ONERA HOR20 AIRFOIL (hor20-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: ONERA HOR20 AIRFOIL (hor20-il) Reynolds number: 200,000 Max Cl/Cd: 63.43 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hor20-il-200000-n5.txt Download as CSV file: xf-hor20-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.250 -0.8951 0.09553 0.09002 -0.0358 1.0000 0.0763
-16.000 -0.8926 0.09237 0.08688 -0.0374 1.0000 0.0775
-15.750 -0.8977 0.08797 0.08245 -0.0399 1.0000 0.0788
-15.500 -0.9121 0.08217 0.07656 -0.0432 1.0000 0.0803
-15.250 -0.9310 0.07577 0.07000 -0.0471 1.0000 0.0819
-15.000 -0.9457 0.07019 0.06427 -0.0504 1.0000 0.0833
-14.750 -0.9451 0.06711 0.06121 -0.0520 1.0000 0.0844
-14.500 -0.9509 0.06323 0.05728 -0.0542 1.0000 0.0856
-14.250 -0.9579 0.05921 0.05319 -0.0565 1.0000 0.0869
-14.000 -0.9650 0.05520 0.04909 -0.0588 1.0000 0.0882
-13.750 -0.9717 0.05129 0.04506 -0.0612 1.0000 0.0896
-13.500 -0.9735 0.04807 0.04180 -0.0630 1.0000 0.0908
-13.250 -0.9740 0.04503 0.03874 -0.0648 1.0000 0.0919
-13.000 -0.9749 0.04187 0.03554 -0.0668 1.0000 0.0932
-12.750 -0.9750 0.03877 0.03238 -0.0689 1.0000 0.0947
-12.500 -0.9742 0.03573 0.02924 -0.0712 1.0000 0.0963
-12.250 -0.9747 0.03270 0.02609 -0.0736 1.0000 0.0978
-12.000 -0.9690 0.03055 0.02393 -0.0751 1.0000 0.0992
-11.750 -0.9581 0.02913 0.02247 -0.0754 1.0000 0.1011
-11.500 -0.9343 0.02788 0.02114 -0.0773 0.9801 0.1038
-11.250 -0.9040 0.02673 0.01989 -0.0799 0.9605 0.1066
-11.000 -0.8767 0.02575 0.01889 -0.0815 0.9405 0.1092
-10.750 -0.8521 0.02494 0.01798 -0.0820 0.9187 0.1119
-10.500 -0.8284 0.02422 0.01712 -0.0821 0.8986 0.1146
-10.250 -0.8062 0.02352 0.01639 -0.0819 0.8794 0.1169
-9.750 -0.7593 0.02236 0.01502 -0.0813 0.8441 0.1223
-9.500 -0.7353 0.02181 0.01438 -0.0810 0.8290 0.1249
-9.250 -0.7111 0.02132 0.01381 -0.0807 0.8145 0.1276
-9.000 -0.6855 0.02086 0.01326 -0.0806 0.8011 0.1309
-8.500 -0.6336 0.02000 0.01226 -0.0804 0.7765 0.1377
-8.250 -0.6071 0.01965 0.01178 -0.0803 0.7650 0.1417
-8.000 -0.5797 0.01927 0.01133 -0.0803 0.7536 0.1455
-7.750 -0.5526 0.01892 0.01094 -0.0803 0.7426 0.1495
-7.500 -0.5247 0.01861 0.01053 -0.0804 0.7322 0.1541
-7.250 -0.4969 0.01829 0.01016 -0.0804 0.7210 0.1583
-7.000 -0.4689 0.01801 0.00982 -0.0804 0.7111 0.1630
-6.750 -0.4402 0.01775 0.00947 -0.0806 0.7007 0.1681
-6.500 -0.4120 0.01750 0.00919 -0.0806 0.6909 0.1728
-6.250 -0.3830 0.01727 0.00891 -0.0808 0.6809 0.1786
-6.000 -0.3542 0.01706 0.00864 -0.0809 0.6705 0.1840
