EPPLER 858 AIRFOIL (e858-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: EPPLER 858 AIRFOIL (e858-il) Reynolds number: 1,000,000 Max Cl/Cd: 88.05 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-e858-il-1000000.txt Download as CSV file: xf-e858-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: EPPLER 858 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.7399 0.11578 0.11244 -0.0570 1.0000 0.0110
-19.000 -0.7457 0.11151 0.10811 -0.0589 1.0000 0.0112
-18.750 -0.7536 0.10699 0.10353 -0.0608 1.0000 0.0112
-18.500 -0.7604 0.10265 0.09913 -0.0625 1.0000 0.0114
-18.250 -0.7662 0.09866 0.09508 -0.0641 1.0000 0.0113
-18.000 -0.7735 0.09446 0.09082 -0.0657 1.0000 0.0114
-17.750 -0.7809 0.09034 0.08664 -0.0672 1.0000 0.0114
-17.500 -0.7866 0.08654 0.08278 -0.0685 1.0000 0.0116
-17.250 -0.7934 0.08269 0.07887 -0.0697 1.0000 0.0116
-17.000 -0.8005 0.07890 0.07503 -0.0709 1.0000 0.0116
-16.750 -0.8057 0.07544 0.07150 -0.0718 1.0000 0.0117
-16.500 -0.8121 0.07191 0.06791 -0.0728 1.0000 0.0118
-16.250 -0.8168 0.06873 0.06468 -0.0734 1.0000 0.0119
-16.000 -0.8224 0.06553 0.06143 -0.0740 1.0000 0.0119
-15.750 -0.8174 0.06190 0.05772 -0.0772 0.9990 0.0119
-15.500 -0.8093 0.05810 0.05386 -0.0813 0.9972 0.0121
-15.250 -0.8068 0.05386 0.04955 -0.0856 0.9953 0.0124
-15.000 -0.7987 0.05016 0.04578 -0.0900 0.9936 0.0127
-14.750 -0.7855 0.04705 0.04262 -0.0944 0.9924 0.0128
-14.500 -0.7808 0.04407 0.03959 -0.0964 0.9889 0.0130
-14.250 -0.7695 0.04136 0.03682 -0.0993 0.9862 0.0133
-14.000 -0.7514 0.03886 0.03428 -0.1031 0.9839 0.0136
-13.750 -0.7328 0.03622 0.03158 -0.1073 0.9823 0.0139
-13.500 -0.7090 0.03393 0.02924 -0.1117 0.9811 0.0143
-13.250 -0.7065 0.03159 0.02685 -0.1118 0.9745 0.0144
-13.000 -0.6868 0.02941 0.02462 -0.1149 0.9712 0.0147
-12.750 -0.6903 0.02667 0.02183 -0.1150 0.9620 0.0152
-12.500 -0.6933 0.02455 0.01966 -0.1139 0.9469 0.0155
-12.250 -0.6883 0.02243 0.01748 -0.1142 0.9288 0.0159
-12.000 -0.6531 0.02042 0.01540 -0.1194 0.9153 0.0168
-11.750 -0.5844 0.01830 0.01317 -0.1309 0.8980 0.0184
-11.500 -0.4874 0.01677 0.01148 -0.1470 0.8651 0.0215
-11.250 -0.4442 0.01598 0.01042 -0.1523 0.8139 0.0238
-11.000 -0.4516 0.01546 0.00971 -0.1473 0.7767 0.0250
-10.750 -0.4529 0.01508 0.00921 -0.1427 0.7510 0.0268
-10.500 -0.4465 0.01472 0.00874 -0.1394 0.7293 0.0287
-10.250 -0.4367 0.01438 0.00831 -0.1366 0.7103 0.0316
-10.000 -0.4244 0.01405 0.00792 -0.1341 0.6930 0.0347
-9.750 -0.4104 0.01371 0.00754 -0.1318 0.6772 0.0383
-9.500 -0.3953 0.01341 0.00718 -0.1297 0.6633 0.0423
-9.250 -0.3790 0.01311 0.00684 -0.1278 0.6497 0.0466
-9.000 -0.3609 0.01282 0.00652 -0.1261 0.6380 0.0513
-8.500 -0.3228 0.01227 0.00592 -0.1231 0.6146 0.0626
-8.000 -0.2820 0.01176 0.00536 -0.1205 0.5926 0.0775
-7.750 -0.2615 0.01153 0.00511 -0.1191 0.5812 0.0865
