EPPLER 552 AIRFOIL (e552-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: EPPLER 552 AIRFOIL (e552-il) Reynolds number: 1,000,000 Max Cl/Cd: 119.87 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-e552-il-1000000-n5.txt Download as CSV file: xf-e552-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: EPPLER 552 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7652 0.14351 0.14096 -0.0222 1.0000 0.0032
-19.500 -0.7854 0.13516 0.13250 -0.0264 1.0000 0.0032
-19.250 -0.8073 0.12662 0.12384 -0.0307 1.0000 0.0032
-19.000 -0.8272 0.11875 0.11586 -0.0347 1.0000 0.0032
-18.750 -0.8433 0.11180 0.10880 -0.0382 1.0000 0.0032
-18.500 -0.8626 0.10441 0.10129 -0.0418 1.0000 0.0032
-18.250 -0.8721 0.09894 0.09573 -0.0445 1.0000 0.0032
-18.000 -0.8898 0.09226 0.08893 -0.0477 1.0000 0.0032
-17.750 -0.9052 0.08618 0.08273 -0.0506 1.0000 0.0031
-17.500 -0.9078 0.08222 0.07869 -0.0524 1.0000 0.0032
-17.250 -0.9201 0.07696 0.07333 -0.0547 1.0000 0.0032
-17.000 -0.9260 0.07276 0.06904 -0.0564 1.0000 0.0032
-16.750 -0.9298 0.06898 0.06518 -0.0580 1.0000 0.0032
-16.500 -0.9342 0.06522 0.06133 -0.0594 1.0000 0.0032
-16.250 -0.9355 0.06195 0.05799 -0.0605 1.0000 0.0032
-16.000 -0.9353 0.05898 0.05495 -0.0614 1.0000 0.0033
-15.750 -0.9368 0.05586 0.05175 -0.0624 1.0000 0.0033
-15.500 -0.9385 0.05281 0.04863 -0.0632 1.0000 0.0033
-15.250 -0.9365 0.05028 0.04603 -0.0638 1.0000 0.0033
-15.000 -0.9352 0.04776 0.04344 -0.0642 1.0000 0.0033
-14.750 -0.9342 0.04529 0.04090 -0.0646 1.0000 0.0033
-14.500 -0.9308 0.04319 0.03875 -0.0647 1.0000 0.0033
-14.250 -0.9293 0.04100 0.03650 -0.0648 1.0000 0.0033
-14.000 -0.9242 0.03919 0.03463 -0.0646 1.0000 0.0034
-13.750 -0.9175 0.03688 0.03226 -0.0658 0.9995 0.0034
-13.500 -0.9005 0.03457 0.02988 -0.0687 0.9968 0.0035
-13.000 -0.8323 0.02982 0.02493 -0.0810 0.9321 0.0036
-12.750 -0.7372 0.02745 0.02215 -0.0993 0.8492 0.0037
-12.500 -0.7318 0.02627 0.02073 -0.0983 0.7997 0.0039
-12.250 -0.7247 0.02515 0.01944 -0.0973 0.7673 0.0039
-12.000 -0.7171 0.02400 0.01816 -0.0964 0.7433 0.0040
-11.750 -0.7092 0.02284 0.01690 -0.0955 0.7243 0.0042
-11.500 -0.7003 0.02174 0.01570 -0.0947 0.7088 0.0042
-11.250 -0.6900 0.02075 0.01463 -0.0938 0.6950 0.0043
-11.000 -0.6808 0.01972 0.01351 -0.0928 0.6825 0.0044
-10.750 -0.6710 0.01879 0.01251 -0.0918 0.6705 0.0044
-10.500 -0.6643 0.01780 0.01143 -0.0903 0.6598 0.0045
-10.250 -0.6620 0.01701 0.01056 -0.0877 0.6498 0.0046
-10.000 -0.6490 0.01646 0.00993 -0.0862 0.6392 0.0048
-9.750 -0.6328 0.01595 0.00935 -0.0851 0.6297 0.0049
-9.500 -0.6142 0.01554 0.00886 -0.0842 0.6206 0.0051
-9.250 -0.5955 0.01504 0.00831 -0.0833 0.6128 0.0055
-8.750 -0.5530 0.01426 0.00744 -0.0821 0.5982 0.0064
-8.500 -0.5302 0.01393 0.00705 -0.0816 0.5909 0.0069
