ONERA HOR20 AIRFOIL (hor20-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: ONERA HOR20 AIRFOIL (hor20-il) Reynolds number: 500,000 Max Cl/Cd: 83.87 at α=10° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hor20-il-500000-n5.txt Download as CSV file: xf-hor20-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -1.0107 0.10294 0.09867 -0.0278 1.0000 0.0548
-17.500 -1.0182 0.09829 0.09399 -0.0302 1.0000 0.0557
-17.250 -1.0275 0.09339 0.08903 -0.0328 1.0000 0.0567
-17.000 -1.0335 0.08905 0.08463 -0.0351 1.0000 0.0577
-16.750 -1.0410 0.08453 0.08003 -0.0374 1.0000 0.0586
-16.500 -1.0478 0.08015 0.07560 -0.0397 1.0000 0.0595
-16.250 -1.0597 0.07514 0.07054 -0.0423 1.0000 0.0604
-16.000 -1.0709 0.07024 0.06559 -0.0449 1.0000 0.0613
-15.750 -1.0810 0.06562 0.06089 -0.0474 1.0000 0.0623
-15.500 -1.0897 0.06128 0.05648 -0.0497 1.0000 0.0632
-15.250 -1.0996 0.05700 0.05212 -0.0519 1.0000 0.0641
-15.000 -1.1115 0.05256 0.04760 -0.0542 1.0000 0.0648
-14.750 -1.1266 0.04778 0.04275 -0.0568 1.0000 0.0655
-14.500 -1.1400 0.04321 0.03811 -0.0594 1.0000 0.0663
-14.250 -1.1516 0.03881 0.03363 -0.0620 1.0000 0.0671
-14.000 -1.1611 0.03454 0.02928 -0.0647 1.0000 0.0680
-13.750 -1.1703 0.03005 0.02469 -0.0683 1.0000 0.0688
-13.500 -1.1616 0.02637 0.02085 -0.0732 1.0000 0.0699
-13.250 -1.1471 0.02471 0.01913 -0.0743 1.0000 0.0711
-13.000 -1.1216 0.02343 0.01779 -0.0764 0.9703 0.0726
-12.750 -1.0944 0.02246 0.01674 -0.0780 0.9480 0.0742
-12.500 -1.0719 0.02172 0.01591 -0.0781 0.9234 0.0757
-12.250 -1.0509 0.02103 0.01512 -0.0777 0.8986 0.0770
-12.000 -1.0296 0.02036 0.01436 -0.0774 0.8761 0.0786
-11.750 -1.0067 0.01981 0.01370 -0.0771 0.8547 0.0804
-11.500 -0.9827 0.01934 0.01311 -0.0768 0.8347 0.0822
-11.250 -0.9580 0.01885 0.01252 -0.0767 0.8172 0.0839
-11.000 -0.9328 0.01835 0.01195 -0.0767 0.8028 0.0858
-10.500 -0.8799 0.01757 0.01099 -0.0767 0.7766 0.0897
-10.250 -0.8533 0.01715 0.01051 -0.0767 0.7649 0.0915
-10.000 -0.8260 0.01675 0.01006 -0.0768 0.7544 0.0938
-9.750 -0.7984 0.01643 0.00966 -0.0769 0.7427 0.0963
-9.500 -0.7706 0.01608 0.00926 -0.0770 0.7326 0.0988
-9.250 -0.7426 0.01572 0.00887 -0.0772 0.7222 0.1018
-9.000 -0.7143 0.01545 0.00852 -0.0773 0.7124 0.1045
-8.750 -0.6856 0.01515 0.00817 -0.0775 0.7022 0.1069
-8.500 -0.6572 0.01486 0.00783 -0.0776 0.6916 0.1099
-8.250 -0.6281 0.01460 0.00753 -0.0778 0.6827 0.1130
-8.000 -0.5991 0.01433 0.00723 -0.0780 0.6730 0.1162
-7.750 -0.5701 0.01409 0.00694 -0.0782 0.6635 0.1200
-7.500 -0.5405 0.01388 0.00669 -0.0784 0.6537 0.1237
-7.250 -0.5114 0.01364 0.00641 -0.0786 0.6433 0.1278
-7.000 -0.4817 0.01344 0.00618 -0.0788 0.6347 0.1319
