ONERA HOR20 AIRFOIL (hor20-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: ONERA HOR20 AIRFOIL (hor20-il) Reynolds number: 1,000,000 Max Cl/Cd: 99.86 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hor20-il-1000000-n5.txt Download as CSV file: xf-hor20-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: ONERA HOR20 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
------ -------- --------- --------- -------- -------- --------
-17.500 -1.1288 0.08405 0.08018 -0.0367 1.0000 0.0438
-17.250 -1.1471 0.07822 0.07427 -0.0397 1.0000 0.0445
-17.000 -1.1675 0.07217 0.06813 -0.0429 1.0000 0.0453
-16.750 -1.1884 0.06620 0.06209 -0.0460 1.0000 0.0462
-16.500 -1.2085 0.06049 0.05628 -0.0490 1.0000 0.0472
-16.250 -1.2304 0.05483 0.05053 -0.0520 1.0000 0.0479
-16.000 -1.2529 0.04920 0.04479 -0.0549 1.0000 0.0486
-15.750 -1.2737 0.04384 0.03932 -0.0578 1.0000 0.0491
-15.500 -1.2942 0.03848 0.03386 -0.0608 1.0000 0.0496
-15.250 -1.3148 0.03286 0.02812 -0.0645 1.0000 0.0501
-15.000 -1.3304 0.02621 0.02131 -0.0716 1.0000 0.0508
-14.750 -1.3179 0.02382 0.01882 -0.0741 1.0000 0.0520
-14.500 -1.3003 0.02262 0.01756 -0.0746 1.0000 0.0532
-14.250 -1.2728 0.02169 0.01656 -0.0763 0.9653 0.0542
-14.000 -1.2514 0.02074 0.01554 -0.0767 0.9437 0.0554
-13.750 -1.2312 0.02000 0.01473 -0.0764 0.9190 0.0565
-13.500 -1.2102 0.01942 0.01404 -0.0759 0.8913 0.0577
-13.250 -1.1876 0.01892 0.01342 -0.0755 0.8642 0.0588
-13.000 -1.1643 0.01839 0.01278 -0.0753 0.8404 0.0600
-12.750 -1.1400 0.01786 0.01217 -0.0752 0.8209 0.0614
-12.500 -1.1147 0.01742 0.01165 -0.0751 0.8042 0.0628
-12.000 -1.0622 0.01661 0.01070 -0.0752 0.7771 0.0653
-11.500 -1.0083 0.01584 0.00983 -0.0753 0.7538 0.0685
-11.250 -0.9807 0.01552 0.00945 -0.0754 0.7423 0.0699
-11.000 -0.9530 0.01517 0.00906 -0.0755 0.7328 0.0715
-10.750 -0.9251 0.01483 0.00868 -0.0757 0.7217 0.0734
-10.500 -0.8968 0.01456 0.00835 -0.0758 0.7114 0.0752
-10.250 -0.8682 0.01428 0.00804 -0.0759 0.7025 0.0769
-10.000 -0.8398 0.01397 0.00769 -0.0761 0.6922 0.0791
-9.750 -0.8109 0.01371 0.00740 -0.0763 0.6831 0.0813
-9.500 -0.7817 0.01350 0.00713 -0.0765 0.6725 0.0830
-9.250 -0.7528 0.01323 0.00683 -0.0766 0.6631 0.0851
-9.000 -0.7235 0.01299 0.00656 -0.0769 0.6551 0.0875
-8.750 -0.6940 0.01280 0.00632 -0.0771 0.6452 0.0898
-8.500 -0.6647 0.01255 0.00605 -0.0773 0.6362 0.0928
-8.250 -0.6350 0.01234 0.00582 -0.0775 0.6261 0.0957
-8.000 -0.6053 0.01219 0.00561 -0.0777 0.6163 0.0980
-7.750 -0.5755 0.01196 0.00538 -0.0780 0.6081 0.1009
-7.500 -0.5456 0.01180 0.00518 -0.0782 0.5974 0.1037
-7.250 -0.5155 0.01166 0.00499 -0.0785 0.5879 0.1063
-7.000 -0.4855 0.01147 0.00479 -0.0788 0.5780 0.1096
