ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: ONERA HOR12 AIRFOIL (hor12-il) Reynolds number: 1,000,000 Max Cl/Cd: 121.35 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hor12-il-1000000.txt Download as CSV file: xf-hor12-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.250 -0.9782 0.08594 0.08346 -0.0227 1.0005 0.0185
-15.000 -1.0050 0.07767 0.07510 -0.0282 1.0005 0.0185
-14.750 -1.0396 0.06864 0.06596 -0.0345 1.0005 0.0185
-14.500 -1.0860 0.05803 0.05522 -0.0424 1.0005 0.0184
-14.250 -1.1500 0.04188 0.03880 -0.0591 1.0005 0.0181
-14.000 -1.1415 0.03082 0.02744 -0.0772 1.0005 0.0184
-13.750 -1.1172 0.02860 0.02511 -0.0807 1.0005 0.0188
-13.500 -1.0926 0.02711 0.02353 -0.0828 1.0005 0.0192
-13.250 -1.0673 0.02586 0.02218 -0.0844 1.0005 0.0197
-13.000 -1.0415 0.02477 0.02099 -0.0857 1.0005 0.0202
-12.750 -1.0150 0.02391 0.02003 -0.0867 1.0005 0.0205
-12.500 -0.9896 0.02239 0.01843 -0.0885 1.0005 0.0211
-12.250 -0.9622 0.02174 0.01775 -0.0893 1.0005 0.0216
-12.000 -0.9345 0.02123 0.01721 -0.0899 1.0005 0.0221
-11.750 -0.9066 0.02077 0.01671 -0.0904 1.0005 0.0227
-11.500 -0.8785 0.02025 0.01613 -0.0910 1.0005 0.0234
-11.250 -0.8503 0.01976 0.01557 -0.0916 1.0005 0.0240
-11.000 -0.8218 0.01932 0.01506 -0.0921 1.0005 0.0244
-10.750 -0.7931 0.01902 0.01468 -0.0926 1.0005 0.0247
-10.500 -0.7655 0.01731 0.01288 -0.0942 1.0005 0.0257
-10.250 -0.7368 0.01662 0.01217 -0.0950 1.0005 0.0264
-10.000 -0.7078 0.01606 0.01158 -0.0956 1.0005 0.0270
-9.750 -0.6786 0.01553 0.01099 -0.0963 1.0005 0.0277
-9.500 -0.6492 0.01504 0.01046 -0.0968 1.0005 0.0284
-9.250 -0.6198 0.01460 0.00996 -0.0974 1.0005 0.0290
-9.000 -0.5903 0.01428 0.00960 -0.0978 1.0005 0.0294
-8.750 -0.5603 0.01342 0.00865 -0.0988 1.0005 0.0303
-8.500 -0.5302 0.01268 0.00787 -0.0997 1.0005 0.0313
-8.250 -0.4957 0.01218 0.00734 -0.1013 0.9862 0.0323
-7.750 -0.4335 0.01151 0.00654 -0.1026 0.9506 0.0339
-7.500 -0.4062 0.01126 0.00620 -0.1024 0.9345 0.0344
-7.250 -0.3784 0.01102 0.00587 -0.1022 0.9161 0.0349
-7.000 -0.3504 0.01073 0.00547 -0.1021 0.8963 0.0355
-6.750 -0.3219 0.01043 0.00506 -0.1021 0.8761 0.0366
-6.500 -0.2929 0.01020 0.00474 -0.1022 0.8546 0.0378
-6.250 -0.2638 0.01002 0.00447 -0.1023 0.8333 0.0390
-6.000 -0.2345 0.00988 0.00422 -0.1024 0.8131 0.0402
-5.750 -0.2049 0.00976 0.00400 -0.1026 0.7953 0.0411
-5.500 -0.1751 0.00961 0.00376 -0.1028 0.7796 0.0424
-5.250 -0.1451 0.00945 0.00355 -0.1031 0.7656 0.0450
