Eiffel 371 (Monge) (eiffel371-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Eiffel 371 (Monge) (eiffel371-il) Reynolds number: 1,000,000 Max Cl/Cd: 80.69 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-eiffel371-il-1000000-n5.txt Download as CSV file: xf-eiffel371-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Eiffel 371 (Monge)
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
------ -------- --------- --------- -------- -------- --------
-14.750 -0.8500 0.04921 0.04663 -0.0845 1.0000 0.0049
-14.500 -0.8770 0.04231 0.03953 -0.0893 1.0000 0.0048
-14.250 -0.8967 0.03853 0.03559 -0.0889 1.0000 0.0049
-14.000 -0.9122 0.03577 0.03269 -0.0869 1.0000 0.0049
-13.750 -0.9183 0.03407 0.03090 -0.0845 1.0000 0.0050
-13.500 -0.9377 0.03190 0.02858 -0.0804 1.0000 0.0049
-13.250 -0.9278 0.02967 0.02616 -0.0808 0.9981 0.0050
-13.000 -0.9071 0.02854 0.02495 -0.0811 0.9956 0.0051
-12.750 -0.8954 0.02680 0.02303 -0.0805 0.9913 0.0051
-12.500 -0.8775 0.02543 0.02152 -0.0802 0.9870 0.0051
-12.250 -0.8586 0.02426 0.02022 -0.0796 0.9825 0.0052
-12.000 -0.8435 0.02295 0.01875 -0.0783 0.9766 0.0053
-11.750 -0.8190 0.02203 0.01773 -0.0783 0.9739 0.0053
-11.500 -0.8031 0.02066 0.01620 -0.0770 0.9671 0.0055
-11.250 -0.7768 0.01952 0.01494 -0.0774 0.9630 0.0056
-11.000 -0.7468 0.01859 0.01392 -0.0784 0.9596 0.0057
-10.750 -0.7202 0.01776 0.01300 -0.0785 0.9538 0.0058
-10.500 -0.6889 0.01720 0.01238 -0.0794 0.9496 0.0060
-10.250 -0.6575 0.01655 0.01165 -0.0803 0.9453 0.0062
-10.000 -0.6306 0.01592 0.01095 -0.0802 0.9379 0.0063
-9.750 -0.6003 0.01537 0.01031 -0.0808 0.9309 0.0064
-9.500 -0.5751 0.01484 0.00971 -0.0804 0.9220 0.0066
-9.000 -0.5262 0.01392 0.00861 -0.0789 0.9046 0.0069
-8.750 -0.5025 0.01349 0.00809 -0.0780 0.8960 0.0071
-8.500 -0.4803 0.01313 0.00766 -0.0767 0.8862 0.0072
-8.250 -0.4573 0.01280 0.00726 -0.0755 0.8763 0.0074
-8.000 -0.4352 0.01246 0.00683 -0.0742 0.8639 0.0076
-7.750 -0.4145 0.01205 0.00632 -0.0726 0.8487 0.0080
-7.500 -0.3929 0.01178 0.00598 -0.0711 0.8299 0.0083
-7.250 -0.3718 0.01158 0.00568 -0.0695 0.8037 0.0086
-7.000 -0.3521 0.01145 0.00540 -0.0676 0.7709 0.0089
-6.750 -0.3323 0.01134 0.00514 -0.0657 0.7395 0.0094
-6.500 -0.3112 0.01125 0.00492 -0.0641 0.7142 0.0099
-6.250 -0.2896 0.01110 0.00467 -0.0626 0.6930 0.0101
-6.000 -0.2681 0.01090 0.00438 -0.0612 0.6738 0.0109
-5.750 -0.2457 0.01074 0.00415 -0.0599 0.6570 0.0114
