GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 493 AIRFOIL (goe493-il) Reynolds number: 1,000,000 Max Cl/Cd: 127.09 at α=4.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe493-il-1000000.txt Download as CSV file: xf-goe493-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 493 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
------ -------- --------- --------- -------- -------- --------
-17.250 -0.8278 0.08508 0.08209 -0.0746 1.0000 0.0113
-17.000 -0.8431 0.07933 0.07625 -0.0774 1.0000 0.0114
-16.750 -0.8602 0.07358 0.07041 -0.0801 1.0000 0.0114
-16.500 -0.8751 0.06822 0.06496 -0.0826 1.0000 0.0114
-16.250 -0.8929 0.06281 0.05945 -0.0851 1.0000 0.0115
-16.000 -0.9078 0.05796 0.05451 -0.0871 1.0000 0.0115
-15.750 -0.9205 0.05355 0.05000 -0.0888 1.0000 0.0116
-15.500 -0.9347 0.04924 0.04560 -0.0902 1.0000 0.0116
-15.250 -0.9472 0.04544 0.04172 -0.0911 1.0000 0.0116
-15.000 -0.9629 0.04174 0.03793 -0.0914 1.0000 0.0117
-14.750 -0.9799 0.03861 0.03472 -0.0906 1.0000 0.0117
-14.500 -0.9777 0.03456 0.03054 -0.0949 0.9986 0.0118
-14.250 -0.9736 0.02983 0.02566 -0.1011 0.9955 0.0122
-14.000 -0.9602 0.02701 0.02273 -0.1051 0.9921 0.0123
-13.750 -0.9436 0.02497 0.02059 -0.1079 0.9881 0.0127
-13.500 -0.9226 0.02337 0.01890 -0.1105 0.9851 0.0129
-13.250 -0.8983 0.02208 0.01754 -0.1128 0.9831 0.0132
-13.000 -0.8814 0.02108 0.01646 -0.1129 0.9773 0.0136
-12.750 -0.8581 0.02011 0.01542 -0.1138 0.9740 0.0140
-12.500 -0.8297 0.01937 0.01459 -0.1153 0.9719 0.0144
-12.250 -0.8002 0.01826 0.01339 -0.1175 0.9702 0.0149
-12.000 -0.7829 0.01723 0.01230 -0.1170 0.9628 0.0155
-11.750 -0.7539 0.01650 0.01151 -0.1184 0.9593 0.0161
-11.500 -0.7223 0.01584 0.01079 -0.1201 0.9562 0.0168
-11.250 -0.7026 0.01536 0.01024 -0.1192 0.9484 0.0173
-11.000 -0.6747 0.01488 0.00969 -0.1199 0.9435 0.0178
-10.750 -0.6569 0.01418 0.00891 -0.1187 0.9360 0.0189
-10.500 -0.6346 0.01370 0.00839 -0.1181 0.9296 0.0198
-10.250 -0.6107 0.01333 0.00795 -0.1178 0.9240 0.0209
-10.000 -0.5898 0.01301 0.00758 -0.1167 0.9175 0.0218
-9.750 -0.5680 0.01251 0.00703 -0.1160 0.9118 0.0236
-9.500 -0.5460 0.01219 0.00666 -0.1151 0.9062 0.0253
-9.250 -0.5248 0.01179 0.00623 -0.1141 0.9003 0.0278
-9.000 -0.5007 0.01146 0.00586 -0.1136 0.8951 0.0308
-8.750 -0.4795 0.01107 0.00548 -0.1125 0.8897 0.0355
-8.500 -0.4573 0.01071 0.00513 -0.1117 0.8842 0.0419
-8.250 -0.4335 0.01038 0.00479 -0.1111 0.8792 0.0505
-8.000 -0.4105 0.01007 0.00452 -0.1104 0.8742 0.0603
-7.750 -0.3868 0.00980 0.00428 -0.1097 0.8690 0.0701
-7.500 -0.3617 0.00957 0.00406 -0.1093 0.8642 0.0790
-7.250 -0.3365 0.00939 0.00387 -0.1089 0.8594 0.0863
-7.000 -0.3114 0.00921 0.00371 -0.1084 0.8543 0.0931