-6.750 -0.4520 0.01324 0.00595 -0.0791 0.6249 0.1358
-6.500 -0.4224 0.01307 0.00573 -0.0793 0.6153 0.1403
-6.250 -0.3924 0.01292 0.00554 -0.0795 0.6057 0.1444
-6.000 -0.3626 0.01274 0.00533 -0.0798 0.5961 0.1489
-5.750 -0.3325 0.01260 0.00516 -0.0800 0.5877 0.1537
-5.500 -0.3025 0.01247 0.00499 -0.0803 0.5780 0.1581
-5.250 -0.2725 0.01234 0.00482 -0.0805 0.5690 0.1632
-5.000 -0.2422 0.01223 0.00468 -0.0808 0.5610 0.1681
-4.750 -0.2120 0.01210 0.00454 -0.0810 0.5529 0.1740
-4.500 -0.1818 0.01202 0.00442 -0.0813 0.5453 0.1805
-4.250 -0.1515 0.01189 0.00432 -0.0816 0.5376 0.1876
-4.000 -0.1212 0.01183 0.00422 -0.0818 0.5298 0.1943
-3.750 -0.0909 0.01176 0.00413 -0.0821 0.5235 0.2002
-3.500 -0.0604 0.01169 0.00406 -0.0823 0.5179 0.2063
-3.250 -0.0299 0.01165 0.00399 -0.0826 0.5116 0.2116
-3.000 0.0003 0.01160 0.00392 -0.0828 0.5053 0.2171
-2.750 0.0308 0.01157 0.00387 -0.0831 0.5000 0.2225
-2.500 0.0614 0.01154 0.00382 -0.0833 0.4950 0.2270
-2.250 0.0918 0.01149 0.00377 -0.0836 0.4896 0.2324
-2.000 0.1221 0.01148 0.00374 -0.0838 0.4839 0.2378
-1.750 0.1526 0.01148 0.00371 -0.0840 0.4788 0.2426
-1.500 0.1832 0.01143 0.00367 -0.0843 0.4733 0.2476
-1.250 0.2136 0.01140 0.00364 -0.0845 0.4672 0.2532
-1.000 0.2438 0.01142 0.00362 -0.0847 0.4613 0.2584
-0.750 0.2743 0.01142 0.00361 -0.0849 0.4565 0.2627
-0.500 0.3047 0.01137 0.00359 -0.0852 0.4511 0.2688
-0.250 0.3350 0.01137 0.00359 -0.0854 0.4453 0.2748
0.250 0.3955 0.01139 0.00360 -0.0858 0.4354 0.2866
0.500 0.4258 0.01139 0.00362 -0.0860 0.4304 0.2938
0.750 0.4559 0.01142 0.00364 -0.0862 0.4249 0.3005
1.000 0.4857 0.01147 0.00368 -0.0864 0.4194 0.3090
1.250 0.5160 0.01148 0.00373 -0.0866 0.4150 0.3191
1.500 0.5461 0.01150 0.00379 -0.0867 0.4101 0.3292
1.750 0.5760 0.01156 0.00385 -0.0869 0.4047 0.3401
2.000 0.6055 0.01164 0.00393 -0.0870 0.3992 0.3507
2.250 0.6356 0.01168 0.00400 -0.0872 0.3949 0.3618
2.500 0.6654 0.01173 0.00409 -0.0873 0.3901 0.3713
2.750 0.6950 0.01182 0.00418 -0.0874 0.3850 0.3807
3.000 0.7242 0.01194 0.00429 -0.0875 0.3797 0.3891
3.250 0.7540 0.01200 0.00439 -0.0876 0.3749 0.3982
3.500 0.7834 0.01211 0.00450 -0.0876 0.3691 0.4059
3.750 0.8123 0.01224 0.00462 -0.0877 0.3633 0.4127
4.000 0.8414 0.01236 0.00475 -0.0877 0.3581 0.4209
4.250 0.8706 0.01247 0.00487 -0.0877 0.3526 0.4283
4.500 0.8993 0.01262 0.00501 -0.0877 0.3466 0.4340
4.750 0.9276 0.01278 0.00517 -0.0876 0.3412 0.4404
5.000 0.9565 0.01289 0.00531 -0.0876 0.3361 0.4474
5.250 0.9850 0.01305 0.00547 -0.0876 0.3308 0.4536
5.500 1.0128 0.01324 0.00565 -0.0874 0.3256 0.4596
5.750 1.0410 0.01339 0.00583 -0.0873 0.3208 0.4657
6.000 1.0690 0.01356 0.00601 -0.0872 0.3147 0.4717
