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GOE 13K AIRFOIL (goe13k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 13K AIRFOIL (goe13k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 129 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe13k-il-1000000.txt
Download as CSV file: xf-goe13k-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.0399   0.12273   0.12051  -0.1570   0.9523   0.0305
 -14.250  -0.0248   0.11881   0.11657  -0.1613   0.9537   0.0310
 -13.750  -0.5047   0.03229   0.02908  -0.2065   0.9345   0.0385
 -13.500  -0.4918   0.03103   0.02776  -0.2070   0.9329   0.0388
 -13.250  -0.4679   0.03041   0.02712  -0.2082   0.9319   0.0390
 -13.000  -0.4403   0.02994   0.02664  -0.2097   0.9311   0.0393
 -12.750  -0.4326   0.02936   0.02601  -0.2077   0.9272   0.0395
 -12.500  -0.4282   0.02855   0.02511  -0.2051   0.9230   0.0397
 -12.250  -0.4049   0.02824   0.02479  -0.2054   0.9211   0.0400
 -12.000  -0.3924   0.02674   0.02312  -0.2050   0.9188   0.0404
 -11.750  -0.3691   0.02573   0.02198  -0.2061   0.9170   0.0409
 -11.500  -0.3880   0.02504   0.02119  -0.1976   0.9103   0.0410
 -11.250  -0.3747   0.02417   0.02018  -0.1960   0.9074   0.0416
 -11.000  -0.3560   0.02278   0.01859  -0.1959   0.9052   0.0421
 -10.750  -0.3294   0.02155   0.01715  -0.1973   0.9034   0.0425
 -10.500  -0.3410   0.02138   0.01690  -0.1893   0.8981   0.0428
 -10.250  -0.3311   0.02090   0.01631  -0.1862   0.8947   0.0430
 -10.000  -0.3197   0.01976   0.01497  -0.1838   0.8920   0.0433
  -9.750  -0.2985   0.01813   0.01319  -0.1839   0.8901   0.0439
  -9.500  -0.2655   0.01750   0.01250  -0.1858   0.8887   0.0443
  -9.250  -0.2645   0.01736   0.01234  -0.1803   0.8851   0.0446
  -9.000  -0.2605   0.01707   0.01200  -0.1755   0.8815   0.0448
  -8.750  -0.2423   0.01667   0.01155  -0.1738   0.8790   0.0452
  -8.500  -0.2198   0.01627   0.01110  -0.1730   0.8768   0.0456
  -8.250  -0.1929   0.01567   0.01040  -0.1733   0.8750   0.0458
  -8.000  -0.1599   0.01518   0.00984  -0.1749   0.8734   0.0464
  -7.750  -0.1480   0.01491   0.00952  -0.1717   0.8707   0.0467
  -7.500  -0.1480   0.01469   0.00926  -0.1657   0.8670   0.0470
  -7.250  -0.1310   0.01437   0.00888  -0.1635   0.8644   0.0475
  -7.000  -0.1086   0.01404   0.00849  -0.1626   0.8623   0.0479
  -6.750  -0.0839   0.01366   0.00804  -0.1621   0.8604   0.0482
  -6.500  -0.0532   0.01338   0.00768  -0.1630   0.8588   0.0486
  -6.250  -0.0179   0.01311   0.00735  -0.1649   0.8572   0.0488
  -6.000  -0.0168   0.01259   0.00679  -0.1592   0.8541   0.0493
  -5.750  -0.0092   0.01223   0.00640  -0.1549   0.8508   0.0496
  -5.500   0.0090   0.01190   0.00607  -0.1529   0.8483   0.0501
  -5.250   0.0320   0.01161   0.00577  -0.1520   0.8460   0.0505
  -5.000   0.0589   0.01138   0.00552  -0.1520   0.8442   0.0512
  -4.750   0.0940   0.01109   0.00521  -0.1538   0.8422   0.0517
  -4.500   0.1054   0.01100   0.00511  -0.1502   0.8389   0.0523
  -4.250   0.1082   0.01093   0.00503  -0.1446   0.8351   0.0527
  -4.000   0.1267   0.01077   0.00485  -0.1426   0.8324   0.0532