-7.500 -0.2392 0.01125 0.00485 -0.1182 0.5728 0.0970
-7.250 -0.2175 0.01099 0.00460 -0.1171 0.5631 0.1090
-7.000 -0.1949 0.01074 0.00437 -0.1162 0.5548 0.1229
-6.750 -0.1720 0.01048 0.00414 -0.1153 0.5462 0.1382
-6.500 -0.1500 0.01022 0.00392 -0.1142 0.5371 0.1576
-6.250 -0.1265 0.00992 0.00368 -0.1135 0.5299 0.1798
-6.000 -0.1043 0.00960 0.00344 -0.1126 0.5213 0.2105
-5.750 -0.0819 0.00926 0.00323 -0.1117 0.5136 0.2497
-5.500 -0.0576 0.00903 0.00310 -0.1110 0.5064 0.2822
-5.250 -0.0329 0.00895 0.00303 -0.1104 0.4985 0.3043
-5.000 -0.0069 0.00889 0.00298 -0.1099 0.4921 0.3189
-4.750 0.0198 0.00888 0.00294 -0.1095 0.4856 0.3289
-4.500 0.0451 0.00888 0.00292 -0.1089 0.4783 0.3390
-4.250 0.0718 0.00891 0.00290 -0.1085 0.4722 0.3463
-4.000 0.0983 0.00889 0.00287 -0.1081 0.4665 0.3541
-3.750 0.1243 0.00893 0.00288 -0.1076 0.4599 0.3614
-3.500 0.1505 0.00901 0.00288 -0.1071 0.4532 0.3664
-3.250 0.1772 0.00899 0.00287 -0.1067 0.4483 0.3730
-3.000 0.2033 0.00903 0.00288 -0.1062 0.4424 0.3785
-2.750 0.2289 0.00912 0.00290 -0.1057 0.4361 0.3830
-2.500 0.2560 0.00918 0.00292 -0.1054 0.4319 0.3863
-2.250 0.2824 0.00918 0.00292 -0.1050 0.4275 0.3918
-2.000 0.3083 0.00923 0.00295 -0.1045 0.4226 0.3968
-1.750 0.3336 0.00934 0.00301 -0.1039 0.4171 0.4013
-1.500 0.3603 0.00942 0.00305 -0.1035 0.4131 0.4055
-1.250 0.3869 0.00946 0.00308 -0.1032 0.4095 0.4104
-1.000 0.4126 0.00950 0.00312 -0.1027 0.4050 0.4154
-0.750 0.4378 0.00959 0.00317 -0.1020 0.4005 0.4189
-0.500 0.4624 0.00971 0.00325 -0.1014 0.3958 0.4222
-0.250 0.4893 0.00975 0.00328 -0.1011 0.3936 0.4250
0.000 0.5156 0.00982 0.00333 -0.1007 0.3906 0.4274
0.250 0.5413 0.00991 0.00338 -0.1002 0.3873 0.4291
0.500 0.5656 0.00995 0.00343 -0.0995 0.3840 0.4340
0.750 0.5892 0.01006 0.00352 -0.0986 0.3800 0.4380
1.000 0.6134 0.01017 0.00362 -0.0979 0.3767 0.4414
1.250 0.6394 0.01023 0.00368 -0.0975 0.3746 0.4446
1.500 0.6649 0.01030 0.00375 -0.0970 0.3722 0.4475
1.750 0.6899 0.01040 0.00382 -0.0964 0.3696 0.4498
2.000 0.7143 0.01050 0.00390 -0.0958 0.3669 0.4525
2.250 0.7377 0.01060 0.00400 -0.0949 0.3641 0.4575
2.500 0.7603 0.01075 0.00414 -0.0940 0.3607 0.4617
2.750 0.7843 0.01087 0.00426 -0.0933 0.3585 0.4654
3.000 0.8097 0.01094 0.00435 -0.0928 0.3570 0.4688
3.250 0.8346 0.01103 0.00445 -0.0923 0.3552 0.4718
3.500 0.8588 0.01114 0.00455 -0.0916 0.3531 0.4742
3.750 0.8819 0.01123 0.00467 -0.0908 0.3509 0.4798
4.000 0.9045 0.01136 0.00480 -0.0899 0.3488 0.4847
4.250 0.9264 0.01151 0.00496 -0.0889 0.3464 0.4892
4.500 0.9476 0.01172 0.00515 -0.0878 0.3437 0.4933
4.750 0.9691 0.01193 0.00535 -0.0867 0.3412 0.4965
5.000 0.9931 0.01201 0.00547 -0.0861 0.3402 0.5024
5.250 1.0164 0.01211 0.00562 -0.0854 0.3389 0.5081
5.500 1.0391 0.01223 0.00577 -0.0846 0.3374 0.5137
5.750 1.0616 0.01238 0.00593 -0.0838 0.3356 0.5186
6.000 1.0834 0.01252 0.00611 -0.0828 0.3338 0.5256
