ONERA HOR20 AIRFOIL (hor20-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: ONERA HOR20 AIRFOIL (hor20-il) Reynolds number: 500,000 Max Cl/Cd: 91.14 at α=8.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hor20-il-500000.txt Download as CSV file: xf-hor20-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -1.0704 0.10329 0.09915 -0.0292 1.0000 0.0624
-18.250 -1.0803 0.09820 0.09396 -0.0321 1.0000 0.0636
-18.000 -1.0917 0.09296 0.08860 -0.0350 1.0000 0.0647
-17.750 -1.0869 0.09040 0.08610 -0.0361 1.0000 0.0658
-17.500 -1.0914 0.08632 0.08200 -0.0383 1.0000 0.0669
-17.250 -1.0966 0.08213 0.07775 -0.0406 1.0000 0.0681
-17.000 -1.1047 0.07752 0.07304 -0.0431 1.0000 0.0693
-16.750 -1.1139 0.07279 0.06819 -0.0458 1.0000 0.0704
-16.500 -1.1128 0.06984 0.06529 -0.0471 1.0000 0.0716
-16.250 -1.1173 0.06597 0.06139 -0.0492 1.0000 0.0727
-16.000 -1.1216 0.06216 0.05753 -0.0513 1.0000 0.0739
-15.750 -1.1284 0.05820 0.05348 -0.0534 1.0000 0.0751
-15.500 -1.1360 0.05421 0.04937 -0.0556 1.0000 0.0762
-15.250 -1.1404 0.05086 0.04600 -0.0573 1.0000 0.0773
-15.000 -1.1457 0.04735 0.04248 -0.0591 1.0000 0.0784
-14.750 -1.1503 0.04383 0.03891 -0.0611 1.0000 0.0795
-14.500 -1.1533 0.04045 0.03547 -0.0631 1.0000 0.0806
-14.250 -1.1542 0.03720 0.03214 -0.0651 1.0000 0.0818
-14.000 -1.1525 0.03410 0.02893 -0.0673 1.0000 0.0829
-13.750 -1.1549 0.03056 0.02536 -0.0700 1.0000 0.0840
-13.500 -1.1527 0.02684 0.02156 -0.0743 1.0000 0.0852
-13.250 -1.1384 0.02528 0.01994 -0.0754 1.0000 0.0867
-13.000 -1.1207 0.02417 0.01876 -0.0758 1.0000 0.0882
-12.750 -1.1008 0.02329 0.01780 -0.0759 1.0000 0.0897
-12.500 -1.0830 0.02226 0.01676 -0.0759 1.0000 0.0913
-12.250 -1.0638 0.02142 0.01593 -0.0757 1.0000 0.0929
-12.000 -1.0427 0.02078 0.01527 -0.0755 0.9990 0.0947
-11.750 -1.0059 0.02014 0.01456 -0.0780 0.9867 0.0969
-11.500 -0.9711 0.01932 0.01373 -0.0803 0.9718 0.0993
-11.250 -0.9392 0.01869 0.01309 -0.0817 0.9555 0.1016
-11.000 -0.9133 0.01827 0.01259 -0.0816 0.9341 0.1039
-10.750 -0.8894 0.01791 0.01211 -0.0809 0.9119 0.1059
-10.500 -0.8670 0.01733 0.01151 -0.0803 0.8913 0.1083
-10.250 -0.8422 0.01694 0.01105 -0.0798 0.8727 0.1108
-10.000 -0.8163 0.01664 0.01062 -0.0795 0.8552 0.1133
-9.500 -0.7638 0.01585 0.00972 -0.0792 0.8235 0.1192
-9.250 -0.7363 0.01561 0.00937 -0.0791 0.8103 0.1224
-9.000 -0.7088 0.01525 0.00896 -0.0791 0.7973 0.1257
-8.750 -0.6811 0.01494 0.00861 -0.0791 0.7854 0.1291
-8.500 -0.6524 0.01471 0.00831 -0.0792 0.7734 0.1326
-8.250 -0.6243 0.01441 0.00795 -0.0792 0.7626 0.1363
-8.000 -0.5953 0.01413 0.00766 -0.0794 0.7522 0.1405
-7.750 -0.5662 0.01399 0.00741 -0.0794 0.7412 0.1444
-7.500 -0.5374 0.01364 0.00709 -0.0797 0.7309 0.1492
-7.250 -0.5081 0.01347 0.00685 -0.0798 0.7200 0.1540
