ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: ONERA HOR12 AIRFOIL (hor12-il) Reynolds number: 1,000,000 Max Cl/Cd: 108.75 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hor12-il-1000000-n5.txt Download as CSV file: xf-hor12-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.250 -1.0348 0.07782 0.07507 -0.0287 1.0005 0.0145
-15.000 -1.1037 0.06354 0.06060 -0.0391 1.0005 0.0141
-14.750 -1.2191 0.03380 0.03030 -0.0725 1.0005 0.0134
-14.500 -1.1987 0.02831 0.02454 -0.0816 1.0005 0.0136
-14.250 -1.1763 0.02619 0.02229 -0.0843 1.0005 0.0140
-14.000 -1.1523 0.02461 0.02063 -0.0862 1.0005 0.0145
-13.750 -1.1273 0.02337 0.01932 -0.0875 1.0005 0.0150
-13.500 -1.1015 0.02231 0.01819 -0.0886 1.0005 0.0155
-13.250 -1.0750 0.02138 0.01717 -0.0896 1.0005 0.0160
-13.000 -1.0482 0.02052 0.01623 -0.0905 1.0005 0.0164
-12.750 -1.0209 0.01973 0.01536 -0.0913 1.0005 0.0168
-12.500 -0.9933 0.01902 0.01461 -0.0920 1.0005 0.0174
-12.250 -0.9654 0.01845 0.01402 -0.0925 1.0005 0.0181
-12.000 -0.9372 0.01793 0.01347 -0.0931 1.0005 0.0187
-11.750 -0.9089 0.01746 0.01296 -0.0936 1.0005 0.0195
-11.500 -0.8804 0.01697 0.01242 -0.0941 1.0005 0.0201
-11.250 -0.8517 0.01648 0.01188 -0.0946 1.0005 0.0206
-11.000 -0.8229 0.01599 0.01137 -0.0952 1.0005 0.0211
-10.750 -0.7940 0.01558 0.01093 -0.0956 1.0005 0.0216
-10.500 -0.7649 0.01519 0.01051 -0.0961 1.0005 0.0222
-10.250 -0.7357 0.01481 0.01009 -0.0966 1.0005 0.0228
-10.000 -0.7025 0.01445 0.00968 -0.0978 0.9724 0.0234
-9.750 -0.6728 0.01416 0.00930 -0.0983 0.9517 0.0239
-9.500 -0.6453 0.01392 0.00898 -0.0982 0.9376 0.0243
-9.250 -0.6173 0.01366 0.00865 -0.0982 0.9227 0.0246
-9.000 -0.5895 0.01337 0.00827 -0.0981 0.9046 0.0249
-8.750 -0.5614 0.01292 0.00770 -0.0983 0.8849 0.0255
-8.500 -0.5330 0.01260 0.00728 -0.0985 0.8649 0.0262
-8.250 -0.5043 0.01235 0.00692 -0.0986 0.8443 0.0268
-8.000 -0.4753 0.01211 0.00657 -0.0988 0.8221 0.0273
-7.750 -0.4461 0.01189 0.00623 -0.0991 0.8004 0.0278
-7.500 -0.4166 0.01169 0.00591 -0.0993 0.7814 0.0282
-7.250 -0.3870 0.01149 0.00561 -0.0996 0.7650 0.0286
-7.000 -0.3573 0.01130 0.00533 -0.0999 0.7509 0.0289
-6.750 -0.3275 0.01113 0.00508 -0.1002 0.7386 0.0293
-6.500 -0.2977 0.01098 0.00485 -0.1005 0.7267 0.0296
-6.250 -0.2676 0.01073 0.00452 -0.1010 0.7152 0.0306
-6.000 -0.2376 0.01051 0.00425 -0.1013 0.7043 0.0314
-5.750 -0.2075 0.01033 0.00401 -0.1017 0.6942 0.0321
-5.500 -0.1775 0.01016 0.00379 -0.1020 0.6840 0.0328
-5.250 -0.1474 0.01002 0.00359 -0.1023 0.6748 0.0332
