GOE 365 AIRFOIL (goe365-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 365 AIRFOIL (goe365-il) Reynolds number: 1,000,000 Max Cl/Cd: 99.08 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe365-il-1000000-n5.txt Download as CSV file: xf-goe365-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 365 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
------ -------- --------- --------- -------- -------- --------
-15.750 -0.3526 0.17093 0.16912 -0.0267 1.0000 0.0050
-15.500 -0.3475 0.16758 0.16577 -0.0277 1.0000 0.0051
-14.500 -0.3326 0.15272 0.15094 -0.0316 1.0000 0.0054
-11.500 -0.2443 0.10879 0.10706 -0.0554 0.9670 0.0074
-11.250 -0.2272 0.10367 0.10191 -0.0612 0.9559 0.0074
-11.000 -0.2003 0.09956 0.09777 -0.0681 0.9453 0.0077
-10.750 -0.1697 0.09419 0.09232 -0.0773 0.9336 0.0079
-10.500 -0.1516 0.08437 0.08242 -0.0899 0.9213 0.0093
-10.250 -0.1175 0.07965 0.07756 -0.0997 0.8986 0.0095
-10.000 -0.0990 0.07671 0.07446 -0.1040 0.8675 0.0097
-9.750 -0.0942 0.07388 0.07150 -0.1055 0.8381 0.0097
-9.500 -0.0890 0.07172 0.06924 -0.1062 0.8149 0.0100
-9.250 -0.0890 0.06887 0.06631 -0.1070 0.7952 0.0104
-9.000 -0.0945 0.06528 0.06267 -0.1082 0.7796 0.0106
-8.500 -0.1509 0.05230 0.04961 -0.1145 0.7548 0.0118
-8.250 -0.1451 0.04957 0.04680 -0.1155 0.7480 0.0120
-8.000 -0.1383 0.04658 0.04373 -0.1163 0.7425 0.0122
-7.500 -0.1490 0.03351 0.03014 -0.1164 0.7320 0.0142
-7.000 -0.1592 0.01823 0.01358 -0.1104 0.7242 0.0177
-6.750 -0.1345 0.01799 0.01328 -0.1100 0.7201 0.0178
-6.500 -0.1102 0.01769 0.01290 -0.1094 0.7156 0.0180
-6.250 -0.0847 0.01759 0.01275 -0.1090 0.7109 0.0181
-6.000 -0.0600 0.01724 0.01233 -0.1085 0.7055 0.0183
-5.750 -0.0353 0.01692 0.01192 -0.1080 0.7005 0.0187
-5.500 -0.0111 0.01634 0.01123 -0.1074 0.6967 0.0191
-5.250 0.0116 0.01503 0.00972 -0.1065 0.6936 0.0198
-5.000 0.0348 0.01368 0.00810 -0.1056 0.6904 0.0208
-4.750 0.0600 0.01308 0.00734 -0.1051 0.6869 0.0212
-4.500 0.0846 0.01231 0.00644 -0.1045 0.6836 0.0215
-4.250 0.1103 0.01192 0.00600 -0.1040 0.6803 0.0218
-4.000 0.1369 0.01161 0.00566 -0.1038 0.6771 0.0220
-3.750 0.1634 0.01135 0.00537 -0.1034 0.6734 0.0223
-3.500 0.1898 0.01111 0.00509 -0.1031 0.6695 0.0227
-3.250 0.2160 0.01089 0.00482 -0.1027 0.6657 0.0231
-3.000 0.2425 0.01055 0.00444 -0.1024 0.6621 0.0234
-2.750 0.2688 0.01022 0.00407 -0.1020 0.6578 0.0237
-2.500 0.2948 0.00994 0.00375 -0.1015 0.6526 0.0240
-2.250 0.3205 0.00969 0.00345 -0.1010 0.6451 0.0243
-2.000 0.3461 0.00946 0.00318 -0.1004 0.6364 0.0246
-1.750 0.3718 0.00927 0.00295 -0.0999 0.6275 0.0249
-1.500 0.3972 0.00912 0.00275 -0.0993 0.6179 0.0252
-1.250 0.4227 0.00904 0.00262 -0.0988 0.6042 0.0255
-1.000 0.4469 0.00895 0.00245 -0.0980 0.5856 0.0258
-0.750 0.4688 0.00883 0.00220 -0.0967 0.5575 0.0263
-0.500 0.4909 0.00888 0.00210 -0.0955 0.5260 0.0266
-0.250 0.5143 0.00892 0.00204 -0.0946 0.5021 0.0271
0.000 0.5384 0.00896 0.00200 -0.0938 0.4842 0.0275
0.250 0.5628 0.00899 0.00197 -0.0931 0.4685 0.0279
0.500 0.5873 0.00903 0.00195 -0.0924 0.4539 0.0285
0.750 0.6109 0.00913 0.00196 -0.0915 0.4345 0.0289
1.000 0.6343 0.00926 0.00198 -0.0906 0.4132 0.0295
1.250 0.6584 0.00935 0.00201 -0.0899 0.3980 0.0300
1.500 0.6826 0.00945 0.00205 -0.0892 0.3837 0.0308
1.750 0.7061 0.00957 0.00210 -0.0883 0.3655 0.0316
2.000 0.7295 0.00970 0.00214 -0.0875 0.3477 0.0328
2.250 0.7529 0.00984 0.00221 -0.0866 0.3316 0.0344
2.500 0.7761 0.00999 0.00230 -0.0857 0.3153 0.0361
