GOE 410 AIRFOIL (goe410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 410 AIRFOIL (goe410-il) Reynolds number: 1,000,000 Max Cl/Cd: 81.98 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe410-il-1000000.txt Download as CSV file: xf-goe410-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3411 0.08915 0.08516 -0.0151 1.0000 0.0327
-19.500 -1.3550 0.08379 0.07972 -0.0175 1.0000 0.0331
-19.250 -1.3670 0.07884 0.07469 -0.0197 1.0000 0.0335
-19.000 -1.3782 0.07408 0.06985 -0.0216 1.0000 0.0339
-18.750 -1.3866 0.06979 0.06548 -0.0233 1.0000 0.0344
-18.500 -1.3931 0.06585 0.06145 -0.0248 1.0000 0.0348
-18.250 -1.3986 0.06210 0.05761 -0.0261 1.0000 0.0352
-18.000 -1.4010 0.05881 0.05424 -0.0272 1.0000 0.0357
-17.750 -1.4120 0.05454 0.04990 -0.0287 1.0000 0.0364
-17.500 -1.4201 0.05073 0.04602 -0.0298 1.0000 0.0370
-17.250 -1.4259 0.04731 0.04253 -0.0308 1.0000 0.0375
-17.000 -1.4302 0.04408 0.03925 -0.0316 1.0000 0.0385
-16.750 -1.4315 0.04123 0.03632 -0.0322 1.0000 0.0393
-16.500 -1.4298 0.03869 0.03371 -0.0327 1.0000 0.0401
-16.250 -1.4321 0.03579 0.03076 -0.0333 1.0000 0.0413
-16.000 -1.4323 0.03316 0.02809 -0.0336 1.0000 0.0428
-15.750 -1.4292 0.03095 0.02583 -0.0338 1.0000 0.0443
-15.500 -1.4260 0.02883 0.02367 -0.0337 1.0000 0.0462
-15.250 -1.4223 0.02688 0.02170 -0.0335 1.0000 0.0486
-15.000 -1.4157 0.02527 0.02005 -0.0330 1.0000 0.0511
-14.750 -1.4096 0.02373 0.01851 -0.0324 1.0000 0.0542
-14.500 -1.3999 0.02256 0.01731 -0.0315 1.0000 0.0569
-14.250 -1.3916 0.02140 0.01615 -0.0305 1.0000 0.0596
-14.000 -1.3791 0.02059 0.01531 -0.0294 1.0000 0.0621
-13.750 -1.3684 0.01977 0.01445 -0.0279 1.0000 0.0642
-13.500 -1.3578 0.01903 0.01371 -0.0262 1.0000 0.0663
-13.250 -1.3445 0.01848 0.01314 -0.0246 1.0000 0.0682
-13.000 -1.3290 0.01808 0.01269 -0.0230 1.0000 0.0696
-12.750 -1.3181 0.01754 0.01213 -0.0206 1.0000 0.0711
-12.500 -1.3069 0.01704 0.01162 -0.0182 1.0000 0.0729
-12.250 -1.2896 0.01663 0.01121 -0.0167 1.0000 0.0746
-12.000 -1.2697 0.01630 0.01085 -0.0156 1.0000 0.0762
-11.750 -1.2484 0.01601 0.01053 -0.0146 1.0000 0.0774
-11.500 -1.2287 0.01562 0.01011 -0.0134 1.0000 0.0788
-11.250 -1.2100 0.01514 0.00963 -0.0121 1.0000 0.0806
-11.000 -1.1890 0.01477 0.00926 -0.0111 1.0000 0.0823
-10.750 -1.1669 0.01444 0.00893 -0.0102 1.0000 0.0837
-10.500 -1.1438 0.01417 0.00863 -0.0094 1.0000 0.0852
-10.250 -1.1203 0.01392 0.00835 -0.0086 1.0000 0.0863
-10.000 -1.0983 0.01355 0.00797 -0.0077 1.0000 0.0878
-9.750 -1.0764 0.01317 0.00760 -0.0067 1.0000 0.0898
-9.500 -1.0534 0.01286 0.00729 -0.0059 1.0000 0.0915
-9.250 -1.0300 0.01258 0.00702 -0.0051 1.0000 0.0932
-9.000 -1.0061 0.01234 0.00677 -0.0043 1.0000 0.0948
-8.750 -0.9819 0.01215 0.00655 -0.0036 1.0000 0.0960
-8.500 -0.9600 0.01179 0.00622 -0.0025 1.0000 0.0991
