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GOE 13K AIRFOIL (goe13k-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 13K AIRFOIL (goe13k-il)
Reynolds number: 500,000
Max Cl/Cd: 85.81 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe13k-il-500000-n5.txt
Download as CSV file: xf-goe13k-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 13K 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.0904   0.10120   0.09801  -0.1553   0.9245   0.0323
 -13.000  -0.3944   0.04023   0.03655  -0.1977   0.9166   0.0406
 -12.750  -0.4452   0.03459   0.03051  -0.1968   0.9093   0.0409
 -12.500  -0.4596   0.03144   0.02697  -0.1951   0.9064   0.0414
 -12.250  -0.4548   0.02943   0.02471  -0.1943   0.9045   0.0417
 -12.000  -0.4840   0.02920   0.02443  -0.1839   0.8966   0.0418
 -11.750  -0.4757   0.02821   0.02335  -0.1816   0.8937   0.0421
 -11.500  -0.4588   0.02715   0.02218  -0.1810   0.8918   0.0423
 -11.250  -0.4354   0.02634   0.02129  -0.1813   0.8903   0.0426
 -11.000  -0.4102   0.02546   0.02030  -0.1821   0.8890   0.0429
 -10.750  -0.4301   0.02532   0.02013  -0.1727   0.8826   0.0430
 -10.500  -0.4223   0.02473   0.01946  -0.1694   0.8793   0.0433
 -10.250  -0.4057   0.02416   0.01879  -0.1679   0.8770   0.0436
 -10.000  -0.3859   0.02332   0.01782  -0.1672   0.8752   0.0440
  -9.750  -0.3628   0.02241   0.01676  -0.1671   0.8737   0.0444
  -9.500  -0.3364   0.02150   0.01570  -0.1677   0.8724   0.0449
  -9.250  -0.3564   0.02144   0.01560  -0.1578   0.8662   0.0450
  -9.000  -0.3474   0.02082   0.01486  -0.1544   0.8629   0.0453
  -8.750  -0.3303   0.02025   0.01417  -0.1526   0.8606   0.0458
  -8.500  -0.3085   0.01960   0.01339  -0.1518   0.8589   0.0462
  -8.250  -0.2831   0.01895   0.01260  -0.1518   0.8575   0.0466
  -8.000  -0.2550   0.01834   0.01186  -0.1523   0.8563   0.0470
  -7.750  -0.2494   0.01803   0.01148  -0.1478   0.8530   0.0471
  -7.500  -0.2511   0.01792   0.01130  -0.1416   0.8484   0.0473
  -7.250  -0.2348   0.01758   0.01087  -0.1394   0.8457   0.0476
  -7.000  -0.2133   0.01714   0.01035  -0.1383   0.8436   0.0478
  -6.750  -0.1883   0.01639   0.00952  -0.1381   0.8420   0.0483
  -6.500  -0.1597   0.01586   0.00894  -0.1385   0.8407   0.0487
  -6.250  -0.1291   0.01541   0.00844  -0.1394   0.8396   0.0491
  -6.000  -0.1281   0.01536   0.00837  -0.1338   0.8357   0.0493
  -5.750  -0.1210   0.01527   0.00827  -0.1294   0.8320   0.0496
  -5.500  -0.1027   0.01509   0.00807  -0.1274   0.8295   0.0502
  -5.250  -0.0802   0.01484   0.00779  -0.1264   0.8275   0.0506
  -5.000  -0.0544   0.01451   0.00741  -0.1261   0.8259   0.0510
  -4.750  -0.0256   0.01419   0.00704  -0.1265   0.8247   0.0514
  -4.500   0.0049   0.01388   0.00669  -0.1272   0.8235   0.0519
  -4.250   0.0201   0.01374   0.00653  -0.1246   0.8210   0.0523
  -4.000   0.0177   0.01381   0.00659  -0.1180   0.8162   0.0527