-5.750 -0.3253 0.01689 0.00842 -0.0810 0.6613 0.1896
-5.250 -0.2669 0.01655 0.00797 -0.0812 0.6422 0.2007
-5.000 -0.2373 0.01641 0.00777 -0.0814 0.6328 0.2065
-4.750 -0.2078 0.01627 0.00756 -0.0816 0.6234 0.2120
-4.500 -0.1785 0.01616 0.00741 -0.0817 0.6153 0.2174
-4.250 -0.1486 0.01604 0.00724 -0.0819 0.6062 0.2234
-4.000 -0.1191 0.01594 0.00706 -0.0820 0.5975 0.2288
-3.750 -0.0895 0.01583 0.00694 -0.0821 0.5898 0.2343
-3.500 -0.0596 0.01575 0.00680 -0.0823 0.5817 0.2404
-3.250 -0.0299 0.01567 0.00665 -0.0825 0.5741 0.2458
-3.000 -0.0003 0.01558 0.00655 -0.0826 0.5669 0.2515
-2.750 0.0296 0.01551 0.00645 -0.0828 0.5592 0.2577
-2.500 0.0595 0.01546 0.00632 -0.0830 0.5522 0.2634
-2.250 0.0890 0.01539 0.00624 -0.0831 0.5462 0.2693
-2.000 0.1190 0.01532 0.00619 -0.0833 0.5393 0.2756
-1.500 0.1783 0.01526 0.00605 -0.0836 0.5264 0.2879
-1.250 0.2083 0.01523 0.00603 -0.0838 0.5205 0.2947
-0.750 0.2677 0.01520 0.00599 -0.0840 0.5080 0.3081
-0.500 0.2973 0.01524 0.00598 -0.0841 0.5024 0.3156
-0.250 0.3273 0.01524 0.00599 -0.0843 0.4964 0.3229
0.000 0.3569 0.01525 0.00604 -0.0844 0.4902 0.3308
0.250 0.3864 0.01532 0.00605 -0.0845 0.4846 0.3397
0.500 0.4159 0.01537 0.00611 -0.0846 0.4794 0.3481
0.750 0.4457 0.01540 0.00620 -0.0847 0.4734 0.3577
1.000 0.4753 0.01546 0.00626 -0.0848 0.4676 0.3670
1.250 0.5045 0.01554 0.00634 -0.0848 0.4622 0.3768
1.500 0.5340 0.01564 0.00641 -0.0849 0.4571 0.3866
1.750 0.5634 0.01569 0.00655 -0.0850 0.4516 0.3955
2.000 0.5926 0.01580 0.00663 -0.0850 0.4460 0.4055
2.250 0.6215 0.01591 0.00672 -0.0850 0.4409 0.4139
2.500 0.6506 0.01601 0.00686 -0.0850 0.4357 0.4227
2.750 0.6799 0.01613 0.00697 -0.0851 0.4302 0.4318
3.000 0.7085 0.01623 0.00711 -0.0850 0.4247 0.4396
3.250 0.7369 0.01639 0.00722 -0.0849 0.4197 0.4483
3.500 0.7658 0.01652 0.00737 -0.0849 0.4144 0.4559
3.750 0.7942 0.01663 0.00755 -0.0849 0.4090 0.4631
4.000 0.8224 0.01678 0.00770 -0.0847 0.4037 0.4713
4.250 0.8502 0.01698 0.00782 -0.0846 0.3988 0.4790
4.500 0.8784 0.01709 0.00804 -0.0845 0.3930 0.4859
4.750 0.9061 0.01724 0.00822 -0.0843 0.3871 0.4933
5.000 0.9335 0.01745 0.00837 -0.0841 0.3818 0.5007
5.250 0.9607 0.01760 0.00859 -0.0839 0.3765 0.5079
5.500 0.9880 0.01777 0.00882 -0.0836 0.3706 0.5162
5.750 1.0147 0.01799 0.00901 -0.0834 0.3648 0.5240
6.000 1.0408 0.01819 0.00923 -0.0830 0.3597 0.5313
6.250 1.0675 0.01837 0.00951 -0.0827 0.3540 0.5403
6.500 1.0934 0.01858 0.00977 -0.0823 0.3483 0.5508
6.750 1.1185 0.01882 0.01003 -0.0817 0.3434 0.5632