-8.250 -0.9301 0.01149 0.00596 -0.0030 0.9922 0.1019
-8.000 -0.8884 0.01123 0.00571 -0.0059 0.9749 0.1051
-7.750 -0.8448 0.01094 0.00540 -0.0092 0.9450 0.1087
-7.500 -0.8172 0.01077 0.00515 -0.0089 0.8945 0.1128
-7.250 -0.7934 0.01070 0.00495 -0.0079 0.8556 0.1162
-7.000 -0.7683 0.01059 0.00475 -0.0072 0.8294 0.1194
-6.750 -0.7433 0.01041 0.00453 -0.0065 0.8080 0.1244
-6.500 -0.7172 0.01029 0.00436 -0.0060 0.7887 0.1285
-6.250 -0.6905 0.01018 0.00418 -0.0056 0.7705 0.1319
-6.000 -0.6645 0.00999 0.00396 -0.0051 0.7518 0.1373
-5.750 -0.6378 0.00987 0.00379 -0.0047 0.7320 0.1416
-5.500 -0.6105 0.00980 0.00365 -0.0044 0.7111 0.1444
-5.250 -0.5843 0.00962 0.00342 -0.0040 0.6888 0.1506
-5.000 -0.5575 0.00950 0.00325 -0.0036 0.6664 0.1556
-4.750 -0.5302 0.00943 0.00309 -0.0033 0.6449 0.1599
-4.500 -0.5035 0.00925 0.00290 -0.0030 0.6253 0.1685
-3.750 -0.4265 0.00827 0.00225 -0.0017 0.5803 0.2690
-3.500 -0.3997 0.00805 0.00213 -0.0014 0.5692 0.3006
-3.250 -0.3720 0.00792 0.00204 -0.0012 0.5599 0.3215
-3.000 -0.3442 0.00783 0.00196 -0.0010 0.5497 0.3386
-2.750 -0.3160 0.00773 0.00190 -0.0009 0.5404 0.3541
-2.500 -0.2879 0.00766 0.00184 -0.0007 0.5313 0.3681
-2.250 -0.2594 0.00761 0.00181 -0.0006 0.5242 0.3808
-2.000 -0.2306 0.00756 0.00177 -0.0006 0.5179 0.3935
-1.750 -0.2022 0.00752 0.00175 -0.0004 0.5111 0.4041
-1.500 -0.1732 0.00752 0.00173 -0.0004 0.5044 0.4125
-1.250 -0.1446 0.00746 0.00171 -0.0003 0.4967 0.4232
-1.000 -0.1158 0.00748 0.00170 -0.0002 0.4893 0.4328
-0.750 -0.0869 0.00744 0.00170 -0.0002 0.4841 0.4428
-0.500 -0.0577 0.00744 0.00169 -0.0001 0.4781 0.4507
-0.250 -0.0291 0.00743 0.00169 0.0000 0.4717 0.4590
0.000 0.0000 0.00743 0.00170 0.0000 0.4659 0.4659
0.250 0.0291 0.00743 0.00169 0.0000 0.4589 0.4717
0.500 0.0577 0.00744 0.00169 0.0001 0.4506 0.4781
0.750 0.0869 0.00744 0.00170 0.0002 0.4427 0.4841
1.000 0.1158 0.00748 0.00170 0.0002 0.4328 0.4893
1.250 0.1446 0.00746 0.00171 0.0003 0.4232 0.4968
1.500 0.1732 0.00752 0.00173 0.0004 0.4125 0.5043
1.750 0.2022 0.00752 0.00175 0.0004 0.4041 0.5111
2.000 0.2307 0.00756 0.00177 0.0006 0.3935 0.5179
2.250 0.2594 0.00761 0.00181 0.0006 0.3809 0.5242
2.500 0.2879 0.00767 0.00184 0.0007 0.3680 0.5312
2.750 0.3161 0.00773 0.00190 0.0009 0.3541 0.5405
3.000 0.3442 0.00783 0.00196 0.0010 0.3386 0.5497
3.250 0.3720 0.00792 0.00204 0.0012 0.3215 0.5600
3.500 0.3998 0.00805 0.00213 0.0014 0.3006 0.5692
3.750 0.4265 0.00827 0.00225 0.0017 0.2689 0.5804
4.500 0.5035 0.00925 0.00290 0.0030 0.1685 0.6252
4.750 0.5302 0.00942 0.00309 0.0033 0.1600 0.6449
5.000 0.5575 0.00950 0.00325 0.0036 0.1555 0.6662
5.250 0.5843 0.00962 0.00342 0.0040 0.1506 0.6887
5.500 0.6105 0.00980 0.00365 0.0044 0.1445 0.7110
5.750 0.6378 0.00987 0.00379 0.0047 0.1416 0.7320
