WORTMANN FX 60-126 AIRFOIL (fx60126-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 60-126 AIRFOIL (fx60126-il) Reynolds number: 500,000 Max Cl/Cd: 88.35 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx60126-il-500000-n5.txt Download as CSV file: xf-fx60126-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 60-126 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
------ -------- --------- --------- -------- -------- --------
-13.750 -0.6176 0.08691 0.08397 -0.0493 1.0000 0.0068
-13.500 -0.6562 0.07501 0.07183 -0.0565 1.0000 0.0066
-13.250 -0.6726 0.06821 0.06491 -0.0608 1.0000 0.0066
-13.000 -0.6890 0.06198 0.05857 -0.0647 1.0000 0.0066
-12.750 -0.7032 0.05643 0.05290 -0.0681 1.0000 0.0066
-12.500 -0.7169 0.05134 0.04769 -0.0712 1.0000 0.0066
-12.250 -0.7265 0.04710 0.04334 -0.0736 1.0000 0.0066
-12.000 -0.7362 0.04322 0.03934 -0.0755 1.0000 0.0066
-11.750 -0.7452 0.03988 0.03591 -0.0766 1.0000 0.0066
-11.500 -0.7581 0.03706 0.03302 -0.0763 1.0000 0.0065
-11.250 -0.7592 0.03379 0.02963 -0.0793 0.9954 0.0066
-11.000 -0.7356 0.02993 0.02557 -0.0873 0.9864 0.0066
-10.750 -0.7068 0.02705 0.02249 -0.0940 0.9806 0.0067
-10.500 -0.6797 0.02503 0.02032 -0.0977 0.9748 0.0068
-10.250 -0.6498 0.02332 0.01846 -0.1011 0.9708 0.0069
-10.000 -0.6223 0.02190 0.01691 -0.1033 0.9650 0.0070
-9.750 -0.5935 0.02061 0.01550 -0.1054 0.9594 0.0072
-9.500 -0.5631 0.01946 0.01423 -0.1075 0.9550 0.0073
-9.250 -0.5370 0.01849 0.01316 -0.1083 0.9468 0.0075
-9.000 -0.5083 0.01754 0.01209 -0.1095 0.9401 0.0077
-8.750 -0.4826 0.01673 0.01118 -0.1100 0.9312 0.0078
-8.500 -0.4553 0.01597 0.01031 -0.1105 0.9242 0.0081
-8.250 -0.4295 0.01531 0.00955 -0.1107 0.9156 0.0082
-8.000 -0.4024 0.01472 0.00885 -0.1110 0.9087 0.0085
-7.750 -0.3761 0.01407 0.00812 -0.1112 0.9004 0.0087
-7.250 -0.3216 0.01299 0.00688 -0.1116 0.8859 0.0095
-7.000 -0.2940 0.01258 0.00637 -0.1118 0.8788 0.0099
-6.750 -0.2663 0.01219 0.00591 -0.1119 0.8713 0.0105
-6.500 -0.2383 0.01186 0.00549 -0.1120 0.8643 0.0112
-6.250 -0.2102 0.01145 0.00504 -0.1122 0.8579 0.0127
-6.000 -0.1819 0.01109 0.00463 -0.1124 0.8514 0.0153
-5.750 -0.1536 0.01068 0.00422 -0.1126 0.8454 0.0228
-5.500 -0.1252 0.01032 0.00389 -0.1129 0.8379 0.0377
-5.000 -0.0682 0.00978 0.00336 -0.1132 0.8220 0.0620
-4.750 -0.0397 0.00955 0.00311 -0.1134 0.8143 0.0767
-4.500 -0.0110 0.00914 0.00284 -0.1138 0.8061 0.1139
-4.250 0.0177 0.00878 0.00260 -0.1141 0.7988 0.1562
-4.000 0.0466 0.00849 0.00241 -0.1145 0.7909 0.1930
-3.750 0.0753 0.00831 0.00225 -0.1146 0.7826 0.2169
-3.500 0.1041 0.00815 0.00212 -0.1148 0.7726 0.2439
-3.250 0.1328 0.00803 0.00201 -0.1148 0.7620 0.2653
-3.000 0.1613 0.00794 0.00191 -0.1149 0.7508 0.2885
-2.750 0.1900 0.00787 0.00183 -0.1149 0.7393 0.3074
-2.500 0.2186 0.00781 0.00177 -0.1150 0.7283 0.3259
-2.250 0.2471 0.00777 0.00173 -0.1150 0.7167 0.3504
-2.000 0.2755 0.00775 0.00170 -0.1150 0.7038 0.3705
-1.500 0.3322 0.00780 0.00165 -0.1149 0.6760 0.3939
-1.250 0.3603 0.00784 0.00164 -0.1148 0.6610 0.4039
-1.000 0.3882 0.00791 0.00164 -0.1147 0.6434 0.4150
-0.750 0.4160 0.00799 0.00165 -0.1145 0.6234 0.4267
-0.500 0.4436 0.00808 0.00168 -0.1144 0.6032 0.4378
-0.250 0.4713 0.00818 0.00171 -0.1142 0.5853 0.4475
0.000 0.4992 0.00827 0.00175 -0.1141 0.5696 0.4565
0.250 0.5270 0.00837 0.00180 -0.1140 0.5548 0.4642
0.500 0.5549 0.00847 0.00186 -0.1139 0.5408 0.4718
0.750 0.5826 0.00859 0.00192 -0.1138 0.5253 0.4790
1.000 0.6103 0.00870 0.00199 -0.1137 0.5104 0.4872
