Eiffel 428 (Bleriot) (eiffel428-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: Eiffel 428 (Bleriot) (eiffel428-il) Reynolds number: 500,000 Max Cl/Cd: 67.99 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-eiffel428-il-500000-n5.txt Download as CSV file: xf-eiffel428-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.3930 0.11826 0.11590 -0.0263 1.0000 0.0093
-12.000 -0.3938 0.11352 0.11117 -0.0279 1.0000 0.0099
-11.750 -0.3973 0.10821 0.10587 -0.0298 1.0000 0.0102
-11.500 -0.3946 0.10486 0.10255 -0.0310 1.0000 0.0106
-11.250 -0.3899 0.10209 0.09979 -0.0319 1.0000 0.0108
-11.000 -0.3804 0.10058 0.09830 -0.0324 1.0000 0.0113
-10.750 -0.3758 0.09726 0.09499 -0.0340 0.9995 0.0118
-10.500 -0.3673 0.09262 0.09036 -0.0377 0.9609 0.0123
-10.250 -0.3440 0.08058 0.07824 -0.0548 0.9297 0.0138
-10.000 -0.2969 0.07524 0.07273 -0.0683 0.9015 0.0146
-9.750 -0.2760 0.07214 0.06926 -0.0736 0.8210 0.0152
-9.500 -0.2764 0.06928 0.06637 -0.0747 0.8059 0.0157
-9.250 -0.2843 0.06631 0.06329 -0.0751 0.7753 0.0163
-8.750 -0.3288 0.04218 0.03893 -0.0942 0.7719 0.0189
-8.250 -0.2936 0.03915 0.03558 -0.0947 0.7358 0.0197
-8.000 -0.2777 0.03631 0.03250 -0.0953 0.7209 0.0206
-7.750 -0.2858 0.02319 0.01825 -0.0959 0.7228 0.0244
-7.500 -0.2657 0.02197 0.01677 -0.0953 0.7085 0.0251
-7.250 -0.2417 0.02183 0.01652 -0.0948 0.6928 0.0256
-7.000 -0.2183 0.02153 0.01605 -0.0942 0.6741 0.0261
-6.750 -0.1957 0.02076 0.01506 -0.0935 0.6545 0.0267
-6.500 -0.1733 0.02006 0.01409 -0.0928 0.6252 0.0275
-6.250 -0.1514 0.01911 0.01280 -0.0919 0.5910 0.0285
-6.000 -0.1304 0.01796 0.01120 -0.0908 0.5432 0.0292
-5.750 -0.1109 0.01733 0.00996 -0.0894 0.4455 0.0298
-5.500 -0.0947 0.01758 0.00932 -0.0876 0.2206 0.0304
-5.250 -0.0703 0.01723 0.00871 -0.0870 0.1816 0.0311
-4.750 -0.0210 0.01612 0.00718 -0.0859 0.1158 0.0318
-4.500 0.0037 0.01527 0.00620 -0.0854 0.1141 0.0326
-4.250 0.0293 0.01486 0.00571 -0.0850 0.1128 0.0331
-4.000 0.0551 0.01452 0.00532 -0.0845 0.1117 0.0335
-3.750 0.0809 0.01424 0.00499 -0.0841 0.1108 0.0340
-3.500 0.1067 0.01397 0.00467 -0.0837 0.1100 0.0345
-3.250 0.1325 0.01373 0.00437 -0.0833 0.1092 0.0350
-3.000 0.1582 0.01352 0.00413 -0.0828 0.1084 0.0356
-2.750 0.1841 0.01337 0.00395 -0.0824 0.1078 0.0365
-2.500 0.2099 0.01322 0.00376 -0.0820 0.1072 0.0374
-2.250 0.2356 0.01306 0.00357 -0.0815 0.1068 0.0382
-2.000 0.2613 0.01294 0.00342 -0.0811 0.1062 0.0390
-1.750 0.2870 0.01285 0.00331 -0.0806 0.1058 0.0397
-1.500 0.3128 0.01281 0.00324 -0.0802 0.1054 0.0404
-1.250 0.3380 0.01266 0.00309 -0.0797 0.1050 0.0420
-1.000 0.3636 0.01262 0.00305 -0.0793 0.1047 0.0438
-0.750 0.3892 0.01263 0.00305 -0.0788 0.1045 0.0456
-0.500 0.4149 0.01266 0.00308 -0.0784 0.1043 0.0476
-0.250 0.4407 0.01268 0.00308 -0.0780 0.1040 0.0498
0.000 0.4667 0.01271 0.00310 -0.0777 0.1032 0.0518
0.250 0.4924 0.01271 0.00309 -0.0773 0.1023 0.0576
0.500 0.5182 0.01274 0.00313 -0.0769 0.1007 0.0628
0.750 0.5437 0.01277 0.00319 -0.0765 0.0992 0.0765
1.000 0.5673 0.01251 0.00333 -0.0759 0.0982 0.2389
1.250 0.5858 0.01176 0.00352 -0.0745 0.0972 0.5914
1.750 0.6823 0.01137 0.00395 -0.0841 0.0934 1.0000
2.000 0.7083 0.01140 0.00396 -0.0837 0.0912 1.0000
2.250 0.7340 0.01146 0.00398 -0.0834 0.0866 1.0000
2.500 0.7593 0.01155 0.00402 -0.0829 0.0622 1.0000
2.750 0.7819 0.01188 0.00420 -0.0820 0.0492 1.0000
