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GOE 13K AIRFOIL (goe13k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 13K AIRFOIL (goe13k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.89 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe13k-il-1000000-n5.txt
Download as CSV file: xf-goe13k-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.8354   0.03301   0.02971  -0.2006   0.9384   0.0321
 -17.000  -0.8322   0.03065   0.02724  -0.2021   0.9357   0.0324
 -16.750  -0.8190   0.02909   0.02562  -0.2035   0.9339   0.0328
 -16.500  -0.8016   0.02783   0.02429  -0.2049   0.9327   0.0331
 -16.250  -0.7867   0.02720   0.02362  -0.2046   0.9291   0.0337
 -16.000  -0.7805   0.02563   0.02192  -0.2044   0.9256   0.0338
 -15.750  -0.7587   0.02492   0.02114  -0.2052   0.9234   0.0344
 -15.500  -0.7381   0.02397   0.02009  -0.2061   0.9214   0.0347
 -15.250  -0.7123   0.02325   0.01928  -0.2076   0.9198   0.0353
 -15.000  -0.6986   0.02235   0.01826  -0.2069   0.9163   0.0356
 -14.750  -0.6823   0.02166   0.01746  -0.2062   0.9128   0.0358
 -14.500  -0.6608   0.02110   0.01680  -0.2063   0.9099   0.0361
 -14.250  -0.6402   0.02036   0.01595  -0.2065   0.9071   0.0365
 -14.000  -0.6173   0.01972   0.01523  -0.2069   0.9046   0.0368
 -13.750  -0.6076   0.01963   0.01512  -0.2038   0.9007   0.0372
 -13.500  -0.5991   0.01916   0.01458  -0.2009   0.8966   0.0374
 -13.250  -0.5770   0.01912   0.01452  -0.2002   0.8939   0.0378
 -13.000  -0.5574   0.01877   0.01410  -0.1993   0.8911   0.0380
 -12.750  -0.5326   0.01857   0.01385  -0.1993   0.8888   0.0384
 -12.500  -0.5373   0.01835   0.01359  -0.1931   0.8849   0.0385
 -12.250  -0.5257   0.01819   0.01340  -0.1901   0.8817   0.0389
 -12.000  -0.5111   0.01784   0.01298  -0.1879   0.8787   0.0392
 -11.750  -0.4938   0.01738   0.01243  -0.1864   0.8761   0.0394
 -11.500  -0.4731   0.01694   0.01191  -0.1855   0.8739   0.0397
 -11.250  -0.4518   0.01654   0.01143  -0.1847   0.8718   0.0400
 -11.000  -0.4457   0.01629   0.01113  -0.1805   0.8691   0.0403
 -10.750  -0.4360   0.01598   0.01077  -0.1770   0.8662   0.0405
 -10.500  -0.4216   0.01566   0.01038  -0.1745   0.8633   0.0407
 -10.250  -0.4046   0.01527   0.00991  -0.1727   0.8607   0.0408
 -10.000  -0.3838   0.01492   0.00948  -0.1715   0.8585   0.0410
  -9.750  -0.3600   0.01460   0.00909  -0.1710   0.8565   0.0413
  -9.500  -0.3422   0.01437   0.00880  -0.1692   0.8544   0.0414
  -9.250  -0.3331   0.01421   0.00861  -0.1653   0.8518   0.0415
  -9.000  -0.3221   0.01380   0.00815  -0.1620   0.8491   0.0418
  -8.750  -0.3069   0.01341   0.00770  -0.1596   0.8465   0.0421
  -8.500  -0.2882   0.01309   0.00735  -0.1579   0.8441   0.0424
  -8.250  -0.2669   0.01280   0.00701  -0.1567   0.8419   0.0426
  -8.000  -0.2424   0.01256   0.00672  -0.1562   0.8397   0.0429
  -7.750  -0.2260   0.01235   0.00649  -0.1539   0.8374   0.0431
  -7.500  -0.2119   0.01220   0.00633  -0.1511   0.8348   0.0434
  -7.250  -0.1952   0.01205   0.00615  -0.1488   0.8322   0.0437
  -7.000  -0.1762   0.01187   0.00595  -0.1470   0.8297   0.0439
  -6.750  -0.1555   0.01168   0.00572  -0.1456   0.8273   0.0442
  -6.500  -0.1331   0.01148   0.00548  -0.1445   0.8252   0.0445
  -6.250  -0.1084   0.01128   0.00524  -0.1440   0.8232   0.0448
