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