  -3.750   0.0354   0.01366   0.00641  -0.1159   0.8134   0.0530
  -3.500   0.0588   0.01341   0.00614  -0.1150   0.8109   0.0534
  -3.250   0.0867   0.01319   0.00587  -0.1151   0.8093   0.0539
  -3.000   0.1192   0.01292   0.00557  -0.1162   0.8077   0.0544
  -2.750   0.1315   0.01286   0.00550  -0.1129   0.8044   0.0546
  -2.500   0.1357   0.01293   0.00556  -0.1078   0.7997   0.0549
  -2.250   0.1529   0.01274   0.00537  -0.1055   0.7969   0.0558
  -2.000   0.1763   0.01255   0.00519  -0.1047   0.7950   0.0567
  -1.750   0.2048   0.01236   0.00499  -0.1049   0.7934   0.0574
  -1.500   0.2362   0.01215   0.00478  -0.1057   0.7919   0.0585
  -1.250   0.2518   0.01214   0.00477  -0.1031   0.7892   0.0592
  -1.000   0.2561   0.01227   0.00492  -0.0981   0.7847   0.0598
  -0.750   0.2746   0.01224   0.00488  -0.0961   0.7818   0.0607
  -0.500   0.2988   0.01215   0.00479  -0.0954   0.7795   0.0616
  -0.250   0.3281   0.01201   0.00464  -0.0958   0.7776   0.0626
   0.000   0.3591   0.01187   0.00450  -0.0965   0.7762   0.0638
   0.250   0.3753   0.01190   0.00455  -0.0941   0.7733   0.0655
   0.500   0.3823   0.01207   0.00476  -0.0898   0.7693   0.0669
   0.750   0.4007   0.01210   0.00481  -0.0879   0.7661   0.0700
   1.000   0.4251   0.01207   0.00479  -0.0872   0.7640   0.0731
   1.250   0.4553   0.01193   0.00469  -0.0878   0.7618   0.0788
   1.500   0.4871   0.01175   0.00464  -0.0888   0.7604   0.1091
   1.750   0.5031   0.01183   0.00482  -0.0865   0.7572   0.1351
   2.000   0.5129   0.01204   0.00510  -0.0829   0.7529   0.1498
   2.250   0.5335   0.01209   0.00522  -0.0815   0.7497   0.1686
   2.500   0.5626   0.01196   0.00525  -0.0821   0.7474   0.2124
   3.000   0.9215   0.01099   0.00656  -0.1521   0.7493   1.0000
   3.250   0.9448   0.01101   0.00655  -0.1513   0.7453   1.0000
   3.500   0.9533   0.01125   0.00679  -0.1472   0.7380   1.0000
   3.750   0.9685   0.01139   0.00692  -0.1447   0.7309   1.0000
   4.000   0.9758   0.01166   0.00716  -0.1404   0.7191   1.0000
   4.250   0.9832   0.01194   0.00738  -0.1361   0.7011   1.0000
   4.500   0.9883   0.01231   0.00765  -0.1314   0.6776   1.0000
   4.750   0.9734   0.01321   0.00827  -0.1227   0.6140   1.0000
   5.000   0.9188   0.01564   0.01013  -0.1068   0.5104   1.0000
   5.250   0.8968   0.01743   0.01158  -0.0979   0.4545   1.0000
   5.500   0.9021   0.01827   0.01231  -0.0941   0.4333   1.0000
   5.750   0.9118   0.01897   0.01293  -0.0911   0.4165   1.0000
   6.000   0.9254   0.01953   0.01344  -0.0888   0.4058   1.0000
   6.250   0.9398   0.02006   0.01394  -0.0867   0.3955   1.0000
   6.500   0.9532   0.02065   0.01448  -0.0845   0.3846   1.0000
   6.750   0.9703   0.02108   0.01491  -0.0829   0.3748   1.0000
   7.000   0.9846   0.02165   0.01544  -0.0808   0.3638   1.0000
   7.250   0.9997   0.02220   0.01596  -0.0790   0.3514   1.0000
   7.500   1.0147   0.02276   0.01649  -0.0771   0.3387   1.0000