-5.000 -0.1174 0.00990 0.00341 -0.1026 0.6651 0.0337
-4.750 -0.0874 0.00977 0.00324 -0.1029 0.6555 0.0342
-4.500 -0.0573 0.00967 0.00309 -0.1032 0.6461 0.0347
-4.250 -0.0273 0.00957 0.00295 -0.1035 0.6356 0.0361
-4.000 0.0027 0.00946 0.00281 -0.1038 0.6254 0.0389
-3.750 0.0329 0.00930 0.00266 -0.1042 0.6157 0.0493
-3.500 0.0632 0.00914 0.00253 -0.1046 0.6061 0.0616
-3.250 0.0932 0.00905 0.00243 -0.1049 0.5973 0.0707
-3.000 0.1233 0.00897 0.00234 -0.1052 0.5884 0.0786
-2.750 0.1533 0.00889 0.00227 -0.1055 0.5796 0.0875
-2.500 0.1832 0.00885 0.00220 -0.1057 0.5695 0.0934
-2.250 0.2132 0.00879 0.00215 -0.1060 0.5603 0.1014
-2.000 0.2431 0.00875 0.00210 -0.1063 0.5509 0.1097
-1.750 0.2730 0.00871 0.00206 -0.1065 0.5408 0.1196
-1.500 0.3030 0.00867 0.00202 -0.1068 0.5311 0.1320
-1.000 0.3628 0.00860 0.00198 -0.1074 0.5107 0.1601
-0.750 0.3926 0.00858 0.00197 -0.1076 0.5013 0.1754
-0.500 0.4224 0.00858 0.00198 -0.1079 0.4917 0.1904
-0.250 0.4522 0.00857 0.00199 -0.1082 0.4834 0.2046
0.000 0.4819 0.00858 0.00200 -0.1084 0.4745 0.2176
0.250 0.5117 0.00859 0.00203 -0.1086 0.4660 0.2321
0.500 0.5413 0.00861 0.00205 -0.1089 0.4573 0.2480
0.750 0.5711 0.00860 0.00208 -0.1091 0.4489 0.2675
1.000 0.6008 0.00859 0.00213 -0.1094 0.4396 0.2975
1.250 0.6305 0.00858 0.00219 -0.1097 0.4315 0.3265
1.500 0.6600 0.00862 0.00225 -0.1099 0.4226 0.3515
1.750 0.6894 0.00868 0.00233 -0.1101 0.4099 0.3754
2.000 0.7187 0.00878 0.00241 -0.1103 0.3951 0.3927
2.250 0.7480 0.00886 0.00250 -0.1105 0.3842 0.4096
2.500 0.7773 0.00895 0.00259 -0.1107 0.3759 0.4258
2.750 0.8065 0.00902 0.00268 -0.1108 0.3677 0.4404
3.000 0.8356 0.00913 0.00278 -0.1110 0.3584 0.4537
3.250 0.8647 0.00923 0.00289 -0.1111 0.3482 0.4678
3.500 0.8937 0.00934 0.00300 -0.1112 0.3381 0.4809
3.750 0.9226 0.00948 0.00312 -0.1114 0.3266 0.4917
4.000 0.9513 0.00963 0.00326 -0.1115 0.3152 0.5041
4.250 0.9800 0.00979 0.00340 -0.1116 0.3019 0.5172
4.500 1.0084 0.01000 0.00357 -0.1117 0.2847 0.5324
4.750 1.0367 0.01021 0.00376 -0.1118 0.2668 0.5537
5.000 1.0650 0.01040 0.00397 -0.1120 0.2485 0.5963
5.250 1.0928 0.01034 0.00430 -0.1122 0.2278 0.7987
5.500 1.1147 0.01025 0.00444 -0.1107 0.2104 0.9995
5.750 1.1421 0.01062 0.00470 -0.1107 0.1918 0.9995
6.000 1.1695 0.01098 0.00497 -0.1107 0.1743 0.9995
6.250 1.1966 0.01135 0.00525 -0.1106 0.1579 0.9995
6.500 1.2234 0.01176 0.00557 -0.1105 0.1400 0.9995
6.750 1.2497 0.01222 0.00592 -0.1104 0.1223 0.9995
7.000 1.2758 0.01268 0.00628 -0.1102 0.1057 0.9995
7.250 1.3016 0.01318 0.00668 -0.1099 0.0888 0.9995
