Eiffel 428 (Bleriot) (eiffel428-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Eiffel 428 (Bleriot) (eiffel428-il) Reynolds number: 1,000,000 Max Cl/Cd: 84.03 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-eiffel428-il-1000000-n5.txt Download as CSV file: xf-eiffel428-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Eiffel 428 (Bleriot)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.000 -0.3292 0.09341 0.09087 -0.0648 0.7878 0.0094
-11.750 -0.3497 0.08434 0.08203 -0.0699 0.8331 0.0105
-11.250 -0.6926 0.01988 0.01648 -0.0927 0.9555 0.0103
-11.000 -0.6378 0.01646 0.01260 -0.1010 0.9118 0.0124
-10.750 -0.6142 0.01557 0.01143 -0.1006 0.8759 0.0136
-10.500 -0.5921 0.01513 0.01080 -0.0996 0.8445 0.0147
-10.250 -0.5678 0.01510 0.01069 -0.0989 0.8175 0.0160
-10.000 -0.5439 0.01488 0.01033 -0.0981 0.7961 0.0172
-9.750 -0.5217 0.01451 0.00973 -0.0971 0.7642 0.0181
-9.500 -0.4980 0.01413 0.00917 -0.0964 0.7448 0.0187
-9.250 -0.4719 0.01420 0.00920 -0.0959 0.7282 0.0195
-9.000 -0.4451 0.01441 0.00937 -0.0956 0.7141 0.0201
-8.750 -0.4187 0.01451 0.00942 -0.0952 0.6993 0.0207
-8.500 -0.3927 0.01456 0.00938 -0.0947 0.6816 0.0213
-8.250 -0.3668 0.01461 0.00932 -0.0943 0.6608 0.0220
-8.000 -0.3421 0.01441 0.00895 -0.0937 0.6343 0.0227
-7.750 -0.3179 0.01409 0.00842 -0.0930 0.6056 0.0232
-7.500 -0.2940 0.01408 0.00815 -0.0923 0.5511 0.0237
-7.250 -0.2755 0.01462 0.00799 -0.0907 0.3706 0.0241
-7.000 -0.2551 0.01514 0.00791 -0.0894 0.1522 0.0243
-6.750 -0.2292 0.01506 0.00772 -0.0890 0.1130 0.0244
-6.500 -0.2062 0.01399 0.00645 -0.0883 0.1091 0.0255
-6.250 -0.1804 0.01367 0.00606 -0.0879 0.1066 0.0260
-6.000 -0.1543 0.01344 0.00575 -0.0875 0.1050 0.0264
-5.750 -0.1278 0.01329 0.00556 -0.0872 0.1042 0.0268
-5.500 -0.1014 0.01315 0.00537 -0.0869 0.1038 0.0274
-5.250 -0.0752 0.01291 0.00506 -0.0865 0.1034 0.0278
-5.000 -0.0492 0.01263 0.00472 -0.0861 0.1030 0.0283
-4.750 -0.0231 0.01239 0.00441 -0.0858 0.1025 0.0287
-4.500 0.0030 0.01217 0.00414 -0.0854 0.1020 0.0291
-4.250 0.0291 0.01196 0.00388 -0.0850 0.1016 0.0295
-4.000 0.0551 0.01175 0.00362 -0.0846 0.1011 0.0298
-3.750 0.0813 0.01158 0.00340 -0.0842 0.1007 0.0301
-3.500 0.1074 0.01142 0.00319 -0.0838 0.1003 0.0304
-3.250 0.1335 0.01128 0.00301 -0.0834 0.0998 0.0307
-3.000 0.1598 0.01117 0.00287 -0.0831 0.0993 0.0310
-2.750 0.1860 0.01108 0.00275 -0.0827 0.0990 0.0312
-2.500 0.2124 0.01104 0.00268 -0.0824 0.0985 0.0315
-2.250 0.2384 0.01091 0.00251 -0.0820 0.0983 0.0325
-2.000 0.2645 0.01082 0.00240 -0.0816 0.0979 0.0337
-1.750 0.2908 0.01080 0.00236 -0.0812 0.0976 0.0347
-1.500 0.3171 0.01080 0.00236 -0.0809 0.0974 0.0358
-1.250 0.3435 0.01081 0.00236 -0.0806 0.0970 0.0371
-1.000 0.3697 0.01084 0.00238 -0.0803 0.0966 0.0384
-0.750 0.3958 0.01088 0.00241 -0.0799 0.0957 0.0394
-0.500 0.4214 0.01099 0.00252 -0.0795 0.0940 0.0402
-0.250 0.4479 0.01098 0.00248 -0.0792 0.0936 0.0422
0.000 0.4744 0.01096 0.00247 -0.0790 0.0933 0.0452
0.250 0.5009 0.01097 0.00248 -0.0787 0.0928 0.0478
0.500 0.5274 0.01100 0.00250 -0.0785 0.0922 0.0502
0.750 0.5538 0.01104 0.00253 -0.0782 0.0913 0.0530
1.000 0.5801 0.01105 0.00256 -0.0780 0.0901 0.0606
1.250 0.6062 0.01103 0.00259 -0.0777 0.0884 0.0905
1.500 0.6311 0.01082 0.00263 -0.0773 0.0855 0.2263
1.750 0.6552 0.01059 0.00273 -0.0767 0.0821 0.3665
2.250 0.7506 0.00976 0.00326 -0.0867 0.0424 1.0000
2.500 0.7748 0.00996 0.00344 -0.0860 0.0399 1.0000
2.750 0.7989 0.01016 0.00365 -0.0853 0.0378 1.0000
