EPPLER 553 AIRFOIL (e553-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: EPPLER 553 AIRFOIL (e553-il) Reynolds number: 1,000,000 Max Cl/Cd: 121.54 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-e553-il-1000000.txt Download as CSV file: xf-e553-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: EPPLER 553 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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.5676 0.16823 0.16630 -0.0243 1.0000 0.0054
-18.750 -0.6558 0.14106 0.13882 -0.0362 1.0000 0.0050
-18.500 -0.6876 0.12975 0.12735 -0.0418 1.0000 0.0049
-18.250 -0.7130 0.12039 0.11784 -0.0464 1.0000 0.0049
-18.000 -0.7324 0.11264 0.10996 -0.0502 1.0000 0.0048
-17.750 -0.7502 0.10543 0.10262 -0.0537 1.0000 0.0048
-17.500 -0.7638 0.09929 0.09637 -0.0566 1.0000 0.0047
-17.250 -0.7805 0.09280 0.08974 -0.0596 1.0000 0.0048
-17.000 -0.7876 0.08809 0.08494 -0.0618 1.0000 0.0047
-16.750 -0.7986 0.08295 0.07968 -0.0640 1.0000 0.0047
-16.500 -0.8070 0.07835 0.07498 -0.0658 1.0000 0.0047
-16.250 -0.8132 0.07419 0.07072 -0.0675 1.0000 0.0047
-16.000 -0.8187 0.07028 0.06673 -0.0689 1.0000 0.0047
-15.750 -0.8236 0.06658 0.06292 -0.0701 1.0000 0.0047
-15.500 -0.8269 0.06318 0.05944 -0.0711 1.0000 0.0047
-15.250 -0.8304 0.05990 0.05608 -0.0719 1.0000 0.0047
-15.000 -0.8320 0.05692 0.05301 -0.0726 1.0000 0.0047
-14.750 -0.8345 0.05397 0.04998 -0.0731 1.0000 0.0048
-14.500 -0.8337 0.05149 0.04744 -0.0734 1.0000 0.0047
-14.250 -0.8352 0.04883 0.04471 -0.0736 1.0000 0.0048
-14.000 -0.8352 0.04650 0.04232 -0.0736 1.0000 0.0048
-13.750 -0.8368 0.04415 0.03990 -0.0733 1.0000 0.0049
-13.500 -0.8386 0.04194 0.03762 -0.0729 1.0000 0.0049
-13.250 -0.8391 0.03993 0.03557 -0.0723 1.0000 0.0049
-13.000 -0.8399 0.03800 0.03359 -0.0715 1.0000 0.0050
-12.750 -0.8418 0.03616 0.03169 -0.0703 1.0000 0.0051
-12.500 -0.8423 0.03423 0.02972 -0.0697 0.9997 0.0050
-12.250 -0.8213 0.03198 0.02739 -0.0733 0.9978 0.0051
-12.000 -0.7976 0.02997 0.02531 -0.0770 0.9950 0.0053
-11.750 -0.7769 0.02789 0.02316 -0.0801 0.9907 0.0052
-11.500 -0.7575 0.02566 0.02085 -0.0834 0.9839 0.0054
-11.250 -0.7508 0.02297 0.01810 -0.0853 0.9658 0.0059
-10.750 -0.6853 0.01955 0.01454 -0.0947 0.9478 0.0063
-10.500 -0.6371 0.01812 0.01303 -0.1019 0.9411 0.0068
-10.250 -0.5898 0.01680 0.01161 -0.1087 0.9283 0.0071
-10.000 -0.5673 0.01549 0.01013 -0.1112 0.9023 0.0077
-9.750 -0.5509 0.01484 0.00935 -0.1105 0.8818 0.0081
-9.500 -0.5346 0.01433 0.00874 -0.1094 0.8655 0.0089
-9.250 -0.5163 0.01392 0.00823 -0.1084 0.8513 0.0095
-9.000 -0.4995 0.01336 0.00760 -0.1072 0.8385 0.0108
-8.750 -0.4792 0.01297 0.00713 -0.1064 0.8271 0.0123
-8.500 -0.4589 0.01253 0.00665 -0.1056 0.8160 0.0151
-8.250 -0.4377 0.01208 0.00618 -0.1050 0.8059 0.0200