   7.750   1.0278   0.02342   0.01708  -0.0750   0.3198   1.0000
   8.000   1.0383   0.02423   0.01777  -0.0726   0.2950   1.0000
   8.250   1.0466   0.02517   0.01855  -0.0698   0.2639   1.0000
   8.750   1.0627   0.02713   0.02013  -0.0644   0.1977   1.0000
   9.000   1.0733   0.02800   0.02088  -0.0622   0.1725   1.0000
   9.250   1.0857   0.02880   0.02158  -0.0603   0.1540   1.0000
   9.500   1.0991   0.02954   0.02225  -0.0585   0.1392   1.0000
   9.750   1.1133   0.03024   0.02290  -0.0569   0.1277   1.0000
  10.000   1.1270   0.03099   0.02360  -0.0552   0.1176   1.0000
  10.250   1.1413   0.03171   0.02430  -0.0536   0.1104   1.0000
  10.500   1.1559   0.03242   0.02500  -0.0521   0.1049   1.0000
  10.750   1.1705   0.03315   0.02571  -0.0507   0.0988   1.0000
  11.000   1.1846   0.03390   0.02646  -0.0492   0.0943   1.0000
  11.250   1.1994   0.03462   0.02720  -0.0478   0.0910   1.0000
  11.500   1.2125   0.03545   0.02801  -0.0462   0.0857   1.0000
  11.750   1.2259   0.03626   0.02883  -0.0447   0.0823   1.0000
  12.000   1.2408   0.03700   0.02960  -0.0434   0.0797   1.0000
  12.250   1.2539   0.03785   0.03047  -0.0420   0.0762   1.0000
  12.500   1.2662   0.03878   0.03141  -0.0405   0.0737   1.0000
  12.750   1.2794   0.03965   0.03230  -0.0391   0.0712   1.0000
  13.000   1.2928   0.04051   0.03320  -0.0378   0.0691   1.0000
  13.250   1.3051   0.04146   0.03417  -0.0364   0.0666   1.0000
  13.500   1.3160   0.04252   0.03525  -0.0349   0.0645   1.0000
  13.750   1.3279   0.04351   0.03627  -0.0335   0.0625   1.0000
  14.000   1.3401   0.04448   0.03730  -0.0322   0.0609   1.0000
  14.250   1.3513   0.04555   0.03842  -0.0309   0.0590   1.0000
  14.500   1.3612   0.04673   0.03961  -0.0294   0.0566   1.0000
  14.750   1.3710   0.04793   0.04085  -0.0280   0.0548   1.0000
  15.000   1.3818   0.04907   0.04205  -0.0268   0.0531   1.0000
  15.250   1.3919   0.05027   0.04331  -0.0255   0.0511   1.0000
  15.500   1.4011   0.05156   0.04463  -0.0242   0.0490   1.0000
  15.750   1.4088   0.05298   0.04610  -0.0228   0.0473   1.0000
  16.000   1.4179   0.05430   0.04748  -0.0216   0.0450   1.0000
  16.250   1.4257   0.05575   0.04896  -0.0204   0.0426   1.0000
  16.500   1.4318   0.05737   0.05063  -0.0191   0.0405   1.0000
  16.750   1.4389   0.05894   0.05224  -0.0179   0.0377   1.0000
  17.250   1.4487   0.06254   0.05594  -0.0156   0.0341   1.0000
  17.500   1.4525   0.06447   0.05793  -0.0144   0.0321   1.0000
  17.750   1.4545   0.06662   0.06010  -0.0133   0.0297   1.0000
  18.000   1.4569   0.06878   0.06233  -0.0123   0.0284   1.0000
  18.250   1.4586   0.07105   0.06467  -0.0114   0.0273   1.0000
  18.500   1.4580   0.07362   0.06730  -0.0105   0.0260   1.0000
  18.750   1.4584   0.07613   0.06990  -0.0097   0.0252   1.0000
  19.000   1.4583   0.07873   0.07259  -0.0091   0.0242   1.0000
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