GOE 410 AIRFOIL (goe410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 410 AIRFOIL (goe410-il) Reynolds number: 1,000,000 Max Cl/Cd: 81.79 at α=10.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe410-il-1000000-n5.txt Download as CSV file: xf-goe410-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 410 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3456 0.08828 0.08412 -0.0154 1.0000 0.0277
-19.500 -1.3593 0.08297 0.07872 -0.0178 1.0000 0.0280
-19.250 -1.3705 0.07814 0.07380 -0.0199 1.0000 0.0282
-19.000 -1.3810 0.07348 0.06906 -0.0218 1.0000 0.0287
-18.750 -1.3895 0.06920 0.06470 -0.0235 1.0000 0.0291
-18.500 -1.3954 0.06534 0.06076 -0.0249 1.0000 0.0293
-18.250 -1.4012 0.06156 0.05691 -0.0263 1.0000 0.0297
-18.000 -1.4053 0.05808 0.05335 -0.0275 1.0000 0.0301
-17.750 -1.4089 0.05471 0.04990 -0.0285 1.0000 0.0304
-17.500 -1.4113 0.05153 0.04665 -0.0295 1.0000 0.0309
-17.000 -1.4170 0.04535 0.04033 -0.0311 1.0000 0.0317
-16.750 -1.4201 0.04229 0.03721 -0.0318 1.0000 0.0326
-16.500 -1.4194 0.03964 0.03450 -0.0324 1.0000 0.0331
-16.250 -1.4180 0.03711 0.03191 -0.0328 1.0000 0.0338
-16.000 -1.4150 0.03478 0.02952 -0.0332 1.0000 0.0345
-15.750 -1.4103 0.03266 0.02734 -0.0334 1.0000 0.0352
-15.500 -1.4076 0.03043 0.02507 -0.0335 1.0000 0.0363
-15.250 -1.4033 0.02844 0.02303 -0.0334 1.0000 0.0376
-15.000 -1.3975 0.02668 0.02123 -0.0332 1.0000 0.0390
-14.750 -1.3909 0.02509 0.01959 -0.0327 1.0000 0.0403
-14.500 -1.3853 0.02354 0.01802 -0.0319 1.0000 0.0423
-14.250 -1.3780 0.02224 0.01668 -0.0310 1.0000 0.0444
-14.000 -1.3719 0.02099 0.01543 -0.0296 1.0000 0.0472
-13.750 -1.3635 0.02001 0.01443 -0.0281 1.0000 0.0500
-13.500 -1.3554 0.01913 0.01355 -0.0263 1.0000 0.0529
-13.250 -1.3446 0.01848 0.01288 -0.0243 1.0000 0.0555
-13.000 -1.3341 0.01788 0.01227 -0.0221 1.0000 0.0574
-12.750 -1.3229 0.01736 0.01174 -0.0198 1.0000 0.0596
-12.500 -1.3091 0.01695 0.01131 -0.0177 1.0000 0.0615
-12.250 -1.2913 0.01655 0.01089 -0.0163 1.0000 0.0631
-12.000 -1.2734 0.01611 0.01045 -0.0149 1.0000 0.0651
-11.750 -1.2538 0.01572 0.01005 -0.0137 1.0000 0.0669
-11.500 -1.2329 0.01538 0.00969 -0.0127 1.0000 0.0684
-11.250 -1.2112 0.01507 0.00936 -0.0117 1.0000 0.0695
-11.000 -1.1894 0.01474 0.00901 -0.0108 1.0000 0.0706
-10.750 -1.1679 0.01438 0.00864 -0.0098 1.0000 0.0721
-10.500 -1.1457 0.01404 0.00831 -0.0089 1.0000 0.0736
-10.250 -1.1229 0.01373 0.00800 -0.0081 1.0000 0.0751
-10.000 -1.0996 0.01346 0.00771 -0.0073 1.0000 0.0764
-9.750 -1.0651 0.01316 0.00739 -0.0089 0.9725 0.0776
-9.500 -1.0220 0.01286 0.00703 -0.0121 0.9247 0.0789
-9.250 -0.9999 0.01272 0.00672 -0.0109 0.8650 0.0804
-9.000 -0.9776 0.01255 0.00644 -0.0098 0.8306 0.0823
-8.750 -0.9537 0.01236 0.00618 -0.0090 0.8079 0.0843
-8.500 -0.9289 0.01219 0.00593 -0.0084 0.7899 0.0860