7.000 1.1438 0.01904 0.01034 -0.0813 0.3383 0.5759
7.250 1.1687 0.01927 0.01065 -0.0807 0.3323 0.5902
7.500 1.1924 0.01952 0.01096 -0.0800 0.3266 0.6059
7.750 1.2159 0.01978 0.01130 -0.0793 0.3214 0.6255
8.000 1.2391 0.02001 0.01169 -0.0785 0.3157 0.6559
8.250 1.2602 0.02018 0.01207 -0.0773 0.3103 0.7238
8.500 1.2774 0.02014 0.01233 -0.0751 0.3057 1.0000
8.750 1.3002 0.02054 0.01277 -0.0744 0.3005 1.0000
9.000 1.3213 0.02099 0.01322 -0.0734 0.2952 1.0000
9.250 1.3403 0.02151 0.01368 -0.0721 0.2904 1.0000
9.500 1.3594 0.02201 0.01420 -0.0709 0.2853 1.0000
9.750 1.3765 0.02254 0.01475 -0.0694 0.2799 1.0000
10.000 1.3896 0.02316 0.01535 -0.0673 0.2751 1.0000
10.250 1.4032 0.02386 0.01603 -0.0655 0.2707 1.0000
10.500 1.4181 0.02456 0.01679 -0.0640 0.2658 1.0000
10.750 1.4311 0.02538 0.01763 -0.0624 0.2611 1.0000
11.000 1.4425 0.02634 0.01855 -0.0608 0.2569 1.0000
11.250 1.4560 0.02726 0.01953 -0.0595 0.2527 1.0000
11.500 1.4682 0.02830 0.02062 -0.0583 0.2481 1.0000
11.750 1.4784 0.02949 0.02182 -0.0570 0.2437 1.0000
12.000 1.4876 0.03082 0.02313 -0.0558 0.2397 1.0000
12.250 1.4986 0.03210 0.02450 -0.0548 0.2352 1.0000
12.500 1.5073 0.03358 0.02603 -0.0539 0.2306 1.0000
12.750 1.5140 0.03524 0.02768 -0.0529 0.2265 1.0000
13.000 1.5216 0.03691 0.02941 -0.0521 0.2224 1.0000
13.250 1.5285 0.03870 0.03127 -0.0514 0.2179 1.0000
13.500 1.5335 0.04066 0.03327 -0.0507 0.2138 1.0000
13.750 1.5372 0.04274 0.03533 -0.0500 0.2103 1.0000
14.000 1.5423 0.04482 0.03753 -0.0495 0.2062 1.0000
14.250 1.5451 0.04713 0.03991 -0.0491 0.2021 1.0000
14.500 1.5462 0.04960 0.04239 -0.0486 0.1983 1.0000
14.750 1.5478 0.05208 0.04492 -0.0483 0.1948 1.0000
15.000 1.5491 0.05475 0.04768 -0.0481 0.1908 1.0000
15.250 1.5488 0.05760 0.05059 -0.0480 0.1869 1.0000
15.500 1.5475 0.06054 0.05352 -0.0480 0.1834 1.0000
15.750 1.5467 0.06364 0.05672 -0.0481 0.1795 1.0000
16.000 1.5442 0.06696 0.06012 -0.0484 0.1753 1.0000
16.250 1.5408 0.07037 0.06354 -0.0487 0.1715 1.0000
16.500 1.5377 0.07386 0.06710 -0.0491 0.1678 1.0000
16.750 1.5338 0.07752 0.07085 -0.0497 0.1638 1.0000
17.000 1.5303 0.08110 0.07446 -0.0502 0.1604 1.0000
17.250 1.5273 0.08461 0.07799 -0.0507 0.1573 1.0000
17.500 1.5227 0.08850 0.08200 -0.0515 0.1537 1.0000
17.750 1.5173 0.09250 0.08606 -0.0524 0.1502 1.0000
18.000 1.5142 0.09610 0.08966 -0.0531 0.1470 1.0000
18.250 1.5081 0.10032 0.09400 -0.0542 0.1437 1.0000
18.500 1.5024 0.10447 0.09823 -0.0553 0.1404 1.0000
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