-8.000 -0.4153 0.01172 0.00579 -0.1044 0.7964 0.0256
-7.750 -0.3918 0.01137 0.00543 -0.1041 0.7867 0.0323
-7.500 -0.3684 0.01099 0.00506 -0.1037 0.7779 0.0423
-7.250 -0.3443 0.01063 0.00471 -0.1034 0.7690 0.0553
-7.000 -0.3205 0.01019 0.00435 -0.1032 0.7607 0.0773
-6.750 -0.2968 0.00968 0.00395 -0.1030 0.7522 0.1093
-6.500 -0.2734 0.00904 0.00351 -0.1029 0.7442 0.1605
-6.250 -0.2511 0.00813 0.00294 -0.1028 0.7359 0.2468
-6.000 -0.2270 0.00741 0.00256 -0.1029 0.7285 0.3378
-5.750 -0.1994 0.00725 0.00246 -0.1030 0.7207 0.3702
-5.500 -0.1713 0.00720 0.00238 -0.1031 0.7133 0.3867
-5.250 -0.1428 0.00717 0.00232 -0.1032 0.7055 0.3963
-5.000 -0.1145 0.00718 0.00226 -0.1033 0.6983 0.4042
-4.750 -0.0857 0.00716 0.00221 -0.1035 0.6911 0.4120
-4.250 -0.0285 0.00720 0.00214 -0.1038 0.6765 0.4251
-4.000 -0.0003 0.00721 0.00212 -0.1039 0.6691 0.4313
-3.750 0.0289 0.00732 0.00215 -0.1041 0.6625 0.4388
-3.500 0.0571 0.00729 0.00213 -0.1043 0.6551 0.4452
-3.250 0.0856 0.00731 0.00210 -0.1044 0.6483 0.4480
-3.000 0.1144 0.00732 0.00206 -0.1046 0.6411 0.4505
-2.750 0.1426 0.00736 0.00202 -0.1047 0.6343 0.4527
-2.500 0.1716 0.00737 0.00199 -0.1049 0.6276 0.4546
-2.250 0.1996 0.00735 0.00194 -0.1050 0.6205 0.4576
-2.000 0.2283 0.00734 0.00192 -0.1052 0.6142 0.4603
-1.750 0.2567 0.00736 0.00191 -0.1053 0.6073 0.4627
-1.500 0.2850 0.00739 0.00190 -0.1054 0.6007 0.4651
-1.250 0.3137 0.00741 0.00189 -0.1056 0.5941 0.4675
-1.000 0.3417 0.00747 0.00190 -0.1057 0.5875 0.4697
-0.750 0.3705 0.00749 0.00189 -0.1059 0.5814 0.4720
-0.500 0.3986 0.00749 0.00189 -0.1060 0.5748 0.4751
-0.250 0.4266 0.00752 0.00190 -0.1061 0.5687 0.4777
0.000 0.4552 0.00755 0.00192 -0.1063 0.5627 0.4802
0.250 0.4831 0.00761 0.00195 -0.1063 0.5564 0.4828
0.500 0.5115 0.00765 0.00198 -0.1065 0.5505 0.4852
0.750 0.5398 0.00771 0.00201 -0.1066 0.5442 0.4874
1.000 0.5671 0.00776 0.00204 -0.1066 0.5382 0.4908
1.250 0.5957 0.00777 0.00208 -0.1068 0.5328 0.4938
1.500 0.6235 0.00783 0.00212 -0.1068 0.5267 0.4966
1.750 0.6511 0.00790 0.00218 -0.1068 0.5209 0.4993
2.000 0.6794 0.00795 0.00223 -0.1070 0.5153 0.5020
2.250 0.7068 0.00804 0.00229 -0.1069 0.5091 0.5045
2.500 0.7345 0.00808 0.00235 -0.1070 0.5034 0.5083
2.750 0.7622 0.00813 0.00243 -0.1070 0.4972 0.5117
3.000 0.7889 0.00824 0.00251 -0.1069 0.4910 0.5149
3.250 0.8169 0.00829 0.00258 -0.1070 0.4857 0.5180
3.750 0.8707 0.00847 0.00277 -0.1068 0.4741 0.5248
4.000 0.8985 0.00852 0.00286 -0.1069 0.4684 0.5287
4.250 0.9250 0.00863 0.00296 -0.1067 0.4619 0.5327
4.500 0.9517 0.00873 0.00307 -0.1066 0.4557 0.5363
4.750 0.9786 0.00881 0.00317 -0.1065 0.4493 0.5406
5.000 1.0040 0.00895 0.00331 -0.1061 0.4428 0.5450
5.250 1.0313 0.00901 0.00342 -0.1061 0.4370 0.5496
5.500 1.0568 0.00916 0.00356 -0.1058 0.4298 0.5537
5.750 1.0829 0.00925 0.00369 -0.1056 0.4230 0.5592
