
-9.000 -0.1966 0.01501 0.00746 -0.1156 0.8668 0.1217
-8.750 -0.1647 0.01470 0.00708 -0.1160 0.8570 0.1265
-8.500 -0.1367 0.01445 0.00675 -0.1157 0.8451 0.1322
-8.250 -0.1069 0.01425 0.00656 -0.1158 0.8334 0.1393
-8.000 -0.0769 0.01405 0.00626 -0.1158 0.8207 0.1454
-7.750 -0.0491 0.01393 0.00612 -0.1154 0.8063 0.1505
-7.500 -0.0209 0.01376 0.00587 -0.1150 0.7921 0.1553
-7.250 0.0072 0.01362 0.00564 -0.1147 0.7777 0.1597
-7.000 0.0352 0.01355 0.00549 -0.1143 0.7635 0.1653
-6.750 0.0631 0.01346 0.00528 -0.1139 0.7499 0.1720
-6.500 0.0902 0.01343 0.00518 -0.1133 0.7364 0.1777
-6.250 0.1175 0.01339 0.00500 -0.1128 0.7240 0.1847
-6.000 0.1446 0.01335 0.00490 -0.1123 0.7129 0.1901
-5.750 0.1716 0.01335 0.00479 -0.1118 0.7023 0.1962
-5.500 0.1986 0.01334 0.00466 -0.1113 0.6927 0.2018
-5.250 0.2253 0.01330 0.00459 -0.1108 0.6837 0.2070
-5.000 0.2522 0.01330 0.00452 -0.1104 0.6753 0.2126
-4.750 0.2792 0.01332 0.00443 -0.1099 0.6669 0.2173
-4.500 0.3056 0.01325 0.00435 -0.1094 0.6586 0.2215
-4.250 0.3319 0.01323 0.00429 -0.1089 0.6497 0.2256
-4.000 0.3585 0.01323 0.00424 -0.1084 0.6415 0.2298
-3.750 0.3850 0.01324 0.00419 -0.1079 0.6336 0.2336
-3.250 0.4379 0.01320 0.00415 -0.1070 0.6202 0.2416
-3.000 0.4644 0.01321 0.00415 -0.1065 0.6136 0.2470
-2.750 0.4912 0.01326 0.00414 -0.1061 0.6077 0.2517
-2.500 0.5173 0.01324 0.00417 -0.1056 0.6009 0.2562
-2.250 0.5434 0.01324 0.00420 -0.1052 0.5944 0.2613
-2.000 0.5698 0.01327 0.00423 -0.1047 0.5884 0.2663
-1.750 0.5957 0.01329 0.00428 -0.1042 0.5813 0.2716
-1.500 0.6216 0.01331 0.00434 -0.1037 0.5748 0.2787
-1.250 0.6474 0.01333 0.00442 -0.1032 0.5680 0.2876
-1.000 0.6729 0.01335 0.00451 -0.1027 0.5607 0.2967
-0.750 0.6987 0.01341 0.00458 -0.1022 0.5543 0.3080
-0.500 0.7238 0.01342 0.00471 -0.1016 0.5461 0.3228
-0.250 0.7490 0.01348 0.00480 -0.1010 0.5385 0.3408
0.000 0.7740 0.01352 0.00493 -0.1004 0.5306 0.3605
0.250 0.7986 0.01358 0.00503 -0.0997 0.5222 0.3798
0.500 0.8231 0.01362 0.00515 -0.0990 0.5133 0.3984
0.750 0.8470 0.01367 0.00524 -0.0982 0.5041 0.4172
1.000 0.8711 0.01371 0.00538 -0.0975 0.4947 0.4384
1.500 0.9476 0.01297 0.00581 -0.1021 0.4709 1.0000
1.750 0.9702 0.01317 0.00597 -0.1011 0.4580 1.0000
2.000 0.9924 0.01340 0.00613 -0.1001 0.4450 1.0000
2.250 1.0140 0.01365 0.00631 -0.0990 0.4319 1.0000
2.500 1.0351 0.01393 0.00652 -0.0978 0.4187 1.0000
2.750 1.0562 0.01421 0.00675 -0.0966 0.4048 1.0000
3.000 1.0768 0.01451 0.00700 -0.0954 0.3915 1.0000
3.250 1.0973 0.01484 0.00728 -0.0941 0.3801 1.0000
3.500 1.1172 0.01518 0.00758 -0.0929 0.3692 1.0000
3.750 1.1373 0.01552 0.00789 -0.0916 0.3576 1.0000
4.000 1.1562 0.01589 0.00822 -0.0902 0.3466 1.0000
4.250 1.1733 0.01631 0.00858 -0.0885 0.3341 1.0000
4.500 1.1909 0.01670 0.00895 -0.0869 0.3210 1.0000
4.750 1.2075 0.01710 0.00933 -0.0851 0.3097 1.0000
5.000 1.2220 0.01755 0.00974 -0.0830 0.2993 1.0000
5.250 1.2377 0.01797 0.01017 -0.0811 0.2883 1.0000