-7.000 -0.4788 0.01324 0.00658 -0.0799 0.7102 0.1587
-6.750 -0.4493 0.01302 0.00635 -0.0802 0.6997 0.1638
-6.250 -0.3900 0.01265 0.00592 -0.0805 0.6789 0.1741
-6.000 -0.3601 0.01255 0.00573 -0.0807 0.6685 0.1795
-5.750 -0.3302 0.01238 0.00555 -0.0809 0.6587 0.1849
-5.500 -0.3002 0.01224 0.00540 -0.0811 0.6480 0.1906
-5.250 -0.2700 0.01220 0.00525 -0.0813 0.6381 0.1957
-5.000 -0.2399 0.01202 0.00511 -0.0816 0.6284 0.2018
-4.750 -0.2098 0.01199 0.00500 -0.0817 0.6187 0.2078
-4.500 -0.1794 0.01189 0.00489 -0.0820 0.6098 0.2137
-4.250 -0.1492 0.01183 0.00482 -0.0822 0.6003 0.2203
-4.000 -0.1188 0.01186 0.00475 -0.0824 0.5917 0.2260
-3.750 -0.0884 0.01172 0.00465 -0.0827 0.5838 0.2321
-3.500 -0.0581 0.01168 0.00458 -0.0829 0.5758 0.2378
-3.250 -0.0276 0.01172 0.00452 -0.0831 0.5682 0.2429
-3.000 0.0028 0.01158 0.00441 -0.0834 0.5608 0.2487
-2.750 0.0331 0.01153 0.00434 -0.0836 0.5533 0.2543
-2.500 0.0634 0.01156 0.00430 -0.0838 0.5464 0.2596
-2.250 0.0940 0.01149 0.00423 -0.0841 0.5402 0.2647
-2.000 0.1243 0.01140 0.00416 -0.0843 0.5332 0.2710
-1.750 0.1544 0.01144 0.00412 -0.0845 0.5260 0.2768
-1.500 0.1851 0.01144 0.00409 -0.0847 0.5203 0.2816
-1.250 0.2154 0.01133 0.00404 -0.0850 0.5140 0.2891
-1.000 0.2455 0.01134 0.00402 -0.0852 0.5077 0.2956
-0.750 0.2758 0.01141 0.00402 -0.0853 0.5017 0.3012
-0.500 0.3063 0.01132 0.00402 -0.0856 0.4966 0.3092
-0.250 0.3366 0.01132 0.00402 -0.0858 0.4908 0.3169
0.000 0.3667 0.01137 0.00403 -0.0860 0.4850 0.3244
0.250 0.3968 0.01140 0.00409 -0.0862 0.4798 0.3334
0.500 0.4274 0.01140 0.00411 -0.0864 0.4749 0.3421
0.750 0.4576 0.01138 0.00414 -0.0866 0.4694 0.3522
1.000 0.4876 0.01145 0.00417 -0.0868 0.4638 0.3624
1.250 0.5175 0.01151 0.00426 -0.0869 0.4586 0.3734
1.500 0.5480 0.01153 0.00431 -0.0871 0.4538 0.3844
1.750 0.5780 0.01155 0.00438 -0.0873 0.4484 0.3949
2.000 0.6077 0.01166 0.00445 -0.0874 0.4428 0.4054
2.250 0.6374 0.01176 0.00455 -0.0875 0.4377 0.4150
2.500 0.6675 0.01180 0.00465 -0.0876 0.4330 0.4245
2.750 0.6974 0.01191 0.00473 -0.0877 0.4277 0.4321
3.000 0.7266 0.01200 0.00482 -0.0878 0.4222 0.4408
3.250 0.7561 0.01213 0.00495 -0.0878 0.4168 0.4489
3.500 0.7859 0.01221 0.00504 -0.0879 0.4116 0.4554
3.750 0.8151 0.01227 0.00513 -0.0880 0.4060 0.4630
4.000 0.8438 0.01245 0.00527 -0.0879 0.4001 0.4704
4.250 0.8733 0.01256 0.00539 -0.0880 0.3952 0.4771
4.500 0.9025 0.01261 0.00549 -0.0880 0.3896 0.4840
4.750 0.9310 0.01274 0.00562 -0.0880 0.3840 0.4907
5.000 0.9593 0.01295 0.00578 -0.0879 0.3784 0.4974
5.250 0.9884 0.01302 0.00591 -0.0879 0.3736 0.5041
5.500 1.0169 0.01312 0.00605 -0.0879 0.3682 0.5112
5.750 1.0445 0.01333 0.00622 -0.0877 0.3624 0.5181
6.000 1.0728 0.01348 0.00638 -0.0876 0.3569 0.5242
