ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: ONERA HOR12 AIRFOIL (hor12-il) Reynolds number: 200,000 Max Cl/Cd: 76.18 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hor12-il-200000-n5.txt Download as CSV file: xf-hor12-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: ONERA HOR12 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
------ -------- --------- --------- -------- -------- --------
-12.500 -0.5121 0.13457 0.13064 -0.0003 1.0005 0.0285
-12.250 -0.5250 0.12550 0.12157 -0.0045 1.0005 0.0294
-11.250 -0.8029 0.04578 0.04116 -0.0634 1.0005 0.0310
-11.000 -0.7895 0.03934 0.03442 -0.0748 1.0005 0.0315
-10.750 -0.7713 0.03606 0.03091 -0.0794 1.0005 0.0323
-10.500 -0.7506 0.03330 0.02789 -0.0828 1.0005 0.0332
-10.250 -0.7279 0.03087 0.02515 -0.0855 1.0005 0.0341
-10.000 -0.7033 0.02883 0.02280 -0.0875 1.0005 0.0349
-9.750 -0.6786 0.02711 0.02099 -0.0889 1.0005 0.0358
-9.500 -0.6524 0.02593 0.01976 -0.0900 1.0005 0.0368
-9.250 -0.6255 0.02482 0.01856 -0.0910 1.0005 0.0379
-9.000 -0.5983 0.02369 0.01729 -0.0920 1.0005 0.0391
-8.750 -0.5707 0.02258 0.01602 -0.0929 1.0005 0.0401
-8.500 -0.5429 0.02158 0.01486 -0.0937 1.0005 0.0410
-8.250 -0.5153 0.02060 0.01383 -0.0944 1.0005 0.0421
-8.000 -0.4878 0.01984 0.01304 -0.0951 1.0005 0.0435
-7.750 -0.4607 0.01917 0.01231 -0.0955 1.0005 0.0449
-7.500 -0.4289 0.01847 0.01151 -0.0968 0.9948 0.0465
-7.250 -0.3920 0.01776 0.01068 -0.0990 0.9826 0.0481
-7.000 -0.3556 0.01705 0.00990 -0.1012 0.9698 0.0502
-6.750 -0.3197 0.01646 0.00926 -0.1031 0.9569 0.0527
-6.500 -0.2852 0.01594 0.00865 -0.1046 0.9435 0.0555
-6.250 -0.2533 0.01545 0.00808 -0.1055 0.9276 0.0588
-6.000 -0.2231 0.01503 0.00762 -0.1059 0.9100 0.0637
-5.750 -0.1940 0.01467 0.00720 -0.1061 0.8920 0.0705
-5.500 -0.1655 0.01438 0.00683 -0.1060 0.8737 0.0793
-5.250 -0.1374 0.01412 0.00651 -0.1059 0.8557 0.0883
-5.000 -0.1092 0.01390 0.00622 -0.1057 0.8382 0.0964
-4.750 -0.0809 0.01374 0.00593 -0.1055 0.8216 0.1043
-4.500 -0.0524 0.01355 0.00569 -0.1055 0.8062 0.1124
-4.250 -0.0237 0.01342 0.00544 -0.1054 0.7916 0.1198
-4.000 0.0051 0.01328 0.00523 -0.1055 0.7781 0.1284
-3.750 0.0341 0.01316 0.00504 -0.1055 0.7649 0.1378
-3.500 0.0634 0.01305 0.00487 -0.1056 0.7524 0.1471
-3.250 0.0927 0.01293 0.00471 -0.1058 0.7406 0.1567
-3.000 0.1220 0.01284 0.00457 -0.1059 0.7293 0.1683
-2.750 0.1515 0.01276 0.00445 -0.1061 0.7178 0.1813
-2.500 0.1809 0.01268 0.00435 -0.1062 0.7066 0.1948
-2.250 0.2103 0.01263 0.00426 -0.1064 0.6961 0.2095
-2.000 0.2398 0.01257 0.00419 -0.1065 0.6847 0.2255
-1.750 0.2693 0.01250 0.00412 -0.1067 0.6739 0.2417
-1.500 0.2987 0.01245 0.00405 -0.1069 0.6636 0.2589
-1.250 0.3282 0.01239 0.00401 -0.1071 0.6528 0.2765
-1.000 0.3578 0.01234 0.00398 -0.1073 0.6426 0.2943
-0.750 0.3871 0.01232 0.00398 -0.1074 0.6328 0.3155
-0.500 0.4166 0.01230 0.00399 -0.1076 0.6222 0.3391
-0.250 0.4459 0.01230 0.00402 -0.1078 0.6122 0.3630
0.000 0.4752 0.01233 0.00406 -0.1078 0.6021 0.3887
0.250 0.5045 0.01234 0.00412 -0.1080 0.5918 0.4125
0.500 0.5336 0.01240 0.00416 -0.1080 0.5818 0.4344
0.750 0.5627 0.01245 0.00422 -0.1081 0.5714 0.4548
1.000 0.5918 0.01249 0.00428 -0.1082 0.5611 0.4741
1.250 0.6206 0.01255 0.00434 -0.1082 0.5513 0.4928