-6.750 -0.2857 0.00904 0.00352 -0.1081 0.8494 0.0999
-6.500 -0.2596 0.00890 0.00335 -0.1078 0.8446 0.1060
-6.250 -0.2343 0.00873 0.00319 -0.1074 0.8394 0.1124
-6.000 -0.2084 0.00858 0.00303 -0.1070 0.8343 0.1194
-5.750 -0.1821 0.00844 0.00287 -0.1068 0.8295 0.1272
-5.500 -0.1565 0.00829 0.00274 -0.1064 0.8241 0.1360
-5.250 -0.1310 0.00811 0.00259 -0.1060 0.8186 0.1477
-5.000 -0.1050 0.00796 0.00245 -0.1057 0.8133 0.1604
-4.750 -0.0795 0.00778 0.00232 -0.1053 0.8078 0.1766
-4.500 -0.0538 0.00762 0.00220 -0.1049 0.8021 0.1946
-4.250 -0.0279 0.00748 0.00208 -0.1045 0.7965 0.2130
-4.000 -0.0026 0.00730 0.00197 -0.1041 0.7902 0.2352
-3.750 0.0232 0.00716 0.00186 -0.1037 0.7842 0.2584
-3.500 0.0487 0.00698 0.00178 -0.1033 0.7783 0.2857
-3.250 0.0743 0.00684 0.00170 -0.1029 0.7718 0.3130
-3.000 0.1001 0.00673 0.00163 -0.1025 0.7656 0.3396
-2.750 0.1259 0.00662 0.00158 -0.1022 0.7586 0.3638
-2.500 0.1518 0.00655 0.00153 -0.1017 0.7519 0.3886
-2.250 0.1779 0.00646 0.00150 -0.1014 0.7444 0.4098
-2.000 0.2035 0.00643 0.00147 -0.1009 0.7362 0.4284
-1.750 0.2296 0.00638 0.00145 -0.1005 0.7275 0.4451
-1.500 0.2553 0.00638 0.00142 -0.1001 0.7189 0.4607
-1.250 0.2814 0.00635 0.00142 -0.0997 0.7100 0.4767
-1.000 0.3072 0.00635 0.00141 -0.0992 0.7017 0.4913
-0.750 0.3331 0.00635 0.00141 -0.0988 0.6926 0.5049
-0.500 0.3587 0.00635 0.00142 -0.0983 0.6838 0.5190
-0.250 0.3839 0.00637 0.00143 -0.0977 0.6742 0.5326
0.000 0.4096 0.00637 0.00146 -0.0973 0.6653 0.5484
0.250 0.4345 0.00640 0.00148 -0.0967 0.6564 0.5632
0.500 0.4606 0.00641 0.00151 -0.0963 0.6484 0.5762
0.750 0.4856 0.00646 0.00154 -0.0957 0.6407 0.5897
1.000 0.5116 0.00645 0.00158 -0.0953 0.6333 0.6040
1.250 0.5362 0.00649 0.00162 -0.0946 0.6257 0.6191
1.500 0.5617 0.00648 0.00167 -0.0942 0.6185 0.6363
1.750 0.5859 0.00651 0.00173 -0.0934 0.6107 0.6569
2.000 0.6105 0.00650 0.00180 -0.0927 0.6034 0.6801
2.250 0.6343 0.00653 0.00187 -0.0919 0.5957 0.7050
2.500 0.6583 0.00654 0.00195 -0.0911 0.5891 0.7314
3.000 0.7047 0.00659 0.00212 -0.0891 0.5732 0.7841
3.250 0.7266 0.00663 0.00221 -0.0878 0.5634 0.8096
3.500 0.7486 0.00664 0.00230 -0.0865 0.5535 0.8379
3.750 0.7690 0.00667 0.00240 -0.0849 0.5435 0.8726
4.000 0.7987 0.00672 0.00256 -0.0853 0.5292 0.9271
4.250 0.8608 0.00695 0.00278 -0.0931 0.5125 0.9638
4.500 0.9111 0.00718 0.00296 -0.0983 0.4967 0.9852
4.750 0.9430 0.00742 0.00314 -0.0995 0.4775 1.0000
5.000 0.9586 0.00763 0.00327 -0.0970 0.4571 1.0000
5.250 0.9726 0.00790 0.00343 -0.0942 0.4347 1.0000
5.500 0.9864 0.00817 0.00361 -0.0914 0.4108 1.0000
5.750 0.9953 0.00850 0.00381 -0.0876 0.3847 1.0000
6.000 1.0060 0.00884 0.00404 -0.0843 0.3604 1.0000
6.250 1.0168 0.00924 0.00431 -0.0810 0.3353 1.0000