2.750 0.7989 0.01017 0.00240 -0.0848 0.2986 0.0383
3.000 0.8201 0.01024 0.00256 -0.0836 0.2810 0.1311
3.500 0.9202 0.00931 0.00335 -0.0949 0.2343 1.0000
3.750 0.9399 0.00954 0.00350 -0.0933 0.2218 1.0000
4.000 0.9597 0.00977 0.00366 -0.0917 0.2109 1.0000
4.250 0.9796 0.00999 0.00382 -0.0902 0.2020 1.0000
4.500 1.0004 0.01018 0.00397 -0.0889 0.1955 1.0000
4.750 1.0205 0.01040 0.00414 -0.0874 0.1892 1.0000
5.000 1.0417 0.01057 0.00430 -0.0862 0.1849 1.0000
5.250 1.0623 0.01076 0.00446 -0.0848 0.1808 1.0000
5.500 1.0824 0.01097 0.00464 -0.0834 0.1765 1.0000
5.750 1.1028 0.01116 0.00482 -0.0820 0.1730 1.0000
6.000 1.1234 0.01134 0.00500 -0.0807 0.1706 1.0000
6.250 1.1424 0.01153 0.00519 -0.0791 0.1681 1.0000
6.500 1.1601 0.01173 0.00538 -0.0772 0.1650 1.0000
6.750 1.1781 0.01194 0.00559 -0.0754 0.1626 1.0000
7.000 1.1960 0.01218 0.00583 -0.0736 0.1592 1.0000
7.250 1.2153 0.01238 0.00604 -0.0721 0.1572 1.0000
7.500 1.2342 0.01260 0.00627 -0.0707 0.1548 1.0000
7.750 1.2532 0.01284 0.00652 -0.0692 0.1527 1.0000
8.000 1.2709 0.01314 0.00682 -0.0676 0.1484 1.0000
8.250 1.2888 0.01345 0.00712 -0.0660 0.1441 1.0000
8.500 1.3066 0.01377 0.00743 -0.0645 0.1379 1.0000
8.750 1.3222 0.01421 0.00782 -0.0627 0.1293 1.0000
9.000 1.3365 0.01472 0.00828 -0.0608 0.1169 1.0000
9.250 1.3432 0.01563 0.00904 -0.0578 0.0935 1.0000
9.500 1.3559 0.01628 0.00966 -0.0558 0.0858 1.0000
9.750 1.3716 0.01680 0.01018 -0.0543 0.0833 1.0000
10.000 1.3857 0.01742 0.01081 -0.0526 0.0801 1.0000
10.250 1.4003 0.01804 0.01145 -0.0511 0.0765 1.0000
10.500 1.4165 0.01858 0.01202 -0.0499 0.0748 1.0000
10.750 1.4324 0.01915 0.01264 -0.0487 0.0725 1.0000
11.000 1.4459 0.01990 0.01340 -0.0472 0.0683 1.0000
11.250 1.4576 0.02078 0.01428 -0.0457 0.0632 1.0000
11.500 1.4551 0.02265 0.01597 -0.0428 0.0357 1.0000
11.750 1.4542 0.02452 0.01781 -0.0403 0.0207 1.0000
12.000 1.4629 0.02578 0.01908 -0.0389 0.0170 1.0000
12.250 1.4725 0.02698 0.02032 -0.0376 0.0151 1.0000
12.500 1.4820 0.02823 0.02162 -0.0365 0.0134 1.0000
12.750 1.4916 0.02949 0.02292 -0.0354 0.0124 1.0000
13.000 1.4994 0.03094 0.02441 -0.0343 0.0112 1.0000
13.250 1.5082 0.03233 0.02585 -0.0333 0.0106 1.0000
13.500 1.5163 0.03379 0.02737 -0.0324 0.0100 1.0000
13.750 1.5232 0.03540 0.02904 -0.0315 0.0092 1.0000
14.000 1.5293 0.03711 0.03079 -0.0306 0.0088 1.0000
14.250 1.5341 0.03897 0.03272 -0.0297 0.0083 1.0000
14.500 1.5395 0.04082 0.03464 -0.0290 0.0081 1.0000
14.750 1.5446 0.04274 0.03663 -0.0283 0.0077 1.0000
15.000 1.5485 0.04482 0.03878 -0.0277 0.0073 1.0000
15.250 1.5518 0.04700 0.04102 -0.0272 0.0069 1.0000
15.500 1.5527 0.04949 0.04358 -0.0268 0.0066 1.0000
15.750 1.5521 0.05223 0.04639 -0.0264 0.0063 1.0000
16.000 1.5516 0.05505 0.04929 -0.0262 0.0062 1.0000
16.250 1.5519 0.05780 0.05213 -0.0261 0.0060 1.0000
16.500 1.5498 0.06093 0.05535 -0.0261 0.0059 1.0000
16.750 1.5465 0.06429 0.05881 -0.0263 0.0058 1.0000
17.000 1.5442 0.06760 0.06220 -0.0266 0.0055 1.0000
17.250 1.5380 0.07147 0.06617 -0.0271 0.0055 1.0000
17.500 1.5319 0.07538 0.07019 -0.0277 0.0054 1.0000
17.750 1.5241 0.07961 0.07451 -0.0284 0.0052 1.0000
18.000 1.5149 0.08408 0.07908 -0.0293 0.0051 1.0000
18.250 1.5045 0.08883 0.08394 -0.0304 0.0051 1.0000
18.500 1.4907 0.09408 0.08930 -0.0317 0.0050 1.0000
18.750 1.4782 0.09924 0.09456 -0.0331 0.0049 1.0000
19.000 1.4644 0.10469 0.10012 -0.0347 0.0048 1.0000
19.250 1.4486 0.11054 0.10608 -0.0366 0.0048 1.0000
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