ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: ONERA HOR12 AIRFOIL (hor12-il) Reynolds number: 500,000 Max Cl/Cd: 97.88 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hor12-il-500000-n5.txt Download as CSV file: xf-hor12-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.500 -0.8410 0.09722 0.09429 -0.0155 1.0005 0.0200
-14.250 -0.8771 0.08640 0.08332 -0.0223 1.0005 0.0201
-14.000 -0.9060 0.07744 0.07424 -0.0283 1.0005 0.0202
-13.750 -0.9340 0.06904 0.06573 -0.0342 1.0005 0.0202
-13.500 -0.9610 0.06096 0.05754 -0.0402 1.0005 0.0203
-13.250 -0.9897 0.05280 0.04926 -0.0466 1.0005 0.0203
-13.000 -1.0076 0.04368 0.03996 -0.0572 1.0005 0.0204
-12.750 -0.9989 0.03478 0.03079 -0.0716 1.0005 0.0206
-12.500 -0.9752 0.03049 0.02629 -0.0793 1.0005 0.0209
-12.250 -0.9511 0.02855 0.02423 -0.0822 1.0005 0.0213
-12.000 -0.9260 0.02704 0.02260 -0.0842 1.0005 0.0217
-11.750 -0.9003 0.02574 0.02119 -0.0859 1.0005 0.0222
-11.500 -0.8740 0.02456 0.01989 -0.0873 1.0005 0.0228
-11.250 -0.8472 0.02347 0.01868 -0.0885 1.0005 0.0234
-11.000 -0.8199 0.02252 0.01759 -0.0896 1.0005 0.0240
-10.750 -0.7921 0.02172 0.01665 -0.0905 1.0005 0.0245
-10.500 -0.7644 0.02075 0.01559 -0.0915 1.0005 0.0250
-10.250 -0.7365 0.01974 0.01451 -0.0926 1.0005 0.0256
-10.000 -0.7080 0.01895 0.01367 -0.0935 1.0005 0.0262
-9.750 -0.6794 0.01824 0.01289 -0.0943 1.0005 0.0268
-9.500 -0.6505 0.01759 0.01217 -0.0950 1.0005 0.0275
-9.250 -0.6215 0.01700 0.01150 -0.0957 1.0005 0.0282
-9.000 -0.5923 0.01649 0.01092 -0.0963 0.9993 0.0290
-8.750 -0.5576 0.01606 0.01038 -0.0980 0.9770 0.0296
-8.500 -0.5240 0.01517 0.00944 -0.0999 0.9600 0.0309
-8.250 -0.4933 0.01462 0.00883 -0.1007 0.9453 0.0318
-8.000 -0.4647 0.01419 0.00832 -0.1009 0.9299 0.0325
-7.750 -0.4368 0.01381 0.00784 -0.1010 0.9117 0.0332
-7.500 -0.4092 0.01347 0.00738 -0.1009 0.8932 0.0338
-7.250 -0.3811 0.01316 0.00696 -0.1008 0.8739 0.0344
-7.000 -0.3529 0.01289 0.00656 -0.1008 0.8534 0.0350
-6.750 -0.3243 0.01257 0.00612 -0.1009 0.8325 0.0361
-6.250 -0.2662 0.01209 0.00541 -0.1012 0.7946 0.0381
-6.000 -0.2368 0.01188 0.00511 -0.1014 0.7790 0.0394
-5.750 -0.2072 0.01170 0.00483 -0.1017 0.7646 0.0408
-5.500 -0.1774 0.01150 0.00456 -0.1020 0.7514 0.0430
-5.250 -0.1475 0.01131 0.00431 -0.1023 0.7394 0.0467
-5.000 -0.1177 0.01112 0.00408 -0.1026 0.7278 0.0525
