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GOE 627 AIRFOIL (goe627-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 627 AIRFOIL (goe627-il)
Reynolds number: 500,000
Max Cl/Cd: 71.89 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe627-il-500000-n5.txt
Download as CSV file: xf-goe627-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 627 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.7671   0.05779   0.05444  -0.0875   0.9974   0.0177
 -14.750  -0.7756   0.05130   0.04777  -0.0943   0.9955   0.0178
 -14.500  -0.7846   0.04569   0.04197  -0.0998   0.9935   0.0179
 -14.250  -0.7862   0.04222   0.03836  -0.1024   0.9910   0.0181
 -14.000  -0.7826   0.03955   0.03556  -0.1043   0.9884   0.0182
 -13.750  -0.7794   0.03695   0.03280  -0.1057   0.9860   0.0184
 -13.500  -0.7707   0.03486   0.03056  -0.1069   0.9841   0.0187
 -13.250  -0.7650   0.03302   0.02855  -0.1067   0.9814   0.0190
 -13.000  -0.7610   0.03137   0.02673  -0.1054   0.9773   0.0193
 -12.750  -0.7521   0.02966   0.02478  -0.1048   0.9744   0.0198
 -12.500  -0.7381   0.02814   0.02302  -0.1045   0.9724   0.0202
 -12.250  -0.7188   0.02696   0.02172  -0.1045   0.9710   0.0205
 -12.000  -0.7146   0.02638   0.02110  -0.1009   0.9648   0.0206
 -11.750  -0.6950   0.02577   0.02046  -0.1002   0.9620   0.0209
 -11.500  -0.6710   0.02513   0.01978  -0.1002   0.9602   0.0212
 -11.250  -0.6442   0.02433   0.01890  -0.1009   0.9588   0.0215
 -11.000  -0.6141   0.02346   0.01794  -0.1021   0.9576   0.0220
 -10.750  -0.6048   0.02287   0.01725  -0.0989   0.9502   0.0224
 -10.500  -0.5794   0.02202   0.01627  -0.0990   0.9475   0.0228
 -10.250  -0.5515   0.02119   0.01530  -0.0995   0.9456   0.0234
 -10.000  -0.5226   0.02055   0.01451  -0.1001   0.9440   0.0239
  -9.750  -0.4935   0.01969   0.01363  -0.1009   0.9426   0.0243
  -9.500  -0.4839   0.01928   0.01320  -0.0974   0.9358   0.0246
  -9.250  -0.4597   0.01875   0.01263  -0.0970   0.9323   0.0249
  -9.000  -0.4318   0.01818   0.01202  -0.0972   0.9297   0.0253
  -8.750  -0.4022   0.01763   0.01141  -0.0978   0.9275   0.0259
  -8.500  -0.3828   0.01721   0.01093  -0.0961   0.9225   0.0264
  -8.250  -0.3630   0.01676   0.01042  -0.0945   0.9171   0.0268
  -8.000  -0.3359   0.01626   0.00986  -0.0944   0.9133   0.0273
  -7.750  -0.3050   0.01576   0.00928  -0.0951   0.9104   0.0277
  -7.500  -0.2903   0.01532   0.00881  -0.0924   0.9025   0.0280
  -7.250  -0.2651   0.01473   0.00821  -0.0919   0.8967   0.0285
  -7.000  -0.2417   0.01431   0.00777  -0.0910   0.8887   0.0290
  -6.750  -0.2153   0.01391   0.00734  -0.0906   0.8800   0.0296
  -6.500  -0.1924   0.01354   0.00694  -0.0895   0.8703   0.0301
  -6.250  -0.1643   0.01314   0.00648  -0.0895   0.8611   0.0306
  -6.000  -0.1413   0.01283   0.00611  -0.0884   0.8486   0.0311
  -5.750  -0.1164   0.01253   0.00575  -0.0876   0.8354   0.0316
  -5.500  -0.0912   0.01227   0.00541  -0.0869   0.8217   0.0321
  -5.250  -0.0677   0.01199   0.00505  -0.0859   0.8066   0.0326
  -5.000  -0.0451   0.01173   0.00473  -0.0847   0.7899   0.0333
  -4.750  -0.0230   0.01154   0.00446  -0.0834   0.7711   0.0340