-8.250 -0.5073 0.01356 0.00665 -0.0812 0.5849 0.0079
-8.000 -0.4834 0.01324 0.00629 -0.0809 0.5783 0.0088
-7.750 -0.4593 0.01293 0.00594 -0.0806 0.5722 0.0105
-7.500 -0.4344 0.01263 0.00561 -0.0804 0.5662 0.0124
-7.250 -0.4093 0.01235 0.00531 -0.0802 0.5598 0.0154
-7.000 -0.3839 0.01207 0.00502 -0.0801 0.5546 0.0192
-6.750 -0.3579 0.01181 0.00474 -0.0800 0.5495 0.0238
-6.500 -0.3319 0.01155 0.00447 -0.0800 0.5445 0.0293
-6.250 -0.3058 0.01127 0.00421 -0.0799 0.5401 0.0374
-6.000 -0.2795 0.01096 0.00395 -0.0800 0.5361 0.0507
-5.750 -0.2534 0.01061 0.00367 -0.0800 0.5318 0.0714
-5.500 -0.2275 0.01021 0.00337 -0.0801 0.5275 0.1028
-5.250 -0.2018 0.00971 0.00305 -0.0802 0.5238 0.1491
-5.000 -0.1765 0.00902 0.00265 -0.0804 0.5201 0.2233
-4.750 -0.1511 0.00830 0.00224 -0.0806 0.5161 0.3107
-4.500 -0.1238 0.00796 0.00208 -0.0808 0.5125 0.3675
-4.250 -0.0954 0.00787 0.00202 -0.0810 0.5092 0.3909
-4.000 -0.0663 0.00781 0.00198 -0.0813 0.5065 0.4087
-3.750 -0.0372 0.00780 0.00194 -0.0816 0.5036 0.4178
-3.500 -0.0081 0.00778 0.00191 -0.0818 0.5006 0.4272
-3.250 0.0208 0.00779 0.00191 -0.0820 0.4976 0.4391
-3.000 0.0498 0.00783 0.00191 -0.0822 0.4945 0.4468
-2.750 0.0791 0.00784 0.00187 -0.0825 0.4920 0.4486
-2.500 0.1082 0.00782 0.00184 -0.0828 0.4894 0.4506
-2.250 0.1374 0.00781 0.00181 -0.0830 0.4869 0.4524
-2.000 0.1665 0.00782 0.00180 -0.0833 0.4844 0.4543
-1.750 0.1954 0.00784 0.00178 -0.0835 0.4820 0.4564
-1.500 0.2244 0.00786 0.00178 -0.0837 0.4795 0.4584
-1.250 0.2534 0.00789 0.00177 -0.0840 0.4774 0.4601
-1.000 0.2826 0.00790 0.00177 -0.0842 0.4754 0.4617
-0.750 0.3118 0.00792 0.00177 -0.0845 0.4731 0.4631
-0.500 0.3409 0.00793 0.00177 -0.0848 0.4708 0.4648
-0.250 0.3698 0.00794 0.00178 -0.0850 0.4687 0.4670
0.000 0.3987 0.00797 0.00180 -0.0852 0.4667 0.4692
0.250 0.4274 0.00801 0.00183 -0.0854 0.4644 0.4713
0.500 0.4561 0.00805 0.00186 -0.0856 0.4621 0.4734
0.750 0.4852 0.00807 0.00189 -0.0859 0.4604 0.4753
1.000 0.5142 0.00810 0.00192 -0.0862 0.4587 0.4772
1.250 0.5432 0.00813 0.00195 -0.0864 0.4567 0.4789
1.500 0.5720 0.00817 0.00199 -0.0867 0.4544 0.4809
1.750 0.6006 0.00820 0.00204 -0.0869 0.4522 0.4832
2.000 0.6291 0.00825 0.00209 -0.0871 0.4499 0.4858
2.250 0.6575 0.00831 0.00215 -0.0872 0.4476 0.4884
2.500 0.6862 0.00836 0.00221 -0.0874 0.4457 0.4910
2.750 0.7150 0.00839 0.00227 -0.0877 0.4437 0.4932
3.000 0.7437 0.00844 0.00233 -0.0879 0.4412 0.4953
3.250 0.7721 0.00848 0.00240 -0.0881 0.4382 0.4978
3.500 0.8003 0.00854 0.00247 -0.0882 0.4350 0.5005
3.750 0.8280 0.00863 0.00256 -0.0883 0.4315 0.5033
4.000 0.8567 0.00867 0.00264 -0.0885 0.4292 0.5062
4.250 0.8851 0.00872 0.00272 -0.0887 0.4263 0.5092
4.750 0.9407 0.00886 0.00290 -0.0889 0.4185 0.5155
5.000 0.9685 0.00894 0.00301 -0.0890 0.4144 0.5191
5.250 0.9966 0.00900 0.00311 -0.0891 0.4103 0.5225