-4.750 -0.0877 0.01093 0.00387 -0.1029 0.7164 0.0608
-4.500 -0.0577 0.01076 0.00369 -0.1033 0.7058 0.0709
-4.250 -0.0278 0.01063 0.00353 -0.1036 0.6958 0.0799
-4.000 0.0021 0.01051 0.00338 -0.1039 0.6854 0.0881
-3.750 0.0320 0.01041 0.00325 -0.1041 0.6754 0.0943
-3.250 0.0918 0.01024 0.00301 -0.1047 0.6545 0.1089
-3.000 0.1216 0.01017 0.00291 -0.1049 0.6445 0.1167
-2.750 0.1515 0.01010 0.00282 -0.1052 0.6342 0.1254
-2.500 0.1814 0.01004 0.00274 -0.1054 0.6245 0.1343
-2.250 0.2112 0.00998 0.00267 -0.1057 0.6152 0.1442
-2.000 0.2411 0.00992 0.00261 -0.1060 0.6057 0.1553
-1.750 0.2710 0.00987 0.00256 -0.1062 0.5964 0.1680
-1.500 0.3008 0.00983 0.00252 -0.1065 0.5864 0.1819
-1.250 0.3306 0.00979 0.00250 -0.1067 0.5770 0.1973
-1.000 0.3603 0.00978 0.00248 -0.1070 0.5672 0.2130
-0.750 0.3901 0.00976 0.00247 -0.1072 0.5569 0.2278
-0.500 0.4198 0.00975 0.00247 -0.1074 0.5473 0.2435
-0.250 0.4495 0.00973 0.00247 -0.1077 0.5372 0.2619
0.000 0.4792 0.00970 0.00249 -0.1080 0.5270 0.2815
0.250 0.5089 0.00969 0.00252 -0.1082 0.5172 0.3081
0.500 0.5384 0.00970 0.00256 -0.1085 0.5071 0.3344
0.750 0.5680 0.00972 0.00262 -0.1087 0.4979 0.3577
1.000 0.5974 0.00977 0.00269 -0.1089 0.4885 0.3839
1.250 0.6269 0.00980 0.00276 -0.1091 0.4795 0.4051
1.500 0.6561 0.00988 0.00284 -0.1092 0.4708 0.4224
1.750 0.6855 0.00994 0.00292 -0.1094 0.4613 0.4394
2.000 0.7147 0.01002 0.00301 -0.1095 0.4528 0.4554
2.250 0.7439 0.01010 0.00310 -0.1097 0.4432 0.4703
2.500 0.7730 0.01018 0.00320 -0.1098 0.4334 0.4849
2.750 0.8020 0.01029 0.00331 -0.1099 0.4229 0.5007
3.000 0.8309 0.01039 0.00341 -0.1100 0.4113 0.5152
3.250 0.8598 0.01049 0.00354 -0.1102 0.4000 0.5305
3.500 0.8886 0.01060 0.00367 -0.1103 0.3897 0.5492
3.750 0.9174 0.01070 0.00381 -0.1104 0.3792 0.5725
4.000 0.9463 0.01075 0.00397 -0.1106 0.3697 0.6156
4.250 0.9728 0.01051 0.00422 -0.1102 0.3593 0.8035
4.500 0.9949 0.01031 0.00423 -0.1087 0.3488 0.9995
4.750 1.0234 0.01051 0.00439 -0.1087 0.3388 0.9995
5.000 1.0517 0.01075 0.00458 -0.1088 0.3275 0.9995
5.250 1.0796 0.01103 0.00479 -0.1088 0.3107 0.9995
5.500 1.1072 0.01134 0.00501 -0.1088 0.2922 0.9995
5.750 1.1347 0.01166 0.00526 -0.1088 0.2754 0.9995
6.000 1.1620 0.01200 0.00552 -0.1087 0.2584 0.9995
6.250 1.1889 0.01237 0.00580 -0.1086 0.2408 0.9995
6.500 1.2155 0.01279 0.00613 -0.1085 0.2226 0.9995
6.750 1.2420 0.01319 0.00646 -0.1083 0.2056 0.9995