6.250 1.1009 0.01356 0.00653 -0.0875 0.3508 0.5318
6.500 1.1279 0.01376 0.00671 -0.0873 0.3450 0.5394
6.750 1.1552 0.01397 0.00691 -0.0870 0.3395 0.5472
7.000 1.1828 0.01407 0.00710 -0.0869 0.3339 0.5569
7.250 1.2094 0.01428 0.00731 -0.0866 0.3283 0.5672
7.500 1.2351 0.01452 0.00758 -0.0862 0.3229 0.5789
8.000 1.2879 0.01483 0.00804 -0.0855 0.3113 0.6154
8.250 1.3120 0.01504 0.00837 -0.0849 0.3051 0.6565
8.500 1.3300 0.01462 0.00864 -0.0826 0.3001 0.8889
8.750 1.3562 0.01488 0.00887 -0.0824 0.2940 1.0000
9.000 1.3792 0.01529 0.00922 -0.0816 0.2884 1.0000
9.250 1.4044 0.01555 0.00951 -0.0811 0.2836 1.0000
9.500 1.4275 0.01591 0.00985 -0.0803 0.2782 1.0000
9.750 1.4475 0.01641 0.01028 -0.0791 0.2727 1.0000
10.000 1.4706 0.01672 0.01063 -0.0784 0.2682 1.0000
10.250 1.4911 0.01713 0.01104 -0.0772 0.2631 1.0000
10.500 1.5077 0.01767 0.01154 -0.0755 0.2582 1.0000
10.750 1.5233 0.01817 0.01205 -0.0736 0.2539 1.0000
11.000 1.5405 0.01865 0.01257 -0.0721 0.2495 1.0000
11.250 1.5550 0.01931 0.01322 -0.0703 0.2450 1.0000
11.500 1.5657 0.02022 0.01409 -0.0683 0.2403 1.0000
11.750 1.5838 0.02079 0.01473 -0.0672 0.2362 1.0000
12.000 1.5981 0.02160 0.01557 -0.0658 0.2314 1.0000
12.250 1.6083 0.02272 0.01666 -0.0643 0.2267 1.0000
12.500 1.6222 0.02368 0.01766 -0.0631 0.2225 1.0000
12.750 1.6356 0.02471 0.01873 -0.0621 0.2177 1.0000
13.000 1.6445 0.02612 0.02013 -0.0609 0.2130 1.0000
13.250 1.6543 0.02752 0.02156 -0.0599 0.2085 1.0000
13.500 1.6660 0.02884 0.02293 -0.0591 0.2040 1.0000
13.750 1.6727 0.03058 0.02467 -0.0582 0.1996 1.0000
14.000 1.6779 0.03251 0.02661 -0.0573 0.1955 1.0000
14.250 1.6876 0.03409 0.02826 -0.0567 0.1913 1.0000
14.500 1.6918 0.03618 0.03038 -0.0559 0.1871 1.0000
14.750 1.6908 0.03878 0.03297 -0.0551 0.1832 1.0000
15.000 1.6982 0.04064 0.03491 -0.0546 0.1797 1.0000
15.250 1.7011 0.04295 0.03727 -0.0541 0.1761 1.0000
15.500 1.6990 0.04578 0.04012 -0.0535 0.1727 1.0000
15.750 1.6972 0.04866 0.04303 -0.0531 0.1694 1.0000
16.000 1.7008 0.05106 0.04551 -0.0529 0.1660 1.0000
16.250 1.6990 0.05408 0.04857 -0.0527 0.1624 1.0000
16.500 1.6928 0.05762 0.05212 -0.0526 0.1592 1.0000
16.750 1.6932 0.06048 0.05505 -0.0525 0.1562 1.0000
17.000 1.6929 0.06347 0.05812 -0.0525 0.1531 1.0000
17.250 1.6886 0.06695 0.06163 -0.0527 0.1501 1.0000
17.500 1.6819 0.07071 0.06540 -0.0529 0.1473 1.0000
17.750 1.6812 0.07385 0.06863 -0.0531 0.1447 1.0000
18.000 1.6803 0.07700 0.07184 -0.0533 0.1418 1.0000
18.250 1.6750 0.08073 0.07562 -0.0538 0.1390 1.0000
18.500 1.6675 0.08473 0.07963 -0.0543 0.1364 1.0000
18.750 1.6657 0.08808 0.08306 -0.0547 0.1339 1.0000
19.000 1.6633 0.09153 0.08658 -0.0553 0.1312 1.0000
19.250 1.6577 0.09540 0.09049 -0.0560 0.1286 1.0000
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