5.500 1.0241 0.00909 0.00321 -0.0892 0.4055 0.5259
5.750 1.0510 0.00920 0.00334 -0.0892 0.4007 0.5291
6.000 1.0787 0.00927 0.00345 -0.0893 0.3951 0.5330
6.250 1.1053 0.00939 0.00359 -0.0892 0.3879 0.5372
6.500 1.1321 0.00951 0.00373 -0.0891 0.3805 0.5413
6.750 1.1577 0.00969 0.00389 -0.0889 0.3704 0.5453
7.000 1.1831 0.00987 0.00408 -0.0886 0.3580 0.5505
7.250 1.2073 0.01011 0.00430 -0.0881 0.3433 0.5559
7.750 1.2514 0.01083 0.00490 -0.0865 0.3041 0.5660
8.000 1.2710 0.01130 0.00529 -0.0854 0.2828 0.5716
8.250 1.2902 0.01178 0.00569 -0.0841 0.2616 0.5769
8.500 1.3067 0.01235 0.00618 -0.0825 0.2389 0.5827
8.750 1.3227 0.01291 0.00666 -0.0807 0.2173 0.5891
9.000 1.3360 0.01354 0.00719 -0.0785 0.1960 0.5952
9.250 1.3462 0.01411 0.00771 -0.0758 0.1777 0.6027
9.750 1.3640 0.01530 0.00883 -0.0699 0.1489 0.6184
10.000 1.3723 0.01595 0.00946 -0.0670 0.1371 0.6267
10.250 1.3781 0.01672 0.01021 -0.0640 0.1246 0.6356
10.500 1.3852 0.01747 0.01097 -0.0613 0.1149 0.6447
10.750 1.3884 0.01844 0.01194 -0.0584 0.1040 0.6549
11.000 1.3908 0.01956 0.01307 -0.0556 0.0946 0.6656
11.250 1.3917 0.02088 0.01441 -0.0531 0.0859 0.6771
11.500 1.3967 0.02211 0.01569 -0.0512 0.0801 0.6916
12.000 1.3963 0.02560 0.01928 -0.0474 0.0653 0.7274
12.250 1.3946 0.02765 0.02139 -0.0459 0.0574 0.7492
12.500 1.3949 0.02965 0.02348 -0.0446 0.0528 0.7774
12.750 1.3972 0.03147 0.02545 -0.0434 0.0492 0.8213
13.000 1.3959 0.03364 0.02792 -0.0426 0.0439 1.0000
13.250 1.3974 0.03589 0.03021 -0.0419 0.0401 1.0000
13.500 1.3956 0.03849 0.03282 -0.0413 0.0361 1.0000
13.750 1.3965 0.04089 0.03525 -0.0408 0.0330 1.0000
14.000 1.3943 0.04366 0.03804 -0.0404 0.0294 1.0000
14.250 1.3956 0.04617 0.04059 -0.0402 0.0270 1.0000
14.500 1.3991 0.04852 0.04299 -0.0401 0.0262 1.0000
14.750 1.3977 0.05143 0.04592 -0.0401 0.0233 1.0000
15.000 1.3999 0.05404 0.04857 -0.0401 0.0216 1.0000
15.250 1.3997 0.05696 0.05152 -0.0403 0.0196 1.0000
15.500 1.4011 0.05977 0.05438 -0.0405 0.0180 1.0000
15.750 1.4040 0.06246 0.05711 -0.0408 0.0169 1.0000
16.000 1.4043 0.06552 0.06021 -0.0412 0.0156 1.0000
16.250 1.4047 0.06859 0.06332 -0.0417 0.0136 1.0000
16.500 1.4073 0.07146 0.06624 -0.0422 0.0130 1.0000
16.750 1.4072 0.07472 0.06954 -0.0429 0.0118 1.0000
17.000 1.4096 0.07770 0.07258 -0.0435 0.0109 1.0000
17.250 1.4100 0.08100 0.07592 -0.0443 0.0099 1.0000
17.500 1.4104 0.08432 0.07928 -0.0452 0.0088 1.0000
17.750 1.4115 0.08764 0.08266 -0.0461 0.0082 1.0000
18.000 1.4111 0.09118 0.08624 -0.0472 0.0073 1.0000
18.250 1.4110 0.09475 0.08988 -0.0483 0.0068 1.0000
18.500 1.4115 0.09823 0.09342 -0.0495 0.0061 1.0000
18.750 1.4100 0.10209 0.09733 -0.0508 0.0056 1.0000
19.000 1.4102 0.10570 0.10100 -0.0521 0.0052 1.0000
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