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GOE 364 AIRFOIL (goe364-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 364 AIRFOIL (goe364-il)
Reynolds number: 500,000
Max Cl/Cd: 104.02 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe364-il-500000-n5.txt
Download as CSV file: xf-goe364-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 364 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.2433   0.13997   0.13758  -0.0333   1.0000   0.0121
 -12.500  -0.2388   0.13745   0.13509  -0.0336   1.0000   0.0125
 -12.250  -0.2346   0.13491   0.13256  -0.0338   1.0000   0.0129
 -12.000  -0.2270   0.13172   0.12939  -0.0352   0.9995   0.0133
 -11.500  -0.2058   0.12239   0.12005  -0.0415   0.9933   0.0111
 -11.250  -0.1927   0.11902   0.11669  -0.0441   0.9891   0.0109
 -10.750  -0.1692   0.11141   0.10907  -0.0499   0.9786   0.0110
 -10.500  -0.1543   0.10771   0.10536  -0.0534   0.9734   0.0109
 -10.250  -0.1397   0.10395   0.10160  -0.0569   0.9654   0.0116
 -10.000  -0.1192   0.10046   0.09810  -0.0614   0.9585   0.0119
  -9.750  -0.0954   0.09649   0.09411  -0.0672   0.9495   0.0124
  -9.500  -0.0704   0.09162   0.08919  -0.0742   0.9363   0.0121
  -9.250  -0.0340   0.08626   0.08372  -0.0841   0.9055   0.0126
  -9.000  -0.0072   0.08187   0.07909  -0.0912   0.8557   0.0128
  -8.750  -0.0013   0.07906   0.07606  -0.0924   0.8170   0.0130
  -8.500   0.0018   0.07658   0.07346  -0.0927   0.7933   0.0131
  -8.250   0.0043   0.07410   0.07091  -0.0930   0.7757   0.0131
  -8.000   0.0027   0.07109   0.06786  -0.0936   0.7621   0.0140
  -7.750   0.0088   0.06958   0.06631  -0.0935   0.7504   0.0143
  -7.500   0.0095   0.06762   0.06432  -0.0933   0.7389   0.0145
  -7.250   0.0135   0.06534   0.06202  -0.0943   0.7296   0.0148
  -7.000   0.0197   0.06259   0.05923  -0.0961   0.7204   0.0151
  -6.750   0.0277   0.05950   0.05611  -0.0984   0.7122   0.0151
  -6.500   0.0378   0.05614   0.05269  -0.1011   0.7044   0.0157
  -6.250   0.0485   0.05113   0.04758  -0.1054   0.6978   0.0163
  -6.000   0.0655   0.04881   0.04520  -0.1071   0.6905   0.0169
  -5.750   0.0837   0.04673   0.04305  -0.1083   0.6840   0.0174
  -5.500   0.1029   0.04392   0.04015  -0.1102   0.6773   0.0179
  -5.000   0.1431   0.03420   0.02998  -0.1148   0.6653   0.0199
  -4.750   0.1653   0.03329   0.02901  -0.1149   0.6579   0.0203
  -4.500   0.1875   0.03154   0.02711  -0.1150   0.6513   0.0209
  -4.250   0.2101   0.02857   0.02393  -0.1152   0.6445   0.0215
  -4.000   0.2292   0.02183   0.01652  -0.1144   0.6392   0.0235
  -3.750   0.2534   0.02128   0.01588  -0.1141   0.6327   0.0238
  -3.500   0.2771   0.01996   0.01437  -0.1135   0.6257   0.0242
  -3.000   0.3250   0.01709   0.01098  -0.1120   0.6122   0.0255
  -2.750   0.3494   0.01584   0.00940  -0.1111   0.6048   0.0264
  -2.500   0.3746   0.01488   0.00817  -0.1104   0.5972   0.0268
  -2.250   0.4001   0.01424   0.00729  -0.1097   0.5883   0.0271
  -2.000   0.4260   0.01379   0.00665  -0.1091   0.5788   0.0273
  -1.750   0.4508   0.01307   0.00581  -0.1085   0.5683   0.0278
  -1.500   0.4761   0.01273   0.00539  -0.1079   0.5554   0.0284
  -1.250   0.5016   0.01244   0.00501  -0.1073   0.5425   0.0288
  -1.000   0.5270   0.01215   0.00462  -0.1066   0.5301   0.0291
  -0.750   0.5521   0.01192   0.00429  -0.1059   0.5167   0.0294
  -0.500   0.5770   0.01174   0.00401  -0.1052   0.5033   0.0298
   0.000   0.6267   0.01148   0.00358  -0.1038   0.4779   0.0306
   0.250   0.6515   0.01140   0.00343  -0.1031   0.4664   0.0310
   0.500   0.6760   0.01136   0.00332  -0.1023   0.4557   0.0316
   0.750   0.7013   0.01135   0.00326  -0.1017   0.4466   0.0322
   1.000   0.7258   0.01128   0.00315  -0.1010   0.4394   0.0327
   1.250   0.7511   0.01118   0.00305  -0.1004   0.4336   0.0333
   1.500   0.7761   0.01116   0.00302  -0.0997   0.4278   0.0339
   1.750   0.8012   0.01117   0.00301  -0.0991   0.4225   0.0347
   2.000   0.8267   0.01118   0.00302  -0.0986   0.4168   0.0356
   2.250   0.8517   0.01124   0.00305  -0.0980   0.4109   0.0365
