ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: ONERA HOR12 AIRFOIL (hor12-il) Reynolds number: 500,000 Max Cl/Cd: 103.72 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hor12-il-500000.txt Download as CSV file: xf-hor12-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.500 -0.8414 0.06273 0.05982 -0.0412 1.0005 0.0270
-12.250 -0.8911 0.04954 0.04637 -0.0539 1.0005 0.0267
-12.000 -0.8932 0.04022 0.03678 -0.0691 1.0005 0.0269
-11.750 -0.8751 0.03506 0.03134 -0.0786 1.0005 0.0275
-11.500 -0.8554 0.03221 0.02825 -0.0824 1.0005 0.0282
-11.250 -0.8329 0.03002 0.02583 -0.0851 1.0005 0.0289
-11.000 -0.8079 0.02851 0.02410 -0.0870 1.0005 0.0294
-10.750 -0.7868 0.02526 0.02058 -0.0895 1.0005 0.0304
-10.500 -0.7613 0.02379 0.01906 -0.0907 1.0005 0.0313
-10.250 -0.7344 0.02268 0.01788 -0.0917 1.0005 0.0321
-10.000 -0.7068 0.02163 0.01672 -0.0927 1.0005 0.0330
-9.750 -0.6789 0.02064 0.01561 -0.0936 1.0005 0.0339
-9.500 -0.6504 0.01981 0.01465 -0.0943 1.0005 0.0347
-9.250 -0.6222 0.01840 0.01311 -0.0954 1.0005 0.0357
-9.000 -0.5937 0.01737 0.01204 -0.0963 1.0005 0.0369
-8.750 -0.5648 0.01677 0.01141 -0.0970 1.0005 0.0381
-8.500 -0.5357 0.01622 0.01082 -0.0976 1.0005 0.0394
-8.250 -0.5067 0.01574 0.01026 -0.0980 1.0005 0.0406
-8.000 -0.4779 0.01516 0.00961 -0.0985 1.0005 0.0417
-7.750 -0.4494 0.01429 0.00873 -0.0992 1.0005 0.0432
-7.500 -0.4206 0.01380 0.00823 -0.0997 0.9992 0.0444
-7.250 -0.3826 0.01329 0.00767 -0.1020 0.9914 0.0458
-7.000 -0.3450 0.01283 0.00715 -0.1041 0.9808 0.0471
-6.750 -0.3096 0.01249 0.00673 -0.1056 0.9663 0.0484
-6.500 -0.2782 0.01202 0.00620 -0.1063 0.9495 0.0503
-6.250 -0.2506 0.01170 0.00582 -0.1060 0.9309 0.0523
-6.000 -0.2236 0.01146 0.00551 -0.1055 0.9111 0.0544
-5.750 -0.1964 0.01125 0.00521 -0.1051 0.8915 0.0570
-5.500 -0.1682 0.01092 0.00483 -0.1050 0.8718 0.0624
-5.250 -0.1396 0.01065 0.00452 -0.1049 0.8526 0.0719
-5.000 -0.1108 0.01044 0.00429 -0.1049 0.8341 0.0860
-4.750 -0.0818 0.01031 0.00409 -0.1050 0.8169 0.0973
-4.500 -0.0527 0.01023 0.00393 -0.1050 0.8010 0.1063
-4.250 -0.0233 0.01013 0.00379 -0.1051 0.7866 0.1155
-4.000 0.0062 0.01005 0.00364 -0.1053 0.7731 0.1234
-3.750 0.0356 0.00999 0.00352 -0.1054 0.7605 0.1315
-3.500 0.0653 0.00990 0.00339 -0.1056 0.7482 0.1401
-3.250 0.0950 0.00984 0.00329 -0.1058 0.7359 0.1497
-3.000 0.1248 0.00975 0.00319 -0.1060 0.7246 0.1609
-2.750 0.1545 0.00969 0.00310 -0.1062 0.7138 0.1730
-2.500 0.1844 0.00961 0.00302 -0.1065 0.7027 0.1863
-2.250 0.2142 0.00956 0.00296 -0.1067 0.6925 0.2003
-2.000 0.2438 0.00954 0.00291 -0.1069 0.6824 0.2153
-1.750 0.2737 0.00948 0.00287 -0.1072 0.6718 0.2307
-1.500 0.3034 0.00945 0.00283 -0.1074 0.6619 0.2461
-1.250 0.3332 0.00941 0.00279 -0.1076 0.6515 0.2622
-1.000 0.3630 0.00935 0.00276 -0.1079 0.6412 0.2804
-0.750 0.3927 0.00932 0.00275 -0.1081 0.6312 0.3018
-0.500 0.4225 0.00928 0.00276 -0.1083 0.6207 0.3284
-0.250 0.4522 0.00925 0.00279 -0.1086 0.6105 0.3589
0.000 0.4817 0.00927 0.00283 -0.1088 0.6004 0.3888
0.250 0.5114 0.00926 0.00289 -0.1090 0.5897 0.4159
0.500 0.5409 0.00931 0.00293 -0.1091 0.5796 0.4382
0.750 0.5702 0.00936 0.00298 -0.1092 0.5693 0.4574
1.000 0.5997 0.00939 0.00303 -0.1094 0.5587 0.4761
1.250 0.6291 0.00945 0.00309 -0.1095 0.5488 0.4932