  -3.750   0.1490   0.01058   0.00464  -0.1414   0.8301   0.0537
  -3.500   0.1766   0.01039   0.00442  -0.1415   0.8279   0.0544
  -3.250   0.2108   0.01019   0.00419  -0.1430   0.8259   0.0548
  -3.000   0.2193   0.01016   0.00416  -0.1387   0.8228   0.0551
  -2.750   0.2279   0.01012   0.00411  -0.1344   0.8193   0.0553
  -2.500   0.2439   0.00989   0.00387  -0.1318   0.8166   0.0560
  -2.250   0.2638   0.00969   0.00366  -0.1301   0.8143   0.0568
  -2.000   0.2905   0.00951   0.00347  -0.1300   0.8122   0.0579
  -1.750   0.3238   0.00936   0.00333  -0.1313   0.8105   0.0591
  -1.500   0.3392   0.00933   0.00330  -0.1286   0.8077   0.0602
  -1.250   0.3454   0.00933   0.00331  -0.1237   0.8042   0.0606
  -1.000   0.3629   0.00928   0.00325  -0.1214   0.8013   0.0617
  -0.750   0.3839   0.00921   0.00318  -0.1199   0.7986   0.0624
  -0.500   0.4113   0.00912   0.00308  -0.1199   0.7968   0.0632
  -0.250   0.4428   0.00897   0.00293  -0.1208   0.7949   0.0663
   0.000   0.4680   0.00892   0.00290  -0.1203   0.7927   0.0684
   0.250   0.4761   0.00896   0.00297  -0.1160   0.7896   0.0698
   0.500   0.4913   0.00896   0.00298  -0.1132   0.7866   0.0738
   0.750   0.5117   0.00891   0.00298  -0.1116   0.7840   0.0803
   1.000   0.5368   0.00875   0.00300  -0.1112   0.7819   0.1290
   1.250   0.5680   0.00863   0.00297  -0.1121   0.7798   0.1647
   1.500   0.6043   0.00847   0.00295  -0.1142   0.7775   0.2082
   1.750   0.6174   0.00830   0.00314  -0.1113   0.7747   0.3306
   2.000   0.8606   0.00743   0.00408  -0.1617   0.7784   0.9774
   2.250   0.9257   0.00774   0.00439  -0.1702   0.7765   0.9887
   2.500   0.9712   0.00791   0.00459  -0.1744   0.7726   0.9949
   2.750   1.0178   0.00789   0.00450  -0.1788   0.7625   0.9996
   3.000   1.0242   0.00802   0.00465  -0.1742   0.7551   1.0000
   3.250   1.0344   0.00813   0.00470  -0.1703   0.7453   1.0000
   3.500   1.0358   0.00835   0.00490  -0.1646   0.7342   1.0000
   3.750   1.0441   0.00854   0.00507  -0.1604   0.7231   1.0000
   4.000   1.0509   0.00878   0.00526  -0.1559   0.7105   1.0000
   4.250   1.0573   0.00906   0.00549  -0.1513   0.6972   1.0000
   4.500   1.0642   0.00938   0.00576  -0.1470   0.6811   1.0000
   4.750   1.0633   0.00987   0.00618  -0.1410   0.6547   1.0000
   5.000   1.0161   0.01162   0.00752  -0.1256   0.5668   1.0000
   5.250   0.9748   0.01370   0.00917  -0.1122   0.4845   1.0000
   5.500   0.9737   0.01465   0.00997  -0.1070   0.4534   1.0000
   5.750   0.9825   0.01529   0.01054  -0.1036   0.4363   1.0000
   6.000   0.9937   0.01586   0.01104  -0.1007   0.4222   1.0000
   6.250   1.0062   0.01640   0.01155  -0.0981   0.4110   1.0000
   6.500   1.0203   0.01690   0.01202  -0.0959   0.3995   1.0000
   6.750   1.0334   0.01744   0.01251  -0.0935   0.3888   1.0000
   7.000   1.0503   0.01785   0.01291  -0.0917   0.3785   1.0000
   7.250   1.0638   0.01841   0.01344  -0.0895   0.3669   1.0000
   7.500   1.0771   0.01899   0.01395  -0.0872   0.3529   1.0000
   7.750   1.0907   0.01956   0.01446  -0.0850   0.3353   1.0000