3.000 0.8052 0.01214 0.00446 -0.0812 0.0462 1.0000
3.250 0.8287 0.01238 0.00471 -0.0805 0.0448 1.0000
3.500 0.8518 0.01265 0.00500 -0.0797 0.0432 1.0000
3.750 0.8746 0.01293 0.00530 -0.0788 0.0417 1.0000
4.000 0.8971 0.01325 0.00563 -0.0779 0.0402 1.0000
4.250 0.9188 0.01361 0.00602 -0.0769 0.0383 1.0000
4.500 0.9412 0.01391 0.00635 -0.0760 0.0373 1.0000
4.750 0.9636 0.01420 0.00668 -0.0751 0.0365 1.0000
5.000 0.9858 0.01450 0.00700 -0.0742 0.0350 1.0000
5.250 1.0073 0.01484 0.00737 -0.0732 0.0335 1.0000
5.500 1.0286 0.01519 0.00774 -0.0722 0.0320 1.0000
5.750 1.0483 0.01563 0.00820 -0.0710 0.0304 1.0000
6.000 1.0667 0.01615 0.00875 -0.0695 0.0290 1.0000
6.250 1.0882 0.01643 0.00907 -0.0686 0.0279 1.0000
6.500 1.1084 0.01679 0.00946 -0.0675 0.0262 1.0000
6.750 1.1284 0.01714 0.00986 -0.0663 0.0245 1.0000
7.000 1.1479 0.01750 0.01022 -0.0651 0.0227 1.0000
7.250 1.1655 0.01796 0.01071 -0.0636 0.0212 1.0000
7.500 1.1825 0.01838 0.01117 -0.0620 0.0197 1.0000
7.750 1.1982 0.01881 0.01163 -0.0601 0.0182 1.0000
8.000 1.2139 0.01923 0.01207 -0.0583 0.0167 1.0000
8.250 1.2261 0.01986 0.01273 -0.0560 0.0154 1.0000
8.500 1.2400 0.02042 0.01335 -0.0541 0.0143 1.0000
8.750 1.2528 0.02108 0.01405 -0.0521 0.0133 1.0000
9.000 1.2652 0.02178 0.01479 -0.0503 0.0125 1.0000
9.250 1.2758 0.02265 0.01569 -0.0483 0.0116 1.0000
9.500 1.2833 0.02377 0.01688 -0.0461 0.0111 1.0000
9.750 1.2927 0.02482 0.01802 -0.0443 0.0106 1.0000
10.000 1.3015 0.02598 0.01929 -0.0426 0.0102 1.0000
10.250 1.3115 0.02710 0.02048 -0.0412 0.0096 1.0000
10.500 1.3211 0.02829 0.02174 -0.0399 0.0091 1.0000
10.750 1.3306 0.02954 0.02304 -0.0388 0.0086 1.0000
11.000 1.3368 0.03113 0.02471 -0.0374 0.0084 1.0000
11.250 1.3393 0.03312 0.02678 -0.0361 0.0080 1.0000
11.500 1.3438 0.03498 0.02874 -0.0349 0.0078 1.0000
11.750 1.3489 0.03685 0.03072 -0.0339 0.0077 1.0000
12.000 1.3543 0.03871 0.03270 -0.0331 0.0074 1.0000
12.250 1.3568 0.04090 0.03501 -0.0321 0.0073 1.0000
12.500 1.3606 0.04300 0.03721 -0.0314 0.0070 1.0000
12.750 1.3635 0.04523 0.03955 -0.0307 0.0068 1.0000
13.000 1.3661 0.04753 0.04195 -0.0301 0.0066 1.0000
13.250 1.3689 0.04983 0.04435 -0.0297 0.0065 1.0000
13.500 1.3718 0.05218 0.04679 -0.0294 0.0063 1.0000
13.750 1.3727 0.05483 0.04954 -0.0292 0.0061 1.0000
14.000 1.3713 0.05783 0.05265 -0.0291 0.0060 1.0000
14.250 1.3713 0.06075 0.05565 -0.0292 0.0058 1.0000
14.500 1.3677 0.06418 0.05922 -0.0293 0.0058 1.0000
14.750 1.3635 0.06785 0.06297 -0.0298 0.0056 1.0000
15.000 1.3566 0.07194 0.06721 -0.0303 0.0055 1.0000
15.250 1.3527 0.07576 0.07118 -0.0310 0.0055 1.0000
15.500 1.3491 0.07965 0.07523 -0.0318 0.0053 1.0000
15.750 1.3436 0.08393 0.07966 -0.0329 0.0053 1.0000
16.000 1.3356 0.08872 0.08460 -0.0342 0.0052 1.0000
16.250 1.3253 0.09403 0.09008 -0.0359 0.0052 1.0000
16.500 1.3154 0.09946 0.09567 -0.0378 0.0051 1.0000
16.750 1.3026 0.10554 0.10191 -0.0402 0.0051 1.0000
17.000 1.2892 0.11195 0.10850 -0.0430 0.0050 1.0000
17.250 1.2752 0.11874 0.11545 -0.0461 0.0050 1.0000
17.500 1.2600 0.12606 0.12293 -0.0497 0.0050 1.0000
17.750 1.2432 0.13406 0.13110 -0.0540 0.0049 1.0000
18.000 1.2220 0.14355 0.14077 -0.0592 0.0049 1.0000
18.250 1.1989 0.15404 0.15143 -0.0652 0.0051 1.0000
18.500 1.1693 0.16702 0.16460 -0.0728 0.0051 1.0000
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