1.500 0.6584 0.00950 0.00314 -0.1097 0.5383 0.5090
1.750 0.6877 0.00954 0.00321 -0.1098 0.5280 0.5259
2.000 0.7169 0.00959 0.00328 -0.1099 0.5182 0.5442
2.250 0.7462 0.00963 0.00335 -0.1101 0.5077 0.5656
2.500 0.7754 0.00964 0.00345 -0.1103 0.4973 0.5946
2.750 0.8043 0.00962 0.00357 -0.1104 0.4869 0.6531
3.000 0.8273 0.00916 0.00370 -0.1090 0.4764 0.8670
3.250 0.8531 0.00908 0.00366 -0.1083 0.4659 0.9995
3.500 0.8821 0.00926 0.00377 -0.1084 0.4554 0.9995
3.750 0.9113 0.00940 0.00388 -0.1086 0.4447 0.9995
4.000 0.9402 0.00957 0.00400 -0.1087 0.4349 0.9995
4.250 0.9688 0.00978 0.00414 -0.1088 0.4243 0.9995
4.500 0.9977 0.00993 0.00429 -0.1089 0.4137 0.9995
4.750 1.0263 0.01013 0.00444 -0.1089 0.4039 0.9995
5.000 1.0546 0.01036 0.00462 -0.1090 0.3930 0.9995
5.250 1.0829 0.01055 0.00478 -0.1090 0.3795 0.9995
5.500 1.1111 0.01077 0.00496 -0.1090 0.3657 0.9995
5.750 1.1391 0.01100 0.00516 -0.1090 0.3529 0.9995
6.000 1.1669 0.01125 0.00537 -0.1090 0.3403 0.9995
6.250 1.1945 0.01152 0.00560 -0.1090 0.3271 0.9995
6.500 1.2219 0.01182 0.00585 -0.1089 0.3137 0.9995
6.750 1.2492 0.01210 0.00611 -0.1088 0.3005 0.9995
7.000 1.2764 0.01240 0.00639 -0.1087 0.2869 0.9995
7.250 1.3031 0.01274 0.00669 -0.1086 0.2717 0.9995
7.500 1.3294 0.01312 0.00702 -0.1084 0.2556 0.9995
7.750 1.3552 0.01356 0.00739 -0.1081 0.2383 0.9995
8.000 1.3806 0.01402 0.00779 -0.1078 0.2196 0.9995
8.250 1.4053 0.01456 0.00825 -0.1074 0.1983 0.9995
8.500 1.4289 0.01522 0.00878 -0.1069 0.1755 0.9995
8.750 1.4511 0.01600 0.00941 -0.1063 0.1487 0.9995
9.000 1.4715 0.01696 0.01018 -0.1054 0.1179 0.9995
9.250 1.4897 0.01811 0.01112 -0.1043 0.0869 0.9995
9.500 1.5074 0.01921 0.01208 -0.1030 0.0672 0.9995
9.750 1.5260 0.02014 0.01296 -0.1018 0.0579 0.9995
10.000 1.5449 0.02096 0.01378 -0.1006 0.0532 0.9995
10.250 1.5615 0.02192 0.01476 -0.0991 0.0497 0.9995
10.500 1.5800 0.02262 0.01553 -0.0978 0.0478 0.9995
10.750 1.5961 0.02344 0.01640 -0.0962 0.0457 0.9995
11.000 1.6084 0.02442 0.01741 -0.0941 0.0437 0.9995
11.250 1.6134 0.02577 0.01881 -0.0911 0.0418 0.9995
11.500 1.6237 0.02661 0.01974 -0.0887 0.0409 0.9995
11.750 1.6327 0.02766 0.02088 -0.0865 0.0397 0.9995
12.000 1.6407 0.02890 0.02220 -0.0845 0.0385 0.9995
12.250 1.6475 0.03037 0.02374 -0.0827 0.0374 0.9995
12.500 1.6516 0.03220 0.02563 -0.0810 0.0363 0.9995
12.750 1.6507 0.03467 0.02817 -0.0795 0.0352 0.9995
13.000 1.6511 0.03721 0.03083 -0.0784 0.0343 0.9995
13.250 1.6575 0.03925 0.03298 -0.0777 0.0335 0.9995
13.500 1.6614 0.04164 0.03547 -0.0772 0.0327 0.9995
13.750 1.6641 0.04423 0.03815 -0.0768 0.0318 0.9995
14.000 1.6646 0.04714 0.04114 -0.0765 0.0310 0.9995
14.250 1.6614 0.05055 0.04462 -0.0764 0.0302 0.9995
14.500 1.6529 0.05465 0.04881 -0.0764 0.0294 0.9995
14.750 1.6388 0.05948 0.05373 -0.0765 0.0287 0.9995
15.000 1.6379 0.06279 0.05717 -0.0766 0.0282 0.9995
15.250 1.6352 0.06637 0.06086 -0.0769 0.0277 0.9995
15.500 1.6314 0.07020 0.06481 -0.0773 0.0270 0.9995
15.750 1.6264 0.07427 0.06899 -0.0779 0.0264 0.9995
16.000 1.6205 0.07855 0.07336 -0.0787 0.0258 0.9995
16.250 1.6138 0.08300 0.07790 -0.0796 0.0253 0.9995
16.500 1.6057 0.08773 0.08270 -0.0806 0.0248 0.9995
16.750 1.5953 0.09279 0.08783 -0.0818 0.0243 0.9995
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