  -6.000  -0.0931   0.01115   0.00510  -0.1413   0.8208   0.0451
  -5.750  -0.0782   0.01105   0.00498  -0.1385   0.8182   0.0455
  -5.500  -0.0602   0.01094   0.00485  -0.1365   0.8156   0.0458
  -5.250  -0.0402   0.01081   0.00470  -0.1348   0.8130   0.0461
  -5.000  -0.0192   0.01064   0.00449  -0.1334   0.8102   0.0464
  -4.750   0.0045   0.01048   0.00429  -0.1326   0.8075   0.0465
  -4.500   0.0207   0.01040   0.00419  -0.1301   0.8042   0.0469
  -4.250   0.0370   0.01030   0.00408  -0.1276   0.8007   0.0471
  -4.000   0.0558   0.01022   0.00397  -0.1256   0.7973   0.0474
  -3.750   0.0764   0.01012   0.00385  -0.1241   0.7945   0.0475
  -3.500   0.0990   0.01001   0.00370  -0.1230   0.7916   0.0477
  -3.250   0.1142   0.00990   0.00359  -0.1202   0.7883   0.0481
  -3.000   0.1318   0.00978   0.00347  -0.1180   0.7854   0.0487
  -2.750   0.1517   0.00968   0.00336  -0.1163   0.7828   0.0492
  -2.500   0.1729   0.00960   0.00328  -0.1149   0.7803   0.0497
  -2.250   0.1952   0.00953   0.00319  -0.1138   0.7775   0.0503
  -2.000   0.2182   0.00947   0.00312  -0.1128   0.7750   0.0509
  -1.750   0.2368   0.00944   0.00310  -0.1108   0.7722   0.0514
  -1.500   0.2549   0.00941   0.00307  -0.1087   0.7686   0.0520
  -1.250   0.2753   0.00938   0.00305  -0.1071   0.7660   0.0527
  -1.000   0.2969   0.00935   0.00301  -0.1058   0.7634   0.0532
  -0.750   0.3200   0.00932   0.00296  -0.1048   0.7610   0.0540
  -0.500   0.3420   0.00930   0.00294  -0.1036   0.7586   0.0543
  -0.250   0.3619   0.00930   0.00296  -0.1019   0.7560   0.0547
   0.000   0.3807   0.00929   0.00296  -0.1000   0.7518   0.0556
   0.250   0.4030   0.00927   0.00295  -0.0989   0.7493   0.0568
   0.500   0.4259   0.00926   0.00294  -0.0979   0.7465   0.0580
   0.750   0.4496   0.00925   0.00293  -0.0971   0.7436   0.0599
   1.000   0.4701   0.00927   0.00298  -0.0956   0.7413   0.0614
   1.250   0.4905   0.00931   0.00305  -0.0941   0.7385   0.0625
   1.500   0.5116   0.00934   0.00310  -0.0927   0.7352   0.0654
   1.750   0.5341   0.00935   0.00314  -0.0917   0.7321   0.0704
   2.000   0.5574   0.00935   0.00318  -0.0908   0.7281   0.0833
   2.250   0.5815   0.00931   0.00329  -0.0903   0.7252   0.1277
   2.500   0.6037   0.00934   0.00341  -0.0893   0.7214   0.1457
   2.750   0.6267   0.00939   0.00351  -0.0884   0.7177   0.1611
   3.000   0.6495   0.00944   0.00360  -0.0876   0.7132   0.1807
   3.500   0.9164   0.00976   0.00586  -0.1383   0.6458   0.9970
   3.750   0.8878   0.01181   0.00741  -0.1275   0.5370   1.0000
   4.000   0.8555   0.01362   0.00882  -0.1159   0.4584   1.0000
   4.250   0.8566   0.01448   0.00951  -0.1110   0.4249   1.0000
   4.500   0.8644   0.01513   0.01006  -0.1074   0.4047   1.0000
   4.750   0.8758   0.01568   0.01052  -0.1046   0.3865   1.0000
   5.000   0.8940   0.01599   0.01082  -0.1030   0.3817   1.0000
   5.250   0.9101   0.01640   0.01120  -0.1010   0.3716   1.0000
   5.500   0.9251   0.01685   0.01161  -0.0989   0.3621   1.0000
   5.750   0.9418   0.01725   0.01198  -0.0971   0.3525   1.0000
   6.000   0.9581   0.01767   0.01236  -0.0952   0.3433   1.0000
   6.250   0.9728   0.01817   0.01281  -0.0931   0.3295   1.0000
   6.500   0.9857   0.01876   0.01333  -0.0908   0.3122   1.0000