-5.000 -0.1151 0.00931 0.00336 -0.1034 0.7527 0.0481
-4.750 -0.0850 0.00914 0.00317 -0.1037 0.7407 0.0553
-4.500 -0.0549 0.00897 0.00300 -0.1041 0.7292 0.0676
-4.250 -0.0248 0.00882 0.00287 -0.1044 0.7174 0.0799
-4.000 0.0053 0.00871 0.00275 -0.1047 0.7062 0.0898
-3.750 0.0353 0.00861 0.00264 -0.1050 0.6956 0.0991
-3.500 0.0652 0.00855 0.00255 -0.1052 0.6851 0.1066
-3.250 0.0953 0.00846 0.00246 -0.1055 0.6754 0.1155
-2.750 0.1552 0.00834 0.00231 -0.1060 0.6560 0.1334
-2.500 0.1852 0.00827 0.00225 -0.1063 0.6463 0.1444
-2.250 0.2152 0.00822 0.00219 -0.1066 0.6364 0.1554
-2.000 0.2451 0.00817 0.00214 -0.1068 0.6271 0.1677
-1.500 0.3050 0.00808 0.00208 -0.1074 0.6075 0.1980
-1.250 0.3349 0.00806 0.00207 -0.1076 0.5979 0.2140
-1.000 0.3647 0.00804 0.00206 -0.1079 0.5877 0.2295
-0.500 0.4244 0.00802 0.00204 -0.1084 0.5676 0.2583
-0.250 0.4542 0.00799 0.00204 -0.1086 0.5575 0.2738
0.000 0.4840 0.00798 0.00205 -0.1089 0.5476 0.2933
0.250 0.5138 0.00796 0.00208 -0.1091 0.5370 0.3237
0.500 0.5437 0.00793 0.00211 -0.1094 0.5272 0.3544
0.750 0.5733 0.00794 0.00217 -0.1097 0.5171 0.3861
1.000 0.6029 0.00797 0.00223 -0.1099 0.5067 0.4138
1.250 0.6325 0.00800 0.00229 -0.1101 0.4975 0.4330
1.500 0.6619 0.00808 0.00235 -0.1102 0.4877 0.4502
1.750 0.6914 0.00814 0.00242 -0.1104 0.4763 0.4657
2.000 0.7207 0.00822 0.00248 -0.1106 0.4636 0.4784
2.250 0.7500 0.00830 0.00255 -0.1107 0.4530 0.4918
2.500 0.7794 0.00837 0.00263 -0.1109 0.4434 0.5058
2.750 0.8087 0.00844 0.00271 -0.1111 0.4343 0.5205
3.250 0.8672 0.00857 0.00289 -0.1114 0.4145 0.5591
3.500 0.8965 0.00861 0.00301 -0.1116 0.4046 0.5953
3.750 0.9257 0.00856 0.00317 -0.1119 0.3936 0.6917
4.000 0.9479 0.00802 0.00322 -0.1104 0.3846 0.9995
4.250 0.9769 0.00820 0.00333 -0.1105 0.3732 0.9995
4.500 1.0056 0.00839 0.00346 -0.1107 0.3598 0.9995
5.000 1.0629 0.00879 0.00374 -0.1109 0.3327 0.9995
5.250 1.0914 0.00901 0.00389 -0.1109 0.3188 0.9995
5.500 1.1197 0.00923 0.00406 -0.1110 0.3060 0.9995
5.750 1.1480 0.00946 0.00424 -0.1110 0.2931 0.9995
6.000 1.1760 0.00972 0.00443 -0.1111 0.2797 0.9995
6.250 1.2039 0.00999 0.00464 -0.1111 0.2655 0.9995
6.500 1.2315 0.01028 0.00488 -0.1111 0.2507 0.9995
6.750 1.2589 0.01060 0.00512 -0.1110 0.2348 0.9995
7.000 1.2859 0.01096 0.00540 -0.1109 0.2173 0.9995
7.250 1.3125 0.01137 0.00572 -0.1108 0.1972 0.9995
7.500 1.3385 0.01186 0.00608 -0.1106 0.1770 0.9995
7.750 1.3642 0.01234 0.00646 -0.1104 0.1563 0.9995