6.000 1.1084 0.00938 0.00384 -0.1053 0.4157 0.5648
6.250 1.1335 0.00953 0.00400 -0.1049 0.4087 0.5701
6.500 1.1588 0.00964 0.00415 -0.1045 0.4010 0.5761
6.750 1.1831 0.00981 0.00433 -0.1040 0.3932 0.5825
7.000 1.2075 0.00996 0.00450 -0.1035 0.3845 0.5887
7.250 1.2312 0.01013 0.00470 -0.1029 0.3753 0.5960
7.500 1.2535 0.01035 0.00491 -0.1020 0.3652 0.6035
7.750 1.2765 0.01053 0.00513 -0.1012 0.3540 0.6122
8.250 1.3160 0.01104 0.00563 -0.0986 0.3284 0.6304
8.500 1.3326 0.01135 0.00592 -0.0967 0.3130 0.6401
8.750 1.3476 0.01174 0.00627 -0.0945 0.2949 0.6510
9.000 1.3611 0.01220 0.00669 -0.0922 0.2759 0.6627
9.250 1.3730 0.01273 0.00717 -0.0896 0.2567 0.6757
9.500 1.3844 0.01328 0.00768 -0.0870 0.2371 0.6901
9.750 1.3926 0.01395 0.00830 -0.0840 0.2160 0.7069
10.000 1.3995 0.01468 0.00898 -0.0809 0.1963 0.7257
10.250 1.4066 0.01542 0.00971 -0.0780 0.1782 0.7477
10.500 1.4132 0.01619 0.01049 -0.0751 0.1626 0.7749
10.750 1.4193 0.01698 0.01133 -0.0722 0.1491 0.8142
11.000 1.4218 0.01758 0.01220 -0.0687 0.1367 1.0000
11.250 1.4272 0.01866 0.01323 -0.0662 0.1237 1.0000
11.500 1.4320 0.01984 0.01436 -0.0638 0.1119 1.0000
12.000 1.4428 0.02235 0.01681 -0.0597 0.0924 1.0000
12.250 1.4469 0.02379 0.01823 -0.0577 0.0832 1.0000
12.500 1.4496 0.02539 0.01980 -0.0558 0.0746 1.0000
12.750 1.4525 0.02707 0.02145 -0.0542 0.0670 1.0000
13.000 1.4549 0.02885 0.02322 -0.0526 0.0593 1.0000
13.250 1.4570 0.03074 0.02510 -0.0512 0.0530 1.0000
13.500 1.4591 0.03271 0.02708 -0.0499 0.0480 1.0000
13.750 1.4635 0.03457 0.02897 -0.0490 0.0444 1.0000
14.000 1.4637 0.03685 0.03125 -0.0479 0.0396 1.0000
14.250 1.4670 0.03896 0.03339 -0.0472 0.0361 1.0000
14.500 1.4659 0.04154 0.03598 -0.0464 0.0320 1.0000
14.750 1.4696 0.04375 0.03823 -0.0459 0.0298 1.0000
15.000 1.4695 0.04640 0.04091 -0.0455 0.0271 1.0000
15.250 1.4718 0.04890 0.04345 -0.0452 0.0251 1.0000
15.500 1.4729 0.05159 0.04619 -0.0450 0.0232 1.0000
15.750 1.4724 0.05451 0.04915 -0.0449 0.0213 1.0000
16.000 1.4745 0.05723 0.05193 -0.0450 0.0198 1.0000
16.250 1.4740 0.06033 0.05507 -0.0452 0.0184 1.0000
16.500 1.4731 0.06353 0.05833 -0.0455 0.0173 1.0000
16.750 1.4743 0.06655 0.06142 -0.0459 0.0162 1.0000
17.000 1.4736 0.06987 0.06479 -0.0464 0.0152 1.0000
17.250 1.4707 0.07356 0.06853 -0.0470 0.0142 1.0000
17.500 1.4715 0.07681 0.07186 -0.0477 0.0136 1.0000
17.750 1.4705 0.08036 0.07548 -0.0486 0.0128 1.0000
18.000 1.4688 0.08406 0.07924 -0.0495 0.0121 1.0000
18.250 1.4646 0.08819 0.08343 -0.0507 0.0114 1.0000
18.500 1.4634 0.09197 0.08730 -0.0518 0.0109 1.0000
18.750 1.4621 0.09578 0.09118 -0.0531 0.0104 1.0000
19.000 1.4601 0.09973 0.09520 -0.0544 0.0099 1.0000
19.250 1.4557 0.10414 0.09968 -0.0560 0.0094 1.0000
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