   2.500   0.8767   0.01132   0.00309  -0.0974   0.4056   0.0376
   2.750   0.9023   0.01135   0.00313  -0.0969   0.4006   0.0402
   3.000   0.9272   0.01142   0.00320  -0.0963   0.3954   0.0431
   3.250   0.9517   0.01152   0.00329  -0.0956   0.3904   0.0509
   3.500   0.9666   0.01047   0.00361  -0.0935   0.3862   0.6911
   4.000   1.0609   0.01038   0.00400  -0.1022   0.3715   1.0000
   4.250   1.0847   0.01054   0.00412  -0.1014   0.3645   1.0000
   4.500   1.1076   0.01074   0.00426  -0.1004   0.3573   1.0000
   4.750   1.1313   0.01090   0.00441  -0.0997   0.3497   1.0000
   5.000   1.1538   0.01111   0.00457  -0.0987   0.3417   1.0000
   5.250   1.1765   0.01131   0.00474  -0.0977   0.3316   1.0000
   5.500   1.1981   0.01156   0.00493  -0.0966   0.3197   1.0000
   5.750   1.2190   0.01183   0.00515  -0.0954   0.3068   1.0000
   6.000   1.2392   0.01214   0.00538  -0.0941   0.2940   1.0000
   6.250   1.2584   0.01249   0.00565  -0.0926   0.2809   1.0000
   6.500   1.2771   0.01285   0.00596  -0.0910   0.2687   1.0000
   6.750   1.2947   0.01325   0.00629  -0.0893   0.2558   1.0000
   7.000   1.3116   0.01364   0.00662  -0.0875   0.2453   1.0000
   7.500   1.3443   0.01436   0.00729  -0.0835   0.2314   1.0000
   7.750   1.3616   0.01468   0.00762  -0.0818   0.2270   1.0000
   8.000   1.3779   0.01506   0.00800  -0.0799   0.2227   1.0000
   8.250   1.3947   0.01543   0.00838  -0.0782   0.2192   1.0000
   8.500   1.4127   0.01575   0.00875  -0.0767   0.2158   1.0000
   8.750   1.4296   0.01614   0.00915  -0.0751   0.2119   1.0000
   9.000   1.4451   0.01659   0.00962  -0.0733   0.2079   1.0000
   9.250   1.4601   0.01709   0.01013  -0.0715   0.2043   1.0000
   9.500   1.4777   0.01747   0.01057  -0.0702   0.2016   1.0000
   9.750   1.4943   0.01791   0.01105  -0.0687   0.1984   1.0000
  10.000   1.5092   0.01844   0.01161  -0.0671   0.1943   1.0000
  10.250   1.5218   0.01911   0.01229  -0.0652   0.1899   1.0000
  10.500   1.5378   0.01962   0.01285  -0.0639   0.1844   1.0000
  10.750   1.5500   0.02036   0.01358  -0.0622   0.1771   1.0000
  11.000   1.5630   0.02107   0.01433  -0.0606   0.1707   1.0000
  11.250   1.5745   0.02192   0.01518  -0.0590   0.1633   1.0000
  11.500   1.5857   0.02281   0.01609  -0.0575   0.1562   1.0000
  12.000   1.6029   0.02507   0.01836  -0.0543   0.1392   1.0000
  12.250   1.6090   0.02648   0.01975  -0.0527   0.1303   1.0000
  12.500   1.6140   0.02802   0.02129  -0.0512   0.1226   1.0000
  12.750   1.6194   0.02959   0.02289  -0.0499   0.1151   1.0000
  13.000   1.6216   0.03150   0.02480  -0.0485   0.1076   1.0000
  13.250   1.6231   0.03353   0.02684  -0.0472   0.0999   1.0000
  13.500   1.6238   0.03568   0.02901  -0.0460   0.0927   1.0000
  13.750   1.6225   0.03811   0.03145  -0.0450   0.0863   1.0000
  14.000   1.6241   0.04034   0.03372  -0.0441   0.0809   1.0000
  14.250   1.6204   0.04315   0.03655  -0.0433   0.0746   1.0000
  14.500   1.6170   0.04601   0.03944  -0.0426   0.0669   1.0000
  14.750   1.6125   0.04909   0.04255  -0.0421   0.0603   1.0000
  15.000   1.5980   0.05337   0.04680  -0.0416   0.0483   1.0000
  15.250   1.5735   0.05906   0.05243  -0.0415   0.0316   1.0000
  15.500   1.5538   0.06443   0.05782  -0.0418   0.0217   1.0000
  15.750   1.5380   0.06951   0.06297  -0.0422   0.0176   1.0000
  16.000   1.5283   0.07396   0.06752  -0.0428   0.0157   1.0000
  16.250   1.5201   0.07825   0.07192  -0.0435   0.0146   1.0000
  16.500   1.5113   0.08275   0.07652  -0.0443   0.0138   1.0000
  16.750   1.5037   0.08713   0.08101  -0.0452   0.0130   1.0000
  17.000   1.4971   0.09144   0.08543  -0.0461   0.0125   1.0000
  17.250   1.4894   0.09593   0.09003  -0.0472   0.0120   1.0000
  17.500   1.4806   0.10066   0.09488  -0.0485   0.0115   1.0000
  17.750   1.4715   0.10553   0.09985  -0.0499   0.0112   1.0000
  18.000   1.4603   0.11081   0.10525  -0.0516   0.0107   1.0000
  18.250   1.4508   0.11586   0.11041  -0.0533   0.0105   1.0000
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