7.500 1.3271 0.01367 0.00709 -0.1096 0.0743 0.9995
7.750 1.3521 0.01420 0.00754 -0.1093 0.0616 0.9995
8.000 1.3771 0.01470 0.00797 -0.1089 0.0512 0.9995
8.250 1.4020 0.01518 0.00841 -0.1085 0.0442 0.9995
8.500 1.4269 0.01563 0.00883 -0.1081 0.0385 0.9995
8.750 1.4513 0.01611 0.00928 -0.1077 0.0341 0.9995
9.000 1.4759 0.01653 0.00970 -0.1072 0.0324 0.9995
9.250 1.4999 0.01698 0.01016 -0.1067 0.0308 0.9995
9.500 1.5235 0.01747 0.01064 -0.1061 0.0289 0.9995
9.750 1.5472 0.01789 0.01108 -0.1055 0.0281 0.9995
10.000 1.5705 0.01833 0.01155 -0.1049 0.0273 0.9995
10.250 1.5931 0.01881 0.01206 -0.1042 0.0265 0.9995
10.500 1.6149 0.01933 0.01260 -0.1033 0.0257 0.9995
10.750 1.6358 0.01989 0.01319 -0.1024 0.0249 0.9995
11.000 1.6557 0.02050 0.01382 -0.1013 0.0241 0.9995
11.250 1.6751 0.02109 0.01446 -0.1001 0.0235 0.9995
11.500 1.6947 0.02160 0.01501 -0.0990 0.0231 0.9995
11.750 1.7129 0.02216 0.01561 -0.0976 0.0226 0.9995
12.000 1.7296 0.02276 0.01626 -0.0961 0.0220 0.9995
12.250 1.7446 0.02343 0.01698 -0.0943 0.0213 0.9995
12.500 1.7555 0.02419 0.01778 -0.0919 0.0204 0.9995
12.750 1.7631 0.02515 0.01877 -0.0892 0.0195 0.9995
13.000 1.7724 0.02615 0.01983 -0.0871 0.0187 0.9995
13.250 1.7817 0.02726 0.02100 -0.0852 0.0178 0.9995
13.500 1.7902 0.02854 0.02232 -0.0835 0.0167 0.9995
14.000 1.8040 0.03168 0.02555 -0.0806 0.0147 0.9995
14.250 1.8098 0.03353 0.02745 -0.0795 0.0138 0.9995
14.500 1.8137 0.03566 0.02964 -0.0785 0.0128 0.9995
14.750 1.8171 0.03795 0.03200 -0.0778 0.0122 0.9995
15.000 1.8196 0.04044 0.03456 -0.0772 0.0116 0.9995
15.250 1.8205 0.04316 0.03736 -0.0767 0.0111 0.9995
15.500 1.8195 0.04616 0.04044 -0.0764 0.0106 0.9995
15.750 1.8168 0.04944 0.04380 -0.0762 0.0102 0.9995
16.000 1.8131 0.05289 0.04733 -0.0760 0.0098 0.9995
16.250 1.8087 0.05645 0.05099 -0.0761 0.0096 0.9995
16.500 1.8030 0.06025 0.05489 -0.0762 0.0093 0.9995
16.750 1.7961 0.06432 0.05906 -0.0765 0.0090 0.9995
17.000 1.7878 0.06867 0.06351 -0.0770 0.0088 0.9995
17.250 1.7787 0.07325 0.06819 -0.0777 0.0085 0.9995
17.500 1.7684 0.07811 0.07315 -0.0786 0.0082 0.9995
17.750 1.7570 0.08317 0.07831 -0.0797 0.0080 0.9995
18.000 1.7451 0.08841 0.08365 -0.0809 0.0078 0.9995
18.250 1.7339 0.09363 0.08897 -0.0822 0.0076 0.9995
18.500 1.7227 0.09887 0.09432 -0.0836 0.0074 0.9995
18.750 1.7110 0.10427 0.09982 -0.0852 0.0073 0.9995
19.000 1.6990 0.10978 0.10544 -0.0869 0.0071 0.9995
19.250 1.6871 0.11535 0.11111 -0.0888 0.0069 0.9995
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