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N-14 (n14-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: N-14 (n14-il)
Reynolds number: 500,000
Max Cl/Cd: 58.95 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n14-il-500000-n5.txt
Download as CSV file: xf-n14-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: N-14                                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.9072   0.14585   0.14310  -0.0026   1.0000   0.0129
 -18.750  -0.9604   0.13008   0.12715  -0.0110   1.0000   0.0128
 -18.500  -1.0020   0.11754   0.11445  -0.0176   1.0000   0.0128
 -18.250  -1.0386   0.10659   0.10336  -0.0234   1.0000   0.0127
 -18.000  -1.0747   0.09613   0.09273  -0.0289   1.0000   0.0126
 -17.750  -1.1072   0.08663   0.08307  -0.0340   1.0000   0.0125
 -17.500  -1.1368   0.07770   0.07398  -0.0389   1.0000   0.0125
 -17.250  -1.1622   0.06967   0.06576  -0.0433   1.0000   0.0124
 -17.000  -1.1793   0.06316   0.05912  -0.0470   1.0000   0.0126
 -16.750  -1.1938   0.05746   0.05327  -0.0500   1.0000   0.0126
 -16.500  -1.2075   0.05227   0.04791  -0.0524   1.0000   0.0127
 -16.250  -1.2130   0.04851   0.04405  -0.0538   1.0000   0.0130
 -16.000  -1.2193   0.04497   0.04038  -0.0547   1.0000   0.0132
 -15.750  -1.2189   0.04240   0.03771  -0.0551   1.0000   0.0137
 -15.500  -1.2208   0.03978   0.03496  -0.0550   1.0000   0.0140
 -15.250  -1.2199   0.03759   0.03265  -0.0546   1.0000   0.0145
 -15.000  -1.2190   0.03555   0.03048  -0.0538   1.0000   0.0148
 -14.750  -1.2173   0.03369   0.02849  -0.0527   1.0000   0.0151
 -14.500  -1.2145   0.03204   0.02674  -0.0514   1.0000   0.0155
 -14.250  -1.2082   0.03076   0.02541  -0.0500   1.0000   0.0160
 -14.000  -1.1997   0.02969   0.02429  -0.0486   1.0000   0.0166
 -13.750  -1.1928   0.02857   0.02308  -0.0469   1.0000   0.0170
 -13.500  -1.1824   0.02773   0.02217  -0.0453   1.0000   0.0177
 -13.250  -1.1729   0.02687   0.02122  -0.0434   1.0000   0.0184
 -13.000  -1.1636   0.02603   0.02026  -0.0414   1.0000   0.0190
 -12.750  -1.1550   0.02519   0.01934  -0.0391   1.0000   0.0195
 -12.500  -1.1459   0.02445   0.01856  -0.0368   1.0000   0.0201
 -12.250  -1.1353   0.02385   0.01791  -0.0345   1.0000   0.0206
 -12.000  -1.1245   0.02330   0.01730  -0.0320   1.0000   0.0212
 -11.750  -1.1138   0.02279   0.01674  -0.0295   1.0000   0.0219
 -11.500  -1.1038   0.02231   0.01619  -0.0266   1.0000   0.0226
 -11.250  -1.0946   0.02185   0.01564  -0.0235   1.0000   0.0232
 -11.000  -1.0841   0.02147   0.01519  -0.0205   1.0000   0.0238
 -10.750  -1.0726   0.02104   0.01468  -0.0177   1.0000   0.0242
 -10.500  -1.0641   0.02031   0.01392  -0.0146   1.0000   0.0250
 -10.250  -1.0524   0.01976   0.01334  -0.0119   1.0000   0.0256