1.500 0.6495 0.01259 0.00442 -0.1083 0.5409 0.5118
1.750 0.6783 0.01264 0.00450 -0.1083 0.5309 0.5317
2.000 0.7070 0.01269 0.00459 -0.1083 0.5211 0.5533
2.250 0.7357 0.01271 0.00470 -0.1084 0.5109 0.5786
2.500 0.7639 0.01274 0.00482 -0.1083 0.5015 0.6131
2.750 0.7913 0.01269 0.00497 -0.1080 0.4917 0.6746
3.000 0.8120 0.01236 0.00503 -0.1059 0.4829 0.8459
3.250 0.8383 0.01234 0.00502 -0.1053 0.4736 0.9995
3.500 0.8672 0.01253 0.00519 -0.1054 0.4633 0.9995
3.750 0.8958 0.01276 0.00535 -0.1055 0.4536 0.9995
4.000 0.9244 0.01297 0.00552 -0.1056 0.4432 0.9995
4.250 0.9528 0.01319 0.00573 -0.1056 0.4337 0.9995
4.750 1.0093 0.01367 0.00616 -0.1056 0.4147 0.9995
5.000 1.0371 0.01393 0.00640 -0.1056 0.4046 0.9995
5.250 1.0646 0.01421 0.00664 -0.1055 0.3931 0.9995
5.500 1.0922 0.01447 0.00690 -0.1054 0.3805 0.9995
5.750 1.1195 0.01476 0.00719 -0.1053 0.3681 0.9995
6.000 1.1465 0.01507 0.00748 -0.1051 0.3555 0.9995
6.250 1.1731 0.01540 0.00778 -0.1049 0.3413 0.9995
6.500 1.1994 0.01576 0.00810 -0.1047 0.3249 0.9995
6.750 1.2251 0.01616 0.00847 -0.1044 0.3065 0.9995
7.000 1.2505 0.01659 0.00885 -0.1041 0.2881 0.9995
7.250 1.2758 0.01703 0.00927 -0.1038 0.2724 0.9995
7.500 1.3007 0.01749 0.00972 -0.1034 0.2573 0.9995
7.750 1.3249 0.01802 0.01021 -0.1029 0.2402 0.9995
8.000 1.3482 0.01862 0.01076 -0.1024 0.2214 0.9995
8.250 1.3709 0.01926 0.01135 -0.1017 0.2014 0.9995
8.500 1.3923 0.02001 0.01204 -0.1010 0.1805 0.9995
8.750 1.4128 0.02082 0.01278 -0.1001 0.1605 0.9995
9.000 1.4322 0.02171 0.01359 -0.0991 0.1398 0.9995
9.250 1.4496 0.02272 0.01452 -0.0979 0.1203 0.9995
9.500 1.4662 0.02376 0.01551 -0.0965 0.1026 0.9995
9.750 1.4809 0.02488 0.01658 -0.0949 0.0878 0.9995
10.000 1.4942 0.02604 0.01772 -0.0932 0.0764 0.9995
10.250 1.5052 0.02724 0.01892 -0.0911 0.0682 0.9995
10.500 1.5145 0.02846 0.02018 -0.0889 0.0624 0.9995
10.750 1.5189 0.02980 0.02157 -0.0860 0.0587 0.9995
11.000 1.5248 0.03117 0.02304 -0.0836 0.0555 0.9995
11.250 1.5288 0.03283 0.02477 -0.0814 0.0527 0.9995
11.500 1.5302 0.03487 0.02686 -0.0795 0.0503 0.9995
11.750 1.5346 0.03680 0.02891 -0.0781 0.0485 0.9995
12.000 1.5386 0.03892 0.03114 -0.0770 0.0467 0.9995
12.250 1.5409 0.04131 0.03365 -0.0761 0.0451 0.9995
12.500 1.5412 0.04404 0.03647 -0.0755 0.0438 0.9995
12.750 1.5392 0.04714 0.03965 -0.0750 0.0426 0.9995
13.000 1.5355 0.05053 0.04313 -0.0747 0.0416 0.9995
13.250 1.5365 0.05344 0.04619 -0.0745 0.0407 0.9995
13.500 1.5358 0.05660 0.04948 -0.0744 0.0397 0.9995
13.750 1.5339 0.05994 0.05295 -0.0744 0.0388 0.9995
14.000 1.5310 0.06347 0.05660 -0.0745 0.0379 0.9995
14.250 1.5273 0.06713 0.06037 -0.0747 0.0371 0.9995
14.500 1.5227 0.07098 0.06434 -0.0751 0.0363 0.9995
14.750 1.5170 0.07508 0.06852 -0.0757 0.0356 0.9995
15.000 1.5100 0.07940 0.07292 -0.0764 0.0349 0.9995
15.250 1.5056 0.08346 0.07708 -0.0770 0.0342 0.9995
15.500 1.5029 0.08738 0.08114 -0.0778 0.0334 0.9995
15.750 1.4995 0.09144 0.08533 -0.0786 0.0327 0.9995
16.000 1.4957 0.09562 0.08962 -0.0796 0.0319 0.9995
16.250 1.4918 0.09988 0.09399 -0.0808 0.0312 0.9995
16.500 1.4875 0.10427 0.09847 -0.0821 0.0305 0.9995
16.750 1.4829 0.10873 0.10300 -0.0835 0.0298 0.9995
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