3.000 0.8233 0.01033 0.00381 -0.0847 0.0373 1.0000
3.250 0.8476 0.01052 0.00399 -0.0841 0.0367 1.0000
3.500 0.8717 0.01071 0.00419 -0.0834 0.0359 1.0000
3.750 0.8957 0.01091 0.00439 -0.0828 0.0349 1.0000
4.000 0.9194 0.01112 0.00459 -0.0821 0.0336 1.0000
4.250 0.9428 0.01136 0.00483 -0.0813 0.0325 1.0000
4.500 0.9657 0.01163 0.00510 -0.0805 0.0309 1.0000
4.750 0.9878 0.01195 0.00544 -0.0796 0.0292 1.0000
5.000 1.0111 0.01217 0.00566 -0.0788 0.0288 1.0000
5.250 1.0343 0.01240 0.00590 -0.0781 0.0281 1.0000
5.500 1.0573 0.01263 0.00614 -0.0774 0.0269 1.0000
5.750 1.0801 0.01286 0.00638 -0.0766 0.0255 1.0000
6.000 1.1025 0.01312 0.00663 -0.0758 0.0239 1.0000
6.250 1.1240 0.01344 0.00694 -0.0748 0.0221 1.0000
6.500 1.1458 0.01372 0.00725 -0.0739 0.0213 1.0000
6.750 1.1676 0.01399 0.00754 -0.0730 0.0198 1.0000
7.000 1.1890 0.01428 0.00780 -0.0721 0.0174 1.0000
7.250 1.2093 0.01462 0.00813 -0.0710 0.0153 1.0000
7.500 1.2290 0.01498 0.00850 -0.0698 0.0138 1.0000
7.750 1.2480 0.01538 0.00890 -0.0685 0.0123 1.0000
8.000 1.2659 0.01582 0.00936 -0.0670 0.0111 1.0000
8.250 1.2837 0.01624 0.00982 -0.0655 0.0104 1.0000
8.500 1.2992 0.01669 0.01030 -0.0636 0.0097 1.0000
8.750 1.3125 0.01718 0.01081 -0.0613 0.0090 1.0000
9.000 1.3252 0.01772 0.01137 -0.0590 0.0082 1.0000
9.250 1.3380 0.01830 0.01200 -0.0568 0.0078 1.0000
9.500 1.3515 0.01888 0.01264 -0.0549 0.0075 1.0000
9.750 1.3642 0.01952 0.01334 -0.0530 0.0072 1.0000
10.000 1.3765 0.02023 0.01410 -0.0511 0.0069 1.0000
10.250 1.3886 0.02099 0.01491 -0.0494 0.0065 1.0000
10.500 1.3996 0.02186 0.01582 -0.0476 0.0062 1.0000
10.750 1.4100 0.02283 0.01684 -0.0460 0.0059 1.0000
11.000 1.4190 0.02396 0.01803 -0.0444 0.0057 1.0000
11.250 1.4266 0.02526 0.01942 -0.0428 0.0055 1.0000
11.500 1.4383 0.02628 0.02050 -0.0417 0.0053 1.0000
11.750 1.4468 0.02760 0.02190 -0.0405 0.0052 1.0000
12.000 1.4559 0.02893 0.02330 -0.0394 0.0050 1.0000
12.250 1.4640 0.03038 0.02482 -0.0384 0.0048 1.0000
12.500 1.4699 0.03208 0.02661 -0.0374 0.0047 1.0000
12.750 1.4778 0.03363 0.02822 -0.0366 0.0045 1.0000
13.000 1.4837 0.03540 0.03006 -0.0358 0.0044 1.0000
13.250 1.4894 0.03721 0.03194 -0.0350 0.0043 1.0000
13.500 1.4939 0.03917 0.03398 -0.0344 0.0042 1.0000
13.750 1.4964 0.04138 0.03627 -0.0337 0.0041 1.0000
14.000 1.4969 0.04381 0.03879 -0.0330 0.0040 1.0000
14.250 1.4965 0.04640 0.04147 -0.0325 0.0038 1.0000
14.500 1.4948 0.04921 0.04438 -0.0321 0.0038 1.0000
14.750 1.4936 0.05203 0.04729 -0.0318 0.0037 1.0000
15.000 1.4916 0.05503 0.05040 -0.0317 0.0037 1.0000
15.250 1.4898 0.05810 0.05358 -0.0317 0.0037 1.0000
15.500 1.4902 0.06095 0.05653 -0.0318 0.0036 1.0000
15.750 1.4879 0.06420 0.05988 -0.0320 0.0035 1.0000
16.000 1.4845 0.06772 0.06350 -0.0324 0.0035 1.0000
16.250 1.4784 0.07167 0.06757 -0.0330 0.0035 1.0000
16.500 1.4741 0.07543 0.07145 -0.0337 0.0034 1.0000
16.750 1.4664 0.07980 0.07593 -0.0346 0.0034 1.0000
17.000 1.4592 0.08418 0.08043 -0.0356 0.0034 1.0000
17.250 1.4522 0.08863 0.08498 -0.0368 0.0033 1.0000
17.500 1.4435 0.09339 0.08985 -0.0382 0.0033 1.0000
17.750 1.4344 0.09833 0.09491 -0.0398 0.0032 1.0000
18.000 1.4217 0.10403 0.10073 -0.0418 0.0032 1.0000
18.250 1.4066 0.11024 0.10708 -0.0441 0.0033 1.0000
18.500 1.3969 0.11563 0.11258 -0.0463 0.0032 1.0000
18.750 1.3825 0.12209 0.11916 -0.0491 0.0032 1.0000
19.000 1.3674 0.12892 0.12612 -0.0523 0.0031 1.0000
19.250 1.3509 0.13630 0.13364 -0.0560 0.0032 1.0000
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