5.500 1.2524 0.01843 0.01062 -0.0791 0.2770 1.0000
5.750 1.2655 0.01896 0.01113 -0.0769 0.2645 1.0000
6.000 1.2790 0.01950 0.01166 -0.0749 0.2525 1.0000
6.250 1.2930 0.02005 0.01223 -0.0730 0.2401 1.0000
6.500 1.3045 0.02071 0.01287 -0.0709 0.2253 1.0000
6.750 1.3141 0.02150 0.01361 -0.0686 0.2079 1.0000
7.000 1.3204 0.02249 0.01452 -0.0661 0.1858 1.0000
7.250 1.3221 0.02381 0.01569 -0.0632 0.1567 1.0000
7.500 1.3195 0.02550 0.01719 -0.0602 0.1282 1.0000
7.750 1.3193 0.02718 0.01877 -0.0576 0.1097 1.0000
8.000 1.3214 0.02881 0.02037 -0.0555 0.0970 1.0000
8.250 1.3247 0.03044 0.02199 -0.0537 0.0879 1.0000
8.500 1.3276 0.03218 0.02373 -0.0521 0.0815 1.0000
8.750 1.3319 0.03388 0.02548 -0.0508 0.0769 1.0000
9.000 1.3348 0.03579 0.02743 -0.0495 0.0735 1.0000
9.250 1.3368 0.03785 0.02955 -0.0485 0.0709 1.0000
9.500 1.3402 0.03988 0.03165 -0.0476 0.0688 1.0000
9.750 1.3426 0.04207 0.03392 -0.0469 0.0670 1.0000
10.000 1.3436 0.04448 0.03640 -0.0463 0.0654 1.0000
10.250 1.3431 0.04712 0.03910 -0.0458 0.0640 1.0000
10.500 1.3411 0.04999 0.04202 -0.0454 0.0627 1.0000
10.750 1.3414 0.05268 0.04480 -0.0451 0.0616 1.0000
11.000 1.3431 0.05526 0.04749 -0.0449 0.0604 1.0000
11.250 1.3440 0.05798 0.05030 -0.0449 0.0591 1.0000
11.500 1.3445 0.06081 0.05321 -0.0449 0.0578 1.0000
11.750 1.3438 0.06382 0.05629 -0.0450 0.0566 1.0000
12.000 1.3420 0.06700 0.05952 -0.0451 0.0553 1.0000
12.250 1.3395 0.07028 0.06282 -0.0453 0.0542 1.0000
12.500 1.3404 0.07321 0.06584 -0.0456 0.0531 1.0000
12.750 1.3428 0.07605 0.06879 -0.0460 0.0520 1.0000
13.000 1.3444 0.07899 0.07183 -0.0464 0.0509 1.0000
13.250 1.3454 0.08205 0.07498 -0.0469 0.0497 1.0000
13.500 1.3466 0.08512 0.07812 -0.0475 0.0487 1.0000
13.750 1.3469 0.08834 0.08140 -0.0481 0.0476 1.0000
14.000 1.3475 0.09143 0.08451 -0.0487 0.0466 1.0000
14.250 1.3492 0.09442 0.08756 -0.0493 0.0457 1.0000
14.500 1.3506 0.09767 0.09096 -0.0502 0.0446 1.0000
14.750 1.3520 0.10089 0.09429 -0.0511 0.0436 1.0000
15.000 1.3527 0.10426 0.09776 -0.0522 0.0425 1.0000
15.250 1.3530 0.10770 0.10128 -0.0534 0.0414 1.0000
15.500 1.3538 0.11100 0.10464 -0.0545 0.0406 1.0000
15.750 1.3549 0.11420 0.10786 -0.0556 0.0397 1.0000
16.000 1.3545 0.11788 0.11167 -0.0571 0.0387 1.0000
16.250 1.3540 0.12160 0.11555 -0.0586 0.0377 1.0000
16.500 1.3532 0.12539 0.11946 -0.0602 0.0367 1.0000
16.750 1.3524 0.12917 0.12334 -0.0620 0.0357 1.0000
17.000 1.3519 0.13291 0.12714 -0.0638 0.0348 1.0000
17.250 1.3517 0.13655 0.13082 -0.0656 0.0341 1.0000
17.500 1.3499 0.14059 0.13499 -0.0677 0.0332 1.0000
17.750 1.3467 0.14497 0.13953 -0.0699 0.0321 1.0000
18.000 1.3446 0.14912 0.14380 -0.0722 0.0312 1.0000
18.250 1.3423 0.15335 0.14813 -0.0746 0.0304 1.0000
18.500 1.3409 0.15741 0.15225 -0.0770 0.0297 1.0000
18.750 1.3400 0.16133 0.15621 -0.0793 0.0291 1.0000
19.000 1.3347 0.16623 0.16127 -0.0822 0.0283 1.0000
19.250 1.3277 0.17159 0.16680 -0.0854 0.0274 1.0000
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