6.000 0.6645 0.00999 0.00396 0.0051 0.1374 0.7520
6.250 0.6905 0.01018 0.00418 0.0056 0.1320 0.7705
6.500 0.7172 0.01029 0.00436 0.0060 0.1285 0.7888
6.750 0.7434 0.01041 0.00453 0.0065 0.1245 0.8076
7.000 0.7684 0.01059 0.00475 0.0071 0.1194 0.8293
7.250 0.7934 0.01069 0.00495 0.0079 0.1162 0.8556
7.500 0.8172 0.01077 0.00515 0.0089 0.1129 0.8943
7.750 0.8448 0.01094 0.00540 0.0092 0.1087 0.9448
8.000 0.8885 0.01123 0.00570 0.0059 0.1051 0.9750
8.250 0.9302 0.01149 0.00595 0.0030 0.1018 0.9922
8.500 0.9600 0.01179 0.00622 0.0025 0.0990 1.0000
8.750 0.9819 0.01215 0.00655 0.0036 0.0961 1.0000
9.000 1.0061 0.01234 0.00677 0.0043 0.0948 1.0000
9.250 1.0300 0.01258 0.00702 0.0051 0.0932 1.0000
9.500 1.0534 0.01285 0.00729 0.0059 0.0915 1.0000
9.750 1.0764 0.01317 0.00760 0.0067 0.0897 1.0000
10.000 1.0983 0.01355 0.00797 0.0077 0.0878 1.0000
10.250 1.1202 0.01392 0.00835 0.0086 0.0862 1.0000
10.500 1.1439 0.01416 0.00863 0.0094 0.0851 1.0000
10.750 1.1669 0.01444 0.00893 0.0102 0.0837 1.0000
11.000 1.1890 0.01476 0.00925 0.0111 0.0822 1.0000
11.250 1.2100 0.01514 0.00963 0.0121 0.0806 1.0000
11.500 1.2287 0.01562 0.01011 0.0134 0.0787 1.0000
11.750 1.2485 0.01601 0.01052 0.0146 0.0774 1.0000
12.000 1.2697 0.01630 0.01085 0.0156 0.0762 1.0000
12.250 1.2897 0.01663 0.01121 0.0167 0.0747 1.0000
12.500 1.3070 0.01703 0.01162 0.0182 0.0729 1.0000
12.750 1.3182 0.01754 0.01212 0.0206 0.0711 1.0000
13.000 1.3294 0.01807 0.01268 0.0229 0.0696 1.0000
13.250 1.3449 0.01847 0.01313 0.0245 0.0681 1.0000
13.500 1.3581 0.01903 0.01371 0.0262 0.0663 1.0000
13.750 1.3688 0.01976 0.01445 0.0279 0.0642 1.0000
14.000 1.3793 0.02060 0.01531 0.0293 0.0622 1.0000
14.250 1.3921 0.02139 0.01613 0.0304 0.0596 1.0000
14.500 1.4003 0.02256 0.01730 0.0315 0.0568 1.0000
14.750 1.4105 0.02370 0.01848 0.0323 0.0542 1.0000
15.000 1.4166 0.02523 0.02002 0.0329 0.0511 1.0000
15.250 1.4234 0.02683 0.02165 0.0334 0.0487 1.0000
15.500 1.4275 0.02876 0.02360 0.0336 0.0463 1.0000
15.750 1.4306 0.03090 0.02577 0.0336 0.0442 1.0000
16.000 1.4337 0.03312 0.02804 0.0335 0.0427 1.0000
16.250 1.4337 0.03573 0.03070 0.0331 0.0413 1.0000
16.500 1.4319 0.03859 0.03360 0.0325 0.0400 1.0000
16.750 1.4335 0.04114 0.03623 0.0320 0.0392 1.0000
17.000 1.4319 0.04405 0.03921 0.0313 0.0384 1.0000
17.250 1.4284 0.04719 0.04241 0.0305 0.0376 1.0000
17.500 1.4220 0.05068 0.04598 0.0296 0.0370 1.0000
17.750 1.4146 0.05443 0.04979 0.0284 0.0364 1.0000
18.000 1.4047 0.05858 0.05401 0.0270 0.0356 1.0000
18.250 1.4019 0.06191 0.05742 0.0259 0.0352 1.0000
18.500 1.3967 0.06562 0.06122 0.0246 0.0348 1.0000
18.750 1.3900 0.06959 0.06527 0.0231 0.0344 1.0000
19.000 1.3806 0.07400 0.06976 0.0213 0.0339 1.0000
19.250 1.3703 0.07865 0.07449 0.0194 0.0335 1.0000
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