   8.000   1.1026   0.02023   0.01505  -0.0826   0.3132   1.0000
   8.250   1.1093   0.02115   0.01580  -0.0794   0.2798   1.0000
   8.500   1.1119   0.02229   0.01668  -0.0756   0.2343   1.0000
   8.750   1.1183   0.02327   0.01748  -0.0725   0.2005   1.0000
   9.000   1.1259   0.02422   0.01825  -0.0697   0.1688   1.0000
   9.250   1.1359   0.02507   0.01895  -0.0672   0.1428   1.0000
   9.500   1.1485   0.02581   0.01958  -0.0652   0.1258   1.0000
   9.750   1.1622   0.02650   0.02022  -0.0634   0.1141   1.0000
  10.000   1.1759   0.02720   0.02086  -0.0616   0.1039   1.0000
  10.250   1.1912   0.02782   0.02146  -0.0600   0.0972   1.0000
  10.500   1.2058   0.02848   0.02208  -0.0584   0.0906   1.0000
  10.750   1.2214   0.02909   0.02269  -0.0570   0.0856   1.0000
  11.000   1.2355   0.02979   0.02337  -0.0554   0.0808   1.0000
  11.250   1.2496   0.03051   0.02408  -0.0538   0.0770   1.0000
  11.500   1.2656   0.03112   0.02472  -0.0525   0.0747   1.0000
  11.750   1.2804   0.03181   0.02540  -0.0510   0.0715   1.0000
  12.000   1.2936   0.03261   0.02618  -0.0494   0.0677   1.0000
  12.250   1.3085   0.03330   0.02691  -0.0481   0.0666   1.0000
  12.500   1.3229   0.03402   0.02765  -0.0467   0.0644   1.0000
  12.750   1.3366   0.03480   0.02843  -0.0452   0.0619   1.0000
  13.000   1.3487   0.03570   0.02932  -0.0436   0.0594   1.0000
  13.250   1.3636   0.03641   0.03008  -0.0424   0.0580   1.0000
  13.500   1.3770   0.03724   0.03093  -0.0410   0.0563   1.0000
  13.750   1.3895   0.03813   0.03184  -0.0396   0.0545   1.0000
  14.000   1.3996   0.03920   0.03290  -0.0379   0.0519   1.0000
  14.250   1.4139   0.03998   0.03374  -0.0367   0.0506   1.0000
  14.500   1.4264   0.04090   0.03470  -0.0354   0.0491   1.0000
  14.750   1.4376   0.04190   0.03570  -0.0340   0.0470   1.0000
  15.000   1.4468   0.04308   0.03689  -0.0323   0.0451   1.0000
  15.250   1.4593   0.04403   0.03789  -0.0311   0.0437   1.0000
  15.500   1.4703   0.04509   0.03897  -0.0298   0.0418   1.0000
  15.750   1.4782   0.04640   0.04029  -0.0282   0.0398   1.0000
  16.000   1.4879   0.04760   0.04155  -0.0269   0.0386   1.0000
  16.250   1.4976   0.04880   0.04277  -0.0256   0.0365   1.0000
  16.500   1.5051   0.05019   0.04418  -0.0241   0.0351   1.0000
  16.750   1.5115   0.05170   0.04573  -0.0227   0.0339   1.0000
  17.000   1.5201   0.05304   0.04712  -0.0214   0.0326   1.0000
  17.250   1.5260   0.05462   0.04874  -0.0200   0.0313   1.0000
  17.500   1.5287   0.05652   0.05066  -0.0185   0.0299   1.0000
  17.750   1.5355   0.05808   0.05228  -0.0173   0.0290   1.0000
  18.000   1.5397   0.05991   0.05418  -0.0161   0.0284   1.0000
  18.250   1.5437   0.06178   0.05608  -0.0149   0.0270   1.0000
  18.500   1.5452   0.06391   0.05826  -0.0137   0.0263   1.0000
  18.750   1.5453   0.06623   0.06064  -0.0125   0.0254   1.0000
  19.000   1.5487   0.06825   0.06274  -0.0115   0.0248   1.0000
  19.250   1.5499   0.07055   0.06511  -0.0106   0.0242   1.0000
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