8.000 1.3889 0.01297 0.00694 -0.1101 0.1319 0.9995
8.250 1.4125 0.01370 0.00750 -0.1096 0.1052 0.9995
8.500 1.4351 0.01452 0.00813 -0.1090 0.0786 0.9995
8.750 1.4575 0.01532 0.00879 -0.1083 0.0589 0.9995
9.000 1.4807 0.01595 0.00935 -0.1077 0.0489 0.9995
9.250 1.5039 0.01654 0.00991 -0.1070 0.0435 0.9995
9.500 1.5278 0.01700 0.01038 -0.1065 0.0405 0.9995
9.750 1.5513 0.01747 0.01086 -0.1059 0.0382 0.9995
10.000 1.5736 0.01803 0.01142 -0.1051 0.0360 0.9995
10.250 1.5957 0.01858 0.01200 -0.1043 0.0343 0.9995
10.500 1.6180 0.01906 0.01251 -0.1035 0.0334 0.9995
10.750 1.6393 0.01960 0.01308 -0.1026 0.0324 0.9995
11.000 1.6594 0.02021 0.01371 -0.1016 0.0314 0.9995
11.250 1.6779 0.02090 0.01442 -0.1003 0.0303 0.9995
11.500 1.6940 0.02170 0.01526 -0.0986 0.0291 0.9995
11.750 1.7101 0.02240 0.01602 -0.0970 0.0284 0.9995
12.000 1.7262 0.02303 0.01671 -0.0954 0.0279 0.9995
12.250 1.7401 0.02375 0.01749 -0.0935 0.0273 0.9995
12.500 1.7490 0.02458 0.01837 -0.0908 0.0265 0.9995
12.750 1.7563 0.02561 0.01946 -0.0882 0.0258 0.9995
13.000 1.7621 0.02692 0.02081 -0.0858 0.0249 0.9995
13.250 1.7643 0.02866 0.02262 -0.0835 0.0240 0.9995
13.500 1.7713 0.03018 0.02422 -0.0820 0.0234 0.9995
13.750 1.7832 0.03135 0.02545 -0.0809 0.0229 0.9995
14.000 1.7930 0.03279 0.02697 -0.0799 0.0223 0.9995
14.250 1.8015 0.03443 0.02868 -0.0790 0.0215 0.9995
14.500 1.8081 0.03634 0.03064 -0.0782 0.0207 0.9995
14.750 1.8123 0.03858 0.03294 -0.0776 0.0200 0.9995
15.000 1.8124 0.04137 0.03579 -0.0770 0.0193 0.9995
15.250 1.8171 0.04368 0.03818 -0.0766 0.0188 0.9995
15.500 1.8209 0.04611 0.04070 -0.0763 0.0182 0.9995
15.750 1.8224 0.04889 0.04354 -0.0760 0.0175 0.9995
16.000 1.8218 0.05193 0.04666 -0.0759 0.0168 0.9995
16.250 1.8185 0.05533 0.05012 -0.0758 0.0161 0.9995
16.500 1.8119 0.05924 0.05410 -0.0760 0.0155 0.9995
16.750 1.8069 0.06302 0.05799 -0.0762 0.0151 0.9995
17.000 1.8004 0.06708 0.06214 -0.0766 0.0147 0.9995
17.250 1.7926 0.07142 0.06657 -0.0772 0.0142 0.9995
17.500 1.7838 0.07602 0.07125 -0.0780 0.0137 0.9995
17.750 1.7735 0.08086 0.07618 -0.0789 0.0133 0.9995
18.000 1.7609 0.08615 0.08156 -0.0801 0.0128 0.9995
18.250 1.7469 0.09176 0.08727 -0.0815 0.0124 0.9995
18.500 1.7361 0.09693 0.09255 -0.0828 0.0122 0.9995
18.750 1.7242 0.10230 0.09803 -0.0843 0.0119 0.9995
19.000 1.7117 0.10784 0.10367 -0.0860 0.0116 0.9995
19.250 1.6989 0.11353 0.10946 -0.0879 0.0113 0.9995
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