1.250 0.6381 0.00880 0.00207 -0.1136 0.4979 0.4955
1.500 0.6657 0.00892 0.00215 -0.1135 0.4849 0.5037
1.750 0.6934 0.00904 0.00225 -0.1134 0.4723 0.5111
2.000 0.7211 0.00916 0.00235 -0.1133 0.4594 0.5199
2.250 0.7484 0.00930 0.00247 -0.1132 0.4430 0.5286
2.500 0.7754 0.00948 0.00260 -0.1130 0.4256 0.5373
2.750 0.8025 0.00965 0.00273 -0.1128 0.4105 0.5447
3.000 0.8296 0.00982 0.00287 -0.1126 0.3958 0.5529
3.250 0.8564 0.01000 0.00303 -0.1124 0.3793 0.5605
3.750 0.9094 0.01044 0.00338 -0.1119 0.3453 0.5773
4.000 0.9358 0.01067 0.00358 -0.1117 0.3293 0.5872
4.250 0.9621 0.01089 0.00379 -0.1114 0.3121 0.5981
4.500 0.9878 0.01118 0.00402 -0.1111 0.2921 0.6087
4.750 1.0132 0.01149 0.00428 -0.1107 0.2728 0.6193
5.000 1.0383 0.01181 0.00455 -0.1103 0.2500 0.6299
5.250 1.0633 0.01215 0.00484 -0.1099 0.2315 0.6411
5.500 1.0885 0.01245 0.00513 -0.1095 0.2164 0.6533
5.750 1.1132 0.01279 0.00545 -0.1090 0.1980 0.6664
6.250 1.1618 0.01351 0.00614 -0.1080 0.1692 0.6978
6.750 1.2080 0.01434 0.00696 -0.1066 0.1351 0.7444
7.000 1.2303 0.01472 0.00739 -0.1058 0.1240 0.7822
7.250 1.2479 0.01477 0.00770 -0.1037 0.1153 0.8821
7.500 1.2692 0.01513 0.00807 -0.1026 0.1045 1.0000
7.750 1.2917 0.01560 0.00850 -0.1019 0.0966 1.0000
8.000 1.3144 0.01605 0.00893 -0.1012 0.0914 1.0000
8.250 1.3361 0.01654 0.00942 -0.1003 0.0863 1.0000
8.500 1.3590 0.01691 0.00983 -0.0996 0.0827 1.0000
8.750 1.3806 0.01736 0.01030 -0.0987 0.0765 1.0000
9.000 1.4008 0.01788 0.01082 -0.0977 0.0703 1.0000
9.250 1.4199 0.01846 0.01137 -0.0965 0.0637 1.0000
9.500 1.4384 0.01903 0.01195 -0.0952 0.0601 1.0000
9.750 1.4546 0.01964 0.01256 -0.0935 0.0569 1.0000
10.000 1.4687 0.02030 0.01324 -0.0915 0.0536 1.0000
10.250 1.4840 0.02088 0.01387 -0.0897 0.0516 1.0000
10.500 1.4992 0.02146 0.01452 -0.0879 0.0493 1.0000
10.750 1.5126 0.02218 0.01529 -0.0861 0.0464 1.0000
11.000 1.5238 0.02305 0.01619 -0.0840 0.0436 1.0000
11.250 1.5368 0.02383 0.01703 -0.0823 0.0413 1.0000
11.500 1.5493 0.02468 0.01792 -0.0806 0.0388 1.0000
11.750 1.5601 0.02568 0.01894 -0.0789 0.0363 1.0000
12.000 1.5702 0.02676 0.02006 -0.0772 0.0342 1.0000
12.250 1.5804 0.02787 0.02124 -0.0756 0.0327 1.0000
12.500 1.5898 0.02909 0.02251 -0.0741 0.0312 1.0000
12.750 1.5979 0.03046 0.02393 -0.0726 0.0298 1.0000
13.000 1.6048 0.03199 0.02551 -0.0712 0.0284 1.0000
13.250 1.6129 0.03347 0.02708 -0.0700 0.0274 1.0000
13.500 1.6202 0.03506 0.02876 -0.0688 0.0265 1.0000
13.750 1.6265 0.03683 0.03061 -0.0678 0.0254 1.0000
14.000 1.6314 0.03879 0.03265 -0.0669 0.0242 1.0000
14.250 1.6343 0.04103 0.03495 -0.0661 0.0230 1.0000
14.500 1.6382 0.04325 0.03727 -0.0655 0.0220 1.0000
14.750 1.6422 0.04555 0.03966 -0.0650 0.0209 1.0000
15.000 1.6443 0.04813 0.04233 -0.0647 0.0197 1.0000
15.250 1.6443 0.05106 0.04534 -0.0646 0.0184 1.0000
15.500 1.6442 0.05413 0.04851 -0.0647 0.0171 1.0000
15.750 1.6439 0.05735 0.05182 -0.0650 0.0154 1.0000
16.000 1.6408 0.06106 0.05561 -0.0655 0.0135 1.0000
16.250 1.6352 0.06528 0.05990 -0.0664 0.0106 1.0000
16.500 1.6248 0.07035 0.06504 -0.0677 0.0081 1.0000
16.750 1.6150 0.07552 0.07032 -0.0693 0.0071 1.0000
17.000 1.6037 0.08113 0.07604 -0.0712 0.0063 1.0000
17.250 1.5935 0.08672 0.08177 -0.0733 0.0058 1.0000
17.500 1.5821 0.09267 0.08785 -0.0756 0.0055 1.0000
17.750 1.5701 0.09887 0.09418 -0.0783 0.0052 1.0000
18.000 1.5574 0.10536 0.10082 -0.0812 0.0050 1.0000
18.250 1.5446 0.11202 0.10761 -0.0844 0.0048 1.0000
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