-8.250 -0.9034 0.01203 0.00570 -0.0079 0.7740 0.0872
-8.000 -0.8783 0.01181 0.00545 -0.0073 0.7576 0.0896
-7.750 -0.8529 0.01162 0.00521 -0.0068 0.7398 0.0919
-7.500 -0.8272 0.01144 0.00499 -0.0063 0.7218 0.0946
-7.250 -0.8010 0.01129 0.00478 -0.0059 0.7033 0.0972
-7.000 -0.7752 0.01110 0.00456 -0.0054 0.6830 0.1012
-6.750 -0.7488 0.01096 0.00436 -0.0050 0.6615 0.1045
-6.500 -0.7221 0.01084 0.00418 -0.0047 0.6414 0.1073
-6.250 -0.6955 0.01070 0.00400 -0.0044 0.6217 0.1113
-6.000 -0.6687 0.01057 0.00383 -0.0041 0.6034 0.1154
-5.750 -0.6414 0.01048 0.00368 -0.0038 0.5872 0.1188
-5.500 -0.6142 0.01036 0.00352 -0.0035 0.5728 0.1225
-5.250 -0.5869 0.01022 0.00338 -0.0033 0.5609 0.1269
-5.000 -0.5593 0.01013 0.00325 -0.0031 0.5501 0.1308
-4.750 -0.5314 0.01003 0.00312 -0.0029 0.5412 0.1340
-4.500 -0.5039 0.00991 0.00299 -0.0027 0.5325 0.1386
-4.250 -0.4759 0.00979 0.00286 -0.0026 0.5256 0.1426
-4.000 -0.4478 0.00970 0.00276 -0.0024 0.5185 0.1459
-3.500 -0.3917 0.00948 0.00253 -0.0021 0.5072 0.1546
-3.250 -0.3636 0.00938 0.00242 -0.0020 0.4994 0.1596
-3.000 -0.3356 0.00929 0.00232 -0.0018 0.4908 0.1660
-2.750 -0.3078 0.00914 0.00220 -0.0016 0.4833 0.1773
-2.500 -0.2828 0.00864 0.00196 -0.0012 0.4770 0.2378
-2.250 -0.2557 0.00841 0.00185 -0.0010 0.4718 0.2731
-2.000 -0.2276 0.00825 0.00177 -0.0008 0.4667 0.2939
-1.750 -0.1994 0.00815 0.00171 -0.0007 0.4597 0.3108
-1.500 -0.1712 0.00807 0.00166 -0.0006 0.4525 0.3265
-1.250 -0.1428 0.00797 0.00162 -0.0005 0.4458 0.3432
-1.000 -0.1146 0.00790 0.00158 -0.0003 0.4376 0.3604
-0.750 -0.0861 0.00784 0.00156 -0.0002 0.4312 0.3738
-0.500 -0.0574 0.00779 0.00154 -0.0002 0.4243 0.3866
-0.250 -0.0287 0.00779 0.00153 -0.0001 0.4165 0.3981
0.000 0.0000 0.00775 0.00153 0.0000 0.4086 0.4087
0.250 0.0287 0.00779 0.00153 0.0001 0.3981 0.4165
0.500 0.0574 0.00779 0.00154 0.0002 0.3865 0.4243
0.750 0.0861 0.00784 0.00156 0.0002 0.3741 0.4311
1.000 0.1146 0.00790 0.00158 0.0003 0.3601 0.4379
1.250 0.1428 0.00797 0.00162 0.0005 0.3434 0.4459
1.500 0.1712 0.00807 0.00166 0.0006 0.3263 0.4526
1.750 0.1994 0.00815 0.00171 0.0007 0.3109 0.4598
2.000 0.2276 0.00825 0.00177 0.0008 0.2938 0.4667
2.250 0.2557 0.00841 0.00185 0.0009 0.2732 0.4718
2.500 0.2827 0.00865 0.00196 0.0012 0.2375 0.4771
2.750 0.3078 0.00913 0.00220 0.0016 0.1776 0.4834
3.000 0.3356 0.00929 0.00232 0.0018 0.1661 0.4908
3.250 0.3636 0.00938 0.00242 0.0020 0.1596 0.4997
3.500 0.3917 0.00949 0.00253 0.0021 0.1546 0.5070
4.000 0.4478 0.00970 0.00276 0.0024 0.1459 0.5185
4.250 0.4759 0.00979 0.00286 0.0026 0.1426 0.5255
4.500 0.5038 0.00991 0.00299 0.0027 0.1386 0.5326
4.750 0.5314 0.01003 0.00312 0.0029 0.1340 0.5412
5.000 0.5593 0.01013 0.00325 0.0031 0.1309 0.5500
5.250 0.5869 0.01022 0.00338 0.0033 0.1269 0.5607
5.500 0.6142 0.01036 0.00352 0.0035 0.1225 0.5727