  -4.500  -0.0014   0.01141   0.00423  -0.0819   0.7511   0.0346
  -4.250   0.0190   0.01132   0.00402  -0.0802   0.7285   0.0353
  -4.000   0.0383   0.01126   0.00384  -0.0782   0.7046   0.0360
  -3.750   0.0575   0.01123   0.00368  -0.0762   0.6807   0.0367
  -3.500   0.0772   0.01118   0.00353  -0.0743   0.6610   0.0375
  -3.250   0.0968   0.01111   0.00338  -0.0725   0.6430   0.0389
  -3.000   0.1171   0.01106   0.00327  -0.0708   0.6268   0.0406
  -2.750   0.1370   0.01105   0.00317  -0.0690   0.6086   0.0425
  -2.500   0.1570   0.01100   0.00307  -0.0672   0.5924   0.0460
  -2.250   0.1768   0.01095   0.00299  -0.0654   0.5762   0.0534
  -2.000   0.1960   0.01087   0.00291  -0.0635   0.5602   0.0735
  -1.750   0.2123   0.01062   0.00281  -0.0612   0.5441   0.1316
  -1.500   0.2303   0.01052   0.00276  -0.0591   0.5265   0.1678
  -1.250   0.2456   0.01033   0.00272  -0.0566   0.5068   0.2321
  -1.000   0.2618   0.01021   0.00271  -0.0542   0.4881   0.2923
  -0.750   0.2778   0.01012   0.00269  -0.0517   0.4697   0.3405
  -0.500   0.2931   0.01004   0.00269  -0.0491   0.4529   0.3870
  -0.250   0.3058   0.00984   0.00269  -0.0460   0.4386   0.4666
   0.000   0.3160   0.00958   0.00270  -0.0423   0.4252   0.5674
   0.250   0.3266   0.00935   0.00275  -0.0386   0.4131   0.6594
   0.500   0.3391   0.00924   0.00284  -0.0352   0.4017   0.7322
   0.750   0.3543   0.00920   0.00298  -0.0323   0.3897   0.8011
   1.000   0.3781   0.00925   0.00314  -0.0312   0.3778   0.8549
   1.250   0.4160   0.00945   0.00336  -0.0333   0.3644   0.8999
   1.500   0.4578   0.00972   0.00356  -0.0363   0.3509   0.9218
   1.750   0.5006   0.01002   0.00376  -0.0397   0.3375   0.9328
   2.000   0.5452   0.01030   0.00397  -0.0433   0.3265   0.9445
   2.250   0.5822   0.01058   0.00417  -0.0453   0.3172   0.9559
   2.500   0.6204   0.01084   0.00436  -0.0476   0.3078   0.9606
   2.750   0.6507   0.01109   0.00454  -0.0482   0.3005   0.9681
   3.000   0.6850   0.01133   0.00473  -0.0497   0.2924   0.9730
   3.250   0.7188   0.01161   0.00492  -0.0512   0.2851   0.9780
   3.500   0.7495   0.01182   0.00510  -0.0519   0.2786   0.9831
   3.750   0.7827   0.01205   0.00526  -0.0533   0.2718   0.9858
   4.000   0.8142   0.01226   0.00543  -0.0543   0.2669   0.9890
   4.250   0.8447   0.01246   0.00561  -0.0552   0.2619   0.9923
   4.500   0.8757   0.01268   0.00579  -0.0562   0.2570   0.9952
   4.750   0.9073   0.01293   0.00599  -0.0573   0.2525   0.9979
   5.000   0.9401   0.01312   0.00617  -0.0587   0.2485   0.9998
   5.250   0.9529   0.01326   0.00630  -0.0559   0.2454   1.0000
   5.500   0.9640   0.01341   0.00644  -0.0527   0.2423   1.0000
   5.750   0.9756   0.01360   0.00662  -0.0497   0.2394   1.0000
   6.000   0.9880   0.01383   0.00681  -0.0468   0.2364   1.0000
   6.250   1.0033   0.01400   0.00700  -0.0445   0.2339   1.0000
   6.500   1.0189   0.01419   0.00720  -0.0424   0.2311   1.0000
   6.750   1.0346   0.01441   0.00742  -0.0402   0.2286   1.0000
   7.000   1.0500   0.01466   0.00766  -0.0381   0.2255   1.0000
   7.250   1.0650   0.01496   0.00794  -0.0359   0.2224   1.0000