7.000 1.2681 0.01363 0.00682 -0.1082 0.1885 0.9995
7.250 1.2937 0.01412 0.00723 -0.1079 0.1700 0.9995
7.500 1.3187 0.01466 0.00768 -0.1076 0.1511 0.9995
7.750 1.3431 0.01525 0.00817 -0.1072 0.1324 0.9995
8.000 1.3671 0.01586 0.00869 -0.1067 0.1140 0.9995
8.250 1.3903 0.01654 0.00928 -0.1062 0.0963 0.9995
8.500 1.4130 0.01723 0.00988 -0.1056 0.0812 0.9995
8.750 1.4353 0.01792 0.01051 -0.1049 0.0677 0.9995
9.000 1.4571 0.01863 0.01117 -0.1041 0.0573 0.9995
9.250 1.4783 0.01934 0.01185 -0.1032 0.0493 0.9995
9.500 1.4996 0.01999 0.01249 -0.1024 0.0445 0.9995
9.750 1.5202 0.02066 0.01317 -0.1014 0.0409 0.9995
10.000 1.5410 0.02126 0.01381 -0.1004 0.0384 0.9995
10.250 1.5605 0.02194 0.01452 -0.0993 0.0364 0.9995
10.500 1.5783 0.02270 0.01531 -0.0980 0.0346 0.9995
10.750 1.5960 0.02339 0.01605 -0.0966 0.0334 0.9995
11.000 1.6116 0.02416 0.01686 -0.0950 0.0321 0.9995
11.250 1.6248 0.02502 0.01776 -0.0931 0.0309 0.9995
11.500 1.6338 0.02599 0.01879 -0.0905 0.0297 0.9995
11.750 1.6393 0.02719 0.02004 -0.0877 0.0287 0.9995
12.000 1.6484 0.02830 0.02123 -0.0857 0.0281 0.9995
12.250 1.6568 0.02957 0.02260 -0.0838 0.0275 0.9995
12.500 1.6644 0.03102 0.02414 -0.0822 0.0268 0.9995
12.750 1.6709 0.03268 0.02588 -0.0808 0.0261 0.9995
13.000 1.6762 0.03458 0.02786 -0.0796 0.0254 0.9995
13.250 1.6799 0.03676 0.03012 -0.0787 0.0247 0.9995
13.500 1.6814 0.03931 0.03276 -0.0779 0.0241 0.9995
13.750 1.6817 0.04210 0.03564 -0.0774 0.0235 0.9995
14.000 1.6868 0.04442 0.03807 -0.0770 0.0230 0.9995
14.250 1.6900 0.04698 0.04074 -0.0767 0.0225 0.9995
14.500 1.6916 0.04980 0.04367 -0.0765 0.0218 0.9995
14.750 1.6917 0.05286 0.04683 -0.0764 0.0212 0.9995
15.000 1.6898 0.05617 0.05025 -0.0764 0.0206 0.9995
15.250 1.6863 0.05976 0.05393 -0.0766 0.0201 0.9995
15.500 1.6813 0.06360 0.05787 -0.0769 0.0196 0.9995
15.750 1.6744 0.06777 0.06213 -0.0774 0.0192 0.9995
16.000 1.6699 0.07172 0.06620 -0.0779 0.0187 0.9995
16.250 1.6648 0.07585 0.07045 -0.0786 0.0182 0.9995
16.500 1.6588 0.08017 0.07487 -0.0794 0.0177 0.9995
16.750 1.6520 0.08466 0.07947 -0.0803 0.0172 0.9995
17.000 1.6448 0.08932 0.08422 -0.0814 0.0167 0.9995
17.250 1.6369 0.09412 0.08912 -0.0826 0.0162 0.9995
17.500 1.6280 0.09912 0.09421 -0.0840 0.0157 0.9995
17.750 1.6190 0.10420 0.09939 -0.0855 0.0154 0.9995
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