-5.500 -0.2227 0.01060 0.00394 -0.0587 0.6418 0.0121
-5.250 -0.1992 0.01048 0.00375 -0.0576 0.6294 0.0129
-5.000 -0.1755 0.01037 0.00357 -0.0566 0.6168 0.0136
-4.750 -0.1521 0.01022 0.00338 -0.0555 0.6038 0.0153
-4.500 -0.1284 0.01012 0.00322 -0.0545 0.5902 0.0170
-4.250 -0.1045 0.01002 0.00307 -0.0535 0.5777 0.0188
-4.000 -0.0807 0.00992 0.00293 -0.0525 0.5666 0.0218
-3.750 -0.0562 0.00981 0.00280 -0.0517 0.5563 0.0255
-3.500 -0.0319 0.00972 0.00268 -0.0509 0.5477 0.0297
-3.250 -0.0073 0.00959 0.00256 -0.0501 0.5404 0.0374
-2.750 0.0410 0.00931 0.00237 -0.0484 0.5287 0.0716
-2.500 0.0657 0.00920 0.00229 -0.0477 0.5225 0.0860
-2.000 0.1133 0.00891 0.00215 -0.0460 0.5116 0.1429
-1.750 0.1354 0.00867 0.00207 -0.0448 0.5058 0.1960
-1.250 0.1712 0.00790 0.00193 -0.0409 0.4953 0.3982
-1.000 0.1925 0.00770 0.00189 -0.0396 0.4898 0.4493
-0.750 0.2163 0.00765 0.00197 -0.0387 0.4826 0.5060
-0.500 0.2434 0.00770 0.00199 -0.0386 0.4757 0.5226
-0.250 0.2696 0.00779 0.00200 -0.0382 0.4635 0.5303
0.000 0.2958 0.00786 0.00203 -0.0379 0.4523 0.5374
0.250 0.3225 0.00794 0.00205 -0.0376 0.4415 0.5427
0.500 0.3485 0.00801 0.00207 -0.0373 0.4316 0.5478
0.750 0.3743 0.00811 0.00211 -0.0369 0.4187 0.5523
1.000 0.4000 0.00824 0.00215 -0.0366 0.4029 0.5567
1.250 0.4249 0.00838 0.00220 -0.0361 0.3844 0.5594
1.500 0.4493 0.00851 0.00224 -0.0355 0.3684 0.5607
1.750 0.4738 0.00864 0.00230 -0.0350 0.3532 0.5620
2.250 0.5234 0.00889 0.00244 -0.0340 0.3294 0.5650
2.500 0.5482 0.00902 0.00251 -0.0336 0.3198 0.5666
2.750 0.5724 0.00918 0.00260 -0.0331 0.3076 0.5683
3.000 0.5972 0.00930 0.00269 -0.0327 0.2976 0.5695
3.250 0.6217 0.00944 0.00278 -0.0323 0.2894 0.5704
3.500 0.6468 0.00954 0.00285 -0.0320 0.2828 0.5712
3.750 0.6711 0.00969 0.00296 -0.0315 0.2750 0.5721
4.000 0.6957 0.00979 0.00305 -0.0311 0.2685 0.5734
4.250 0.7190 0.00994 0.00315 -0.0305 0.2591 0.5749
4.500 0.7430 0.01005 0.00326 -0.0301 0.2522 0.5760
4.750 0.7665 0.01019 0.00337 -0.0295 0.2448 0.5771
5.000 0.7900 0.01032 0.00349 -0.0290 0.2384 0.5784
5.250 0.8131 0.01047 0.00362 -0.0284 0.2308 0.5800
5.500 0.8355 0.01065 0.00376 -0.0277 0.2221 0.5815
5.750 0.8575 0.01083 0.00391 -0.0270 0.2133 0.5830
6.000 0.8790 0.01100 0.00407 -0.0261 0.2058 0.5841
6.250 0.8984 0.01121 0.00423 -0.0249 0.1960 0.5848
6.500 0.9183 0.01138 0.00439 -0.0237 0.1881 0.5854
6.750 0.9366 0.01163 0.00459 -0.0223 0.1773 0.5860