5.750 0.6415 0.01048 0.00368 0.0038 0.1188 0.5870
6.000 0.6687 0.01057 0.00383 0.0041 0.1154 0.6033
6.250 0.6955 0.01070 0.00400 0.0044 0.1113 0.6218
6.500 0.7221 0.01084 0.00418 0.0047 0.1073 0.6412
6.750 0.7488 0.01096 0.00436 0.0050 0.1045 0.6618
7.000 0.7752 0.01110 0.00456 0.0054 0.1013 0.6826
7.250 0.8010 0.01129 0.00478 0.0059 0.0973 0.7034
7.500 0.8272 0.01144 0.00499 0.0063 0.0946 0.7217
7.750 0.8530 0.01162 0.00521 0.0068 0.0919 0.7397
8.000 0.8783 0.01181 0.00545 0.0073 0.0896 0.7575
8.250 0.9034 0.01203 0.00570 0.0079 0.0871 0.7741
8.500 0.9289 0.01219 0.00593 0.0084 0.0859 0.7899
8.750 0.9538 0.01237 0.00618 0.0090 0.0843 0.8076
9.000 0.9776 0.01254 0.00644 0.0098 0.0824 0.8312
9.250 1.0000 0.01272 0.00672 0.0109 0.0805 0.8650
9.500 1.0220 0.01287 0.00703 0.0121 0.0788 0.9245
9.750 1.0651 0.01316 0.00739 0.0088 0.0776 0.9726
10.000 1.0997 0.01345 0.00771 0.0073 0.0764 1.0000
10.250 1.1230 0.01373 0.00800 0.0081 0.0751 1.0000
10.500 1.1457 0.01404 0.00831 0.0089 0.0735 1.0000
10.750 1.1679 0.01437 0.00864 0.0098 0.0721 1.0000
11.000 1.1894 0.01474 0.00901 0.0108 0.0706 1.0000
11.250 1.2112 0.01507 0.00935 0.0117 0.0695 1.0000
11.500 1.2330 0.01538 0.00969 0.0127 0.0684 1.0000
11.750 1.2539 0.01572 0.01005 0.0137 0.0669 1.0000
12.000 1.2736 0.01610 0.01045 0.0149 0.0652 1.0000
12.250 1.2915 0.01655 0.01089 0.0163 0.0631 1.0000
12.500 1.3093 0.01695 0.01130 0.0177 0.0615 1.0000
12.750 1.3233 0.01736 0.01174 0.0197 0.0597 1.0000
13.000 1.3345 0.01788 0.01226 0.0221 0.0574 1.0000
13.250 1.3450 0.01847 0.01287 0.0243 0.0554 1.0000
13.500 1.3558 0.01913 0.01355 0.0262 0.0528 1.0000
13.750 1.3641 0.02000 0.01442 0.0280 0.0500 1.0000
14.000 1.3728 0.02096 0.01540 0.0295 0.0473 1.0000
14.250 1.3792 0.02219 0.01664 0.0308 0.0447 1.0000
14.500 1.3863 0.02351 0.01799 0.0318 0.0423 1.0000
14.750 1.3921 0.02505 0.01955 0.0326 0.0404 1.0000
15.000 1.3985 0.02666 0.02120 0.0330 0.0389 1.0000
15.250 1.4047 0.02839 0.02298 0.0333 0.0376 1.0000
15.500 1.4098 0.03032 0.02495 0.0334 0.0366 1.0000
16.000 1.4165 0.03475 0.02948 0.0330 0.0344 1.0000
16.250 1.4200 0.03704 0.03184 0.0326 0.0338 1.0000
16.500 1.4217 0.03956 0.03442 0.0321 0.0330 1.0000
16.750 1.4211 0.04236 0.03727 0.0315 0.0323 1.0000
17.000 1.4201 0.04521 0.04018 0.0308 0.0318 1.0000
17.250 1.4165 0.04838 0.04342 0.0300 0.0312 1.0000
17.500 1.4142 0.05144 0.04656 0.0292 0.0308 1.0000
17.750 1.4118 0.05462 0.04981 0.0282 0.0305 1.0000
18.000 1.4090 0.05791 0.05317 0.0271 0.0302 1.0000
18.250 1.4047 0.06141 0.05676 0.0260 0.0298 1.0000
18.500 1.3992 0.06515 0.06058 0.0246 0.0294 1.0000
18.750 1.3925 0.06912 0.06462 0.0232 0.0290 1.0000
19.000 1.3838 0.07342 0.06900 0.0215 0.0285 1.0000
19.250 1.3735 0.07805 0.07370 0.0195 0.0282 1.0000
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