-6.750 -0.4554 0.01135 0.00462 -0.0790 0.5687 0.1129
-6.500 -0.4252 0.01119 0.00445 -0.0793 0.5595 0.1166
-6.250 -0.3950 0.01105 0.00428 -0.0796 0.5493 0.1215
-6.000 -0.3647 0.01090 0.00413 -0.0798 0.5418 0.1263
-5.750 -0.3343 0.01076 0.00398 -0.0801 0.5338 0.1313
-5.500 -0.3040 0.01067 0.00385 -0.0804 0.5252 0.1355
-5.250 -0.2734 0.01054 0.00372 -0.0807 0.5188 0.1404
-5.000 -0.2429 0.01046 0.00362 -0.0810 0.5120 0.1444
-4.750 -0.2124 0.01036 0.00350 -0.0813 0.5058 0.1494
-4.500 -0.1817 0.01027 0.00341 -0.0816 0.5012 0.1541
-4.250 -0.1510 0.01017 0.00331 -0.0819 0.4969 0.1589
-4.000 -0.1204 0.01008 0.00322 -0.0822 0.4916 0.1645
-3.750 -0.0897 0.01003 0.00315 -0.0824 0.4859 0.1694
-3.500 -0.0591 0.00994 0.00308 -0.0827 0.4808 0.1765
-3.250 -0.0282 0.00987 0.00301 -0.0830 0.4774 0.1819
-3.000 0.0026 0.00979 0.00295 -0.0833 0.4726 0.1881
-2.750 0.0333 0.00975 0.00290 -0.0836 0.4665 0.1942
-2.500 0.0639 0.00972 0.00286 -0.0839 0.4598 0.2009
-2.250 0.0947 0.00967 0.00282 -0.0842 0.4550 0.2071
-2.000 0.1255 0.00965 0.00279 -0.0845 0.4489 0.2116
-1.750 0.1561 0.00963 0.00277 -0.0847 0.4427 0.2183
-1.500 0.1869 0.00962 0.00275 -0.0850 0.4376 0.2239
-1.250 0.2177 0.00960 0.00273 -0.0853 0.4328 0.2286
-1.000 0.2483 0.00958 0.00272 -0.0856 0.4271 0.2349
-0.750 0.2789 0.00960 0.00272 -0.0858 0.4218 0.2400
-0.500 0.3096 0.00962 0.00272 -0.0861 0.4174 0.2436
-0.250 0.3403 0.00960 0.00271 -0.0863 0.4130 0.2486
0.000 0.3709 0.00960 0.00272 -0.0866 0.4075 0.2539
0.250 0.4014 0.00964 0.00274 -0.0868 0.4020 0.2588
0.500 0.4319 0.00967 0.00276 -0.0870 0.3977 0.2622
0.750 0.4625 0.00967 0.00277 -0.0873 0.3934 0.2682
1.000 0.4930 0.00968 0.00279 -0.0875 0.3880 0.2742
1.250 0.5232 0.00974 0.00283 -0.0877 0.3824 0.2792
1.500 0.5536 0.00977 0.00287 -0.0880 0.3782 0.2851
1.750 0.5841 0.00978 0.00290 -0.0882 0.3744 0.2932
2.250 0.6444 0.00986 0.00302 -0.0886 0.3637 0.3140
2.500 0.6744 0.00991 0.00308 -0.0888 0.3584 0.3253
2.750 0.7046 0.00995 0.00315 -0.0890 0.3532 0.3391
3.000 0.7344 0.01002 0.00324 -0.0891 0.3470 0.3503
3.250 0.7641 0.01013 0.00333 -0.0893 0.3412 0.3602
3.500 0.7940 0.01019 0.00341 -0.0894 0.3361 0.3682
3.750 0.8237 0.01028 0.00352 -0.0896 0.3302 0.3783
4.000 0.8530 0.01042 0.00363 -0.0896 0.3242 0.3853
4.250 0.8827 0.01049 0.00373 -0.0898 0.3203 0.3927
4.500 0.9123 0.01059 0.00384 -0.0899 0.3155 0.4006
4.750 0.9414 0.01073 0.00397 -0.0899 0.3098 0.4073
5.000 0.9704 0.01087 0.00410 -0.0899 0.3043 0.4140
5.250 0.9995 0.01099 0.00424 -0.0900 0.2981 0.4207
5.500 1.0279 0.01118 0.00440 -0.0899 0.2910 0.4265
5.750 1.0567 0.01133 0.00454 -0.0899 0.2858 0.4314
6.000 1.0851 0.01149 0.00470 -0.0899 0.2791 0.4383