   6.750   0.9983   0.01937   0.01385  -0.0884   0.2922   1.0000
   7.000   1.0072   0.02015   0.01448  -0.0854   0.2620   1.0000
   7.500   1.0231   0.02190   0.01590  -0.0794   0.1993   1.0000
   7.750   1.0347   0.02262   0.01650  -0.0771   0.1750   1.0000
   8.000   1.0479   0.02328   0.01705  -0.0750   0.1555   1.0000
   8.250   1.0623   0.02389   0.01760  -0.0732   0.1413   1.0000
   8.500   1.0765   0.02453   0.01817  -0.0713   0.1281   1.0000
   8.750   1.0915   0.02514   0.01872  -0.0696   0.1172   1.0000
   9.000   1.1078   0.02568   0.01923  -0.0681   0.1103   1.0000
   9.250   1.1239   0.02624   0.01976  -0.0666   0.1023   1.0000
   9.500   1.1401   0.02680   0.02029  -0.0652   0.0974   1.0000
   9.750   1.1561   0.02738   0.02086  -0.0638   0.0926   1.0000
  10.000   1.1718   0.02798   0.02144  -0.0623   0.0874   1.0000
  10.250   1.1876   0.02858   0.02203  -0.0608   0.0832   1.0000
  10.500   1.2041   0.02914   0.02258  -0.0596   0.0795   1.0000
  10.750   1.2192   0.02978   0.02320  -0.0581   0.0749   1.0000
  11.000   1.2346   0.03043   0.02385  -0.0567   0.0723   1.0000
  11.250   1.2500   0.03108   0.02450  -0.0553   0.0688   1.0000
  11.500   1.2655   0.03173   0.02515  -0.0540   0.0667   1.0000
  11.750   1.2806   0.03240   0.02582  -0.0526   0.0646   1.0000
  12.000   1.2961   0.03306   0.02650  -0.0513   0.0628   1.0000
  12.250   1.3108   0.03375   0.02722  -0.0500   0.0612   1.0000
  12.500   1.3253   0.03448   0.02797  -0.0486   0.0589   1.0000
  12.750   1.3396   0.03523   0.02872  -0.0472   0.0573   1.0000
  13.000   1.3535   0.03601   0.02951  -0.0459   0.0553   1.0000
  13.250   1.3675   0.03678   0.03032  -0.0445   0.0538   1.0000
  13.500   1.3810   0.03760   0.03117  -0.0432   0.0522   1.0000
  13.750   1.3943   0.03844   0.03202  -0.0419   0.0502   1.0000
  14.000   1.4068   0.03935   0.03293  -0.0405   0.0484   1.0000
  14.250   1.4194   0.04025   0.03387  -0.0391   0.0463   1.0000
  14.500   1.4312   0.04121   0.03484  -0.0377   0.0442   1.0000
  14.750   1.4420   0.04225   0.03588  -0.0363   0.0412   1.0000
  15.000   1.4534   0.04326   0.03691  -0.0349   0.0387   1.0000
  15.250   1.4624   0.04447   0.03813  -0.0334   0.0360   1.0000
  15.500   1.4724   0.04561   0.03930  -0.0319   0.0335   1.0000
  15.750   1.4811   0.04687   0.04056  -0.0305   0.0311   1.0000
  16.000   1.4886   0.04824   0.04196  -0.0289   0.0287   1.0000
  16.250   1.4964   0.04960   0.04334  -0.0275   0.0270   1.0000
  16.500   1.5036   0.05102   0.04479  -0.0260   0.0255   1.0000
  16.750   1.5101   0.05253   0.04634  -0.0246   0.0240   1.0000
  17.000   1.5164   0.05406   0.04791  -0.0232   0.0228   1.0000
  17.250   1.5216   0.05573   0.04962  -0.0218   0.0219   1.0000
  17.500   1.5281   0.05731   0.05125  -0.0206   0.0211   1.0000
  17.750   1.5323   0.05911   0.05310  -0.0192   0.0197   1.0000
  18.000   1.5348   0.06111   0.05514  -0.0179   0.0187   1.0000
  18.250   1.5393   0.06294   0.05703  -0.0168   0.0185   1.0000
  18.500   1.5427   0.06490   0.05905  -0.0157   0.0175   1.0000
  18.750   1.5463   0.06687   0.06108  -0.0147   0.0173   1.0000
  19.000   1.5478   0.06910   0.06338  -0.0137   0.0166   1.0000
  19.250   1.5481   0.07149   0.06583  -0.0127   0.0160   1.0000
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