   7.500   1.0805   0.01526   0.00823  -0.0339   0.2195   1.0000
   7.750   1.0986   0.01549   0.00849  -0.0323   0.2174   1.0000
   8.000   1.1161   0.01575   0.00878  -0.0307   0.2155   1.0000
   8.250   1.1333   0.01604   0.00909  -0.0291   0.2132   1.0000
   8.500   1.1503   0.01636   0.00941  -0.0275   0.2107   1.0000
   8.750   1.1664   0.01674   0.00978  -0.0258   0.2077   1.0000
   9.000   1.1816   0.01716   0.01020  -0.0240   0.2043   1.0000
   9.250   1.2000   0.01747   0.01055  -0.0227   0.2026   1.0000
   9.500   1.2182   0.01780   0.01092  -0.0215   0.2005   1.0000
   9.750   1.2355   0.01817   0.01133  -0.0201   0.1982   1.0000
  10.000   1.2523   0.01859   0.01177  -0.0187   0.1959   1.0000
  10.250   1.2687   0.01903   0.01223  -0.0173   0.1938   1.0000
  10.500   1.2841   0.01954   0.01276  -0.0159   0.1915   1.0000
  10.750   1.2993   0.02007   0.01331  -0.0144   0.1893   1.0000
  11.000   1.3168   0.02050   0.01380  -0.0133   0.1877   1.0000
  11.250   1.3338   0.02097   0.01433  -0.0122   0.1854   1.0000
  11.500   1.3501   0.02149   0.01489  -0.0110   0.1830   1.0000
  11.750   1.3652   0.02208   0.01551  -0.0098   0.1804   1.0000
  12.000   1.3792   0.02274   0.01620  -0.0085   0.1776   1.0000
  12.250   1.3923   0.02347   0.01696  -0.0072   0.1750   1.0000
  12.500   1.4087   0.02404   0.01760  -0.0062   0.1711   1.0000
  12.750   1.4219   0.02481   0.01839  -0.0050   0.1658   1.0000
  13.000   1.4328   0.02574   0.01932  -0.0037   0.1615   1.0000
  13.250   1.4464   0.02654   0.02017  -0.0027   0.1564   1.0000
  13.500   1.4565   0.02758   0.02122  -0.0015   0.1507   1.0000
  13.750   1.4662   0.02869   0.02235  -0.0003   0.1445   1.0000
  14.000   1.4745   0.02995   0.02362   0.0009   0.1387   1.0000
  14.250   1.4815   0.03133   0.02503   0.0020   0.1323   1.0000
  14.500   1.4861   0.03296   0.02666   0.0032   0.1256   1.0000
  14.750   1.4908   0.03464   0.02837   0.0042   0.1195   1.0000
  15.000   1.4913   0.03675   0.03049   0.0052   0.1129   1.0000
  15.250   1.4939   0.03876   0.03253   0.0060   0.1074   1.0000
  15.500   1.4949   0.04096   0.03478   0.0067   0.1037   1.0000
  15.750   1.4958   0.04326   0.03713   0.0073   0.1003   1.0000
  16.000   1.4956   0.04575   0.03968   0.0077   0.0968   1.0000
  16.250   1.4919   0.04866   0.04265   0.0080   0.0935   1.0000
  16.500   1.4892   0.05156   0.04561   0.0081   0.0913   1.0000
  16.750   1.4870   0.05448   0.04861   0.0081   0.0886   1.0000
  17.000   1.4841   0.05755   0.05177   0.0079   0.0869   1.0000
  17.250   1.4758   0.06134   0.05564   0.0075   0.0845   1.0000
  17.500   1.4685   0.06508   0.05948   0.0070   0.0832   1.0000
  17.750   1.4574   0.06940   0.06388   0.0062   0.0806   1.0000
  18.000   1.4517   0.07311   0.06770   0.0055   0.0794   1.0000
  18.250   1.4439   0.07715   0.07184   0.0046   0.0782   1.0000
  18.500   1.4299   0.08207   0.07685   0.0034   0.0760   1.0000
  18.750   1.4180   0.08680   0.08169   0.0021   0.0749   1.0000
  19.000   1.4018   0.09219   0.08717   0.0005   0.0735   1.0000
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