6.250 1.1130 0.01170 0.00489 -0.0898 0.2725 0.4450
6.500 1.1414 0.01185 0.00505 -0.0897 0.2675 0.4503
6.750 1.1692 0.01205 0.00523 -0.0896 0.2619 0.4543
7.000 1.1964 0.01229 0.00545 -0.0894 0.2557 0.4594
7.250 1.2242 0.01246 0.00564 -0.0892 0.2503 0.4654
7.500 1.2510 0.01270 0.00587 -0.0890 0.2441 0.4721
8.000 1.3050 0.01312 0.00631 -0.0885 0.2352 0.4861
8.250 1.3314 0.01335 0.00655 -0.0882 0.2303 0.4927
8.500 1.3568 0.01365 0.00683 -0.0877 0.2250 0.4992
8.750 1.3831 0.01385 0.00707 -0.0874 0.2207 0.5085
9.000 1.4084 0.01412 0.00735 -0.0869 0.2154 0.5180
9.250 1.4325 0.01446 0.00767 -0.0863 0.2101 0.5247
9.500 1.4575 0.01470 0.00794 -0.0857 0.2061 0.5324
9.750 1.4812 0.01501 0.00826 -0.0851 0.2010 0.5403
10.250 1.5266 0.01568 0.00897 -0.0834 0.1912 0.5605
10.500 1.5469 0.01608 0.00939 -0.0822 0.1853 0.5752
10.750 1.5668 0.01646 0.00983 -0.0810 0.1804 0.6028
11.000 1.5860 0.01670 0.01032 -0.0798 0.1757 0.7159
11.250 1.5949 0.01674 0.01086 -0.0764 0.1719 1.0000
11.500 1.6099 0.01731 0.01142 -0.0746 0.1679 1.0000
11.750 1.6240 0.01798 0.01209 -0.0727 0.1628 1.0000
12.000 1.6359 0.01883 0.01292 -0.0709 0.1580 1.0000
12.250 1.6512 0.01956 0.01367 -0.0695 0.1545 1.0000
12.500 1.6642 0.02047 0.01458 -0.0680 0.1504 1.0000
12.750 1.6750 0.02159 0.01570 -0.0666 0.1462 1.0000
13.000 1.6885 0.02261 0.01673 -0.0655 0.1427 1.0000
13.250 1.6991 0.02388 0.01801 -0.0643 0.1385 1.0000
13.500 1.7080 0.02535 0.01950 -0.0632 0.1346 1.0000
13.750 1.7182 0.02678 0.02095 -0.0623 0.1311 1.0000
14.000 1.7258 0.02848 0.02266 -0.0614 0.1276 1.0000
14.250 1.7325 0.03029 0.02450 -0.0605 0.1249 1.0000
14.500 1.7405 0.03204 0.02629 -0.0598 0.1224 1.0000
14.750 1.7459 0.03405 0.02834 -0.0591 0.1195 1.0000
15.000 1.7475 0.03644 0.03075 -0.0583 0.1165 1.0000
15.250 1.7508 0.03870 0.03305 -0.0577 0.1138 1.0000
15.500 1.7517 0.04122 0.03562 -0.0571 0.1105 1.0000
15.750 1.7487 0.04417 0.03860 -0.0566 0.1076 1.0000
16.000 1.7471 0.04707 0.04155 -0.0562 0.1052 1.0000
16.250 1.7456 0.05004 0.04457 -0.0559 0.1027 1.0000
16.500 1.7415 0.05332 0.04789 -0.0556 0.1001 1.0000
16.750 1.7362 0.05678 0.05140 -0.0555 0.0979 1.0000
17.000 1.7331 0.06009 0.05478 -0.0555 0.0960 1.0000
17.250 1.7280 0.06367 0.05842 -0.0556 0.0938 1.0000
17.500 1.7207 0.06750 0.06230 -0.0557 0.0916 1.0000
17.750 1.7134 0.07138 0.06623 -0.0559 0.0896 1.0000
18.000 1.7075 0.07518 0.07010 -0.0562 0.0877 1.0000
18.250 1.7011 0.07900 0.07397 -0.0565 0.0853 1.0000
18.500 1.6898 0.08350 0.07853 -0.0571 0.0831 1.0000
18.750 1.6817 0.08767 0.08276 -0.0576 0.0810 1.0000
19.000 1.6747 0.09170 0.08683 -0.0582 0.0785 1.0000
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