6.500 1.0298 0.00962 0.00460 -0.0782 0.3139 1.0000
6.750 1.0428 0.01003 0.00490 -0.0755 0.2916 1.0000
7.000 1.0560 0.01048 0.00523 -0.0729 0.2662 1.0000
7.250 1.0634 0.01117 0.00570 -0.0694 0.2218 1.0000
7.500 1.0588 0.01240 0.00654 -0.0641 0.1537 1.0000
7.750 1.0647 0.01328 0.00722 -0.0606 0.1172 1.0000
8.000 1.0682 0.01433 0.00802 -0.0569 0.0752 1.0000
8.250 1.0753 0.01526 0.00879 -0.0539 0.0488 1.0000
8.500 1.0887 0.01592 0.00940 -0.0519 0.0406 1.0000
8.750 1.1040 0.01650 0.00998 -0.0503 0.0377 1.0000
9.000 1.1185 0.01715 0.01063 -0.0486 0.0351 1.0000
9.250 1.1343 0.01774 0.01125 -0.0471 0.0339 1.0000
9.500 1.1505 0.01833 0.01187 -0.0457 0.0327 1.0000
9.750 1.1657 0.01899 0.01256 -0.0443 0.0318 1.0000
10.000 1.1793 0.01976 0.01335 -0.0428 0.0303 1.0000
10.250 1.1911 0.02066 0.01428 -0.0410 0.0293 1.0000
10.500 1.2026 0.02162 0.01529 -0.0394 0.0284 1.0000
10.750 1.2176 0.02237 0.01608 -0.0382 0.0279 1.0000
11.000 1.2313 0.02321 0.01697 -0.0369 0.0273 1.0000
11.250 1.2444 0.02412 0.01792 -0.0356 0.0266 1.0000
11.500 1.2571 0.02508 0.01891 -0.0344 0.0258 1.0000
11.750 1.2685 0.02614 0.02000 -0.0331 0.0250 1.0000
12.000 1.2759 0.02752 0.02142 -0.0315 0.0243 1.0000
12.250 1.2766 0.02945 0.02343 -0.0295 0.0236 1.0000
12.500 1.2893 0.03052 0.02455 -0.0285 0.0232 1.0000
12.750 1.3037 0.03148 0.02555 -0.0278 0.0226 1.0000
13.000 1.3152 0.03267 0.02679 -0.0269 0.0220 1.0000
13.250 1.3250 0.03405 0.02821 -0.0259 0.0214 1.0000
13.500 1.3348 0.03545 0.02965 -0.0250 0.0209 1.0000
13.750 1.3435 0.03698 0.03122 -0.0242 0.0204 1.0000
14.000 1.3472 0.03899 0.03327 -0.0231 0.0199 1.0000
14.250 1.3420 0.04185 0.03622 -0.0218 0.0193 1.0000
14.500 1.3540 0.04321 0.03763 -0.0213 0.0190 1.0000
14.750 1.3634 0.04483 0.03931 -0.0208 0.0186 1.0000
15.000 1.3722 0.04653 0.04107 -0.0204 0.0181 1.0000
15.250 1.3799 0.04835 0.04294 -0.0200 0.0177 1.0000
15.500 1.3863 0.05034 0.04498 -0.0195 0.0172 1.0000
15.750 1.3910 0.05254 0.04724 -0.0192 0.0169 1.0000
16.000 1.3973 0.05460 0.04933 -0.0189 0.0164 1.0000
16.250 1.3973 0.05739 0.05217 -0.0186 0.0160 1.0000
16.500 1.3889 0.06110 0.05597 -0.0183 0.0156 1.0000
16.750 1.3967 0.06311 0.05805 -0.0183 0.0154 1.0000
17.000 1.4010 0.06554 0.06055 -0.0183 0.0150 1.0000
17.250 1.4031 0.06824 0.06333 -0.0183 0.0148 1.0000
17.500 1.4042 0.07110 0.06626 -0.0185 0.0145 1.0000
17.750 1.4075 0.07370 0.06893 -0.0187 0.0142 1.0000
18.000 1.4083 0.07664 0.07193 -0.0189 0.0139 1.0000
18.250 1.4084 0.07971 0.07507 -0.0193 0.0137 1.0000
18.500 1.4083 0.08287 0.07828 -0.0198 0.0134 1.0000
18.750 1.4043 0.08653 0.08201 -0.0204 0.0131 1.0000
19.000 1.3964 0.09071 0.08626 -0.0211 0.0128 1.0000
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