7.250 0.9697 0.01227 0.00512 -0.0189 0.1504 0.5875
7.500 0.9875 0.01255 0.00538 -0.0174 0.1421 0.5885
7.750 1.0036 0.01290 0.00569 -0.0158 0.1324 0.5894
8.000 1.0200 0.01324 0.00600 -0.0142 0.1253 0.5905
8.250 1.0375 0.01354 0.00630 -0.0128 0.1198 0.5914
8.500 1.0561 0.01379 0.00657 -0.0117 0.1177 0.5926
8.750 1.0729 0.01410 0.00688 -0.0103 0.1141 0.5938
9.000 1.0889 0.01446 0.00724 -0.0087 0.1092 0.5952
9.250 1.1067 0.01474 0.00755 -0.0076 0.1072 0.5968
9.500 1.1242 0.01503 0.00787 -0.0064 0.1037 0.5983
9.750 1.1403 0.01539 0.00823 -0.0051 0.1001 0.5997
10.250 1.1701 0.01620 0.00907 -0.0022 0.0913 0.6042
10.500 1.1682 0.01733 0.00999 0.0017 0.0631 0.6067
11.000 1.1526 0.02036 0.01281 0.0104 0.0165 0.6130
11.250 1.1611 0.02101 0.01362 0.0123 0.0136 0.6530
11.500 1.1690 0.02186 0.01463 0.0141 0.0119 0.7311
11.750 1.1775 0.02280 0.01563 0.0157 0.0102 0.7345
12.000 1.1875 0.02369 0.01658 0.0169 0.0097 0.7372
12.250 1.1961 0.02471 0.01764 0.0182 0.0089 0.7398
12.500 1.2032 0.02588 0.01885 0.0194 0.0081 0.7413
12.750 1.2104 0.02710 0.02012 0.0205 0.0077 0.7426
13.000 1.2182 0.02834 0.02141 0.0214 0.0073 0.7436
13.250 1.2245 0.02974 0.02287 0.0222 0.0070 0.7445
13.500 1.2301 0.03125 0.02445 0.0230 0.0067 0.7454
13.750 1.2353 0.03287 0.02612 0.0236 0.0064 0.7463
14.000 1.2379 0.03477 0.02809 0.0242 0.0059 0.7472
14.250 1.2398 0.03681 0.03020 0.0247 0.0057 0.7481
14.500 1.2451 0.03862 0.03207 0.0249 0.0053 0.7489
14.750 1.2474 0.04076 0.03429 0.0250 0.0053 0.7496
15.000 1.2488 0.04305 0.03666 0.0251 0.0051 0.7504
15.250 1.2490 0.04554 0.03922 0.0250 0.0050 0.7509
15.500 1.2509 0.04791 0.04165 0.0248 0.0048 0.7515
15.750 1.2477 0.05090 0.04472 0.0246 0.0046 0.7522
16.000 1.2491 0.05342 0.04731 0.0242 0.0046 0.7527
16.250 1.2435 0.05683 0.05081 0.0237 0.0044 0.7532
16.500 1.2379 0.06034 0.05439 0.0230 0.0041 0.7536
16.750 1.2363 0.06346 0.05760 0.0222 0.0041 0.7540
17.000 1.2291 0.06735 0.06158 0.0213 0.0039 0.7543
17.250 1.2225 0.07129 0.06561 0.0202 0.0040 0.7547
17.500 1.2191 0.07492 0.06932 0.0190 0.0038 0.7550
17.750 1.2080 0.07968 0.07420 0.0175 0.0039 0.7552
18.000 1.1988 0.08432 0.07893 0.0159 0.0038 0.7554
18.250 1.1935 0.08847 0.08317 0.0144 0.0036 0.7558
18.500 1.1817 0.09373 0.08853 0.0124 0.0037 0.7559
18.750 1.1688 0.09923 0.09414 0.0103 0.0037 0.7561
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