6.250 1.1047 0.01269 0.00631 -0.0818 0.3321 0.5332
6.500 1.1252 0.01289 0.00652 -0.0807 0.3303 0.5400
6.750 1.1441 0.01313 0.00678 -0.0794 0.3282 0.5475
7.000 1.1620 0.01342 0.00708 -0.0779 0.3256 0.5567
7.250 1.1821 0.01366 0.00735 -0.0768 0.3239 0.5657
7.500 1.2036 0.01379 0.00757 -0.0759 0.3229 0.5780
7.750 1.2243 0.01398 0.00780 -0.0749 0.3217 0.5898
8.000 1.2444 0.01416 0.00806 -0.0739 0.3203 0.6054
8.250 1.2644 0.01436 0.00833 -0.0729 0.3190 0.6217
8.500 1.2835 0.01458 0.00862 -0.0717 0.3175 0.6406
8.750 1.3016 0.01482 0.00895 -0.0704 0.3160 0.6637
9.000 1.3187 0.01508 0.00930 -0.0689 0.3143 0.6939
9.250 1.3336 0.01535 0.00970 -0.0672 0.3127 0.7377
9.500 1.3417 0.01548 0.01018 -0.0640 0.3108 0.8559
9.750 1.3883 0.01588 0.01074 -0.0689 0.3076 1.0000
10.000 1.4080 0.01620 0.01108 -0.0681 0.3068 1.0000
10.250 1.4271 0.01655 0.01147 -0.0672 0.3057 1.0000
10.500 1.4461 0.01692 0.01187 -0.0663 0.3046 1.0000
10.750 1.4643 0.01733 0.01231 -0.0654 0.3033 1.0000
11.000 1.4821 0.01777 0.01278 -0.0645 0.3018 1.0000
11.250 1.4997 0.01823 0.01326 -0.0636 0.3003 1.0000
11.500 1.5159 0.01877 0.01381 -0.0625 0.2988 1.0000
11.750 1.5310 0.01938 0.01443 -0.0614 0.2969 1.0000
12.000 1.5448 0.02007 0.01513 -0.0602 0.2950 1.0000
12.250 1.5582 0.02082 0.01588 -0.0590 0.2927 1.0000
12.500 1.5742 0.02145 0.01654 -0.0582 0.2912 1.0000
12.750 1.5904 0.02208 0.01722 -0.0575 0.2902 1.0000
13.000 1.6069 0.02271 0.01790 -0.0568 0.2890 1.0000
13.250 1.6221 0.02344 0.01868 -0.0560 0.2875 1.0000
13.500 1.6374 0.02419 0.01946 -0.0554 0.2859 1.0000
13.750 1.6518 0.02501 0.02032 -0.0547 0.2842 1.0000
14.000 1.6644 0.02596 0.02129 -0.0539 0.2823 1.0000
14.250 1.6747 0.02708 0.02243 -0.0530 0.2800 1.0000
14.500 1.6838 0.02826 0.02361 -0.0520 0.2770 1.0000
14.750 1.6965 0.02929 0.02469 -0.0515 0.2753 1.0000
15.000 1.7096 0.03036 0.02582 -0.0511 0.2737 1.0000
15.250 1.7221 0.03147 0.02700 -0.0506 0.2717 1.0000
15.500 1.7334 0.03269 0.02826 -0.0502 0.2696 1.0000
15.750 1.7423 0.03410 0.02971 -0.0497 0.2672 1.0000
16.000 1.7488 0.03570 0.03133 -0.0491 0.2650 1.0000
16.250 1.7524 0.03751 0.03315 -0.0483 0.2619 1.0000
16.500 1.7619 0.03894 0.03464 -0.0480 0.2602 1.0000
16.750 1.7703 0.04053 0.03631 -0.0477 0.2582 1.0000
17.000 1.7784 0.04213 0.03798 -0.0474 0.2559 1.0000
17.250 1.7826 0.04406 0.03996 -0.0471 0.2535 1.0000
17.500 1.7835 0.04629 0.04221 -0.0466 0.2505 1.0000
17.750 1.7800 0.04889 0.04481 -0.0460 0.2471 1.0000
18.000 1.7853 0.05080 0.04681 -0.0458 0.2452 1.0000
18.250 1.7882 0.05296 0.04905 -0.0457 0.2429 1.0000
18.500 1.7888 0.05531 0.05146 -0.0454 0.2399 1.0000
18.750 1.7832 0.05826 0.05444 -0.0451 0.2366 1.0000
19.000 1.7722 0.06172 0.05791 -0.0447 0.2329 1.0000
19.250 1.7737 0.06408 0.06036 -0.0447 0.2303 1.0000
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