6.250 1.0960 0.01379 0.00621 -0.0870 0.3082 0.4769
6.500 1.1234 0.01398 0.00642 -0.0868 0.3029 0.4829
6.750 1.1507 0.01416 0.00663 -0.0866 0.2972 0.4901
7.000 1.1770 0.01442 0.00687 -0.0862 0.2913 0.4975
7.250 1.2036 0.01464 0.00711 -0.0859 0.2866 0.5044
7.500 1.2302 0.01484 0.00736 -0.0856 0.2817 0.5121
7.750 1.2556 0.01511 0.00763 -0.0852 0.2759 0.5203
8.000 1.2806 0.01539 0.00793 -0.0847 0.2701 0.5298
8.250 1.3057 0.01565 0.00822 -0.0842 0.2638 0.5407
8.500 1.3290 0.01600 0.00856 -0.0834 0.2575 0.5495
8.750 1.3532 0.01628 0.00889 -0.0828 0.2524 0.5597
9.000 1.3767 0.01658 0.00923 -0.0821 0.2472 0.5712
9.250 1.3985 0.01694 0.00963 -0.0812 0.2422 0.5877
9.500 1.4206 0.01725 0.01003 -0.0803 0.2380 0.6129
9.750 1.4422 0.01749 0.01045 -0.0793 0.2333 0.6718
10.000 1.4551 0.01735 0.01088 -0.0765 0.2288 1.0000
10.250 1.4709 0.01789 0.01139 -0.0747 0.2245 1.0000
10.500 1.4883 0.01834 0.01187 -0.0731 0.2205 1.0000
10.750 1.5040 0.01893 0.01246 -0.0714 0.2160 1.0000
11.000 1.5177 0.01967 0.01320 -0.0697 0.2117 1.0000
11.250 1.5333 0.02036 0.01391 -0.0683 0.2082 1.0000
11.500 1.5489 0.02111 0.01468 -0.0670 0.2041 1.0000
11.750 1.5617 0.02206 0.01564 -0.0656 0.1995 1.0000
12.000 1.5736 0.02314 0.01672 -0.0643 0.1952 1.0000
12.250 1.5874 0.02416 0.01776 -0.0632 0.1906 1.0000
12.500 1.5979 0.02546 0.01907 -0.0621 0.1859 1.0000
12.750 1.6073 0.02691 0.02054 -0.0611 0.1818 1.0000
13.000 1.6182 0.02830 0.02195 -0.0602 0.1773 1.0000
13.250 1.6249 0.03008 0.02375 -0.0593 0.1725 1.0000
13.500 1.6316 0.03191 0.02560 -0.0585 0.1684 1.0000
13.750 1.6391 0.03371 0.02744 -0.0578 0.1644 1.0000
14.000 1.6428 0.03590 0.02966 -0.0571 0.1604 1.0000
14.250 1.6453 0.03824 0.03203 -0.0565 0.1570 1.0000
14.500 1.6499 0.04040 0.03423 -0.0559 0.1534 1.0000
14.750 1.6509 0.04294 0.03681 -0.0554 0.1497 1.0000
15.000 1.6478 0.04593 0.03983 -0.0549 0.1465 1.0000
15.250 1.6506 0.04839 0.04236 -0.0545 0.1436 1.0000
15.500 1.6510 0.05117 0.04519 -0.0543 0.1405 1.0000
15.750 1.6487 0.05426 0.04833 -0.0541 0.1376 1.0000
16.000 1.6452 0.05757 0.05169 -0.0540 0.1350 1.0000
16.250 1.6441 0.06067 0.05486 -0.0540 0.1321 1.0000
16.500 1.6401 0.06414 0.05837 -0.0541 0.1289 1.0000
16.750 1.6334 0.06795 0.06222 -0.0543 0.1260 1.0000
17.000 1.6301 0.07142 0.06575 -0.0545 0.1235 1.0000
17.250 1.6274 0.07484 0.06923 -0.0548 0.1208 1.0000
17.500 1.6216 0.07865 0.07309 -0.0552 0.1181 1.0000
17.750 1.6131 0.08286 0.07735 -0.0557 0.1158 1.0000
18.000 1.6122 0.08612 0.08068 -0.0561 0.1136 1.0000
18.250 1.6076 0.08991 0.08453 -0.0567 0.1112 1.0000
18.500 1.6023 0.09377 0.08844 -0.0573 0.1087 1.0000
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