 -10.000  -1.0384   0.01936   0.01291  -0.0095   1.0000   0.0263
  -9.750  -1.0247   0.01892   0.01242  -0.0071   1.0000   0.0270
  -9.500  -1.0103   0.01853   0.01199  -0.0047   1.0000   0.0278
  -9.250  -0.9961   0.01813   0.01153  -0.0023   1.0000   0.0284
  -9.000  -0.9811   0.01778   0.01113   0.0000   1.0000   0.0292
  -8.750  -0.9567   0.01735   0.01063   0.0003   0.9990   0.0298
  -8.500  -0.9277   0.01680   0.01002  -0.0004   0.9969   0.0306
  -8.250  -0.8992   0.01615   0.00935  -0.0011   0.9945   0.0319
  -8.000  -0.8711   0.01566   0.00883  -0.0016   0.9919   0.0328
  -7.750  -0.8425   0.01523   0.00837  -0.0021   0.9891   0.0338
  -7.500  -0.8127   0.01482   0.00792  -0.0029   0.9866   0.0348
  -7.250  -0.7817   0.01442   0.00748  -0.0038   0.9845   0.0357
  -7.000  -0.7544   0.01405   0.00706  -0.0040   0.9807   0.0365
  -6.750  -0.7253   0.01371   0.00669  -0.0044   0.9772   0.0372
  -6.500  -0.6953   0.01326   0.00621  -0.0052   0.9745   0.0390
  -6.250  -0.6657   0.01287   0.00581  -0.0058   0.9714   0.0408
  -6.000  -0.6392   0.01255   0.00547  -0.0056   0.9661   0.0425
  -5.750  -0.6086   0.01223   0.00513  -0.0064   0.9629   0.0447
  -5.500  -0.5764   0.01191   0.00479  -0.0074   0.9605   0.0481
  -5.250  -0.5514   0.01156   0.00448  -0.0069   0.9535   0.0543
  -5.000  -0.5213   0.01110   0.00423  -0.0077   0.9491   0.0867
  -4.750  -0.4858   0.01087   0.00402  -0.0095   0.9464   0.0979
  -4.500  -0.4566   0.01073   0.00386  -0.0098   0.9395   0.1026
  -4.250  -0.4238   0.01046   0.00361  -0.0110   0.9348   0.1089
  -4.000  -0.3887   0.01024   0.00339  -0.0126   0.9302   0.1132
  -3.750  -0.3569   0.01007   0.00320  -0.0135   0.9217   0.1158
  -3.500  -0.3216   0.00986   0.00297  -0.0151   0.9142   0.1197
  -3.250  -0.2905   0.00967   0.00278  -0.0158   0.9039   0.1244
  -3.000  -0.2599   0.00949   0.00260  -0.0164   0.8937   0.1307
  -2.750  -0.2312   0.00923   0.00242  -0.0167   0.8839   0.1492
  -2.500  -0.2090   0.00878   0.00224  -0.0157   0.8719   0.2217
  -2.250  -0.1846   0.00851   0.00212  -0.0150   0.8612   0.2650
  -2.000  -0.1598   0.00830   0.00201  -0.0144   0.8508   0.3005
  -1.750  -0.1355   0.00813   0.00191  -0.0136   0.8398   0.3288
  -1.500  -0.1118   0.00796   0.00182  -0.0127   0.8274   0.3593
  -1.250  -0.0891   0.00777   0.00173  -0.0116   0.8145   0.3987
  -1.000  -0.0672   0.00754   0.00165  -0.0103   0.8030   0.4475
  -0.750  -0.0472   0.00725   0.00158  -0.0086   0.7927   0.5115
  -0.500  -0.0279   0.00700   0.00153  -0.0067   0.7782   0.5729
  -0.250  -0.0069   0.00684   0.00150  -0.0052   0.7635   0.6170
   0.000   0.0145   0.00673   0.00148  -0.0036   0.7459   0.6535
   0.250   0.0360   0.00666   0.00147  -0.0020   0.7255   0.6876
   0.500   0.0581   0.00661   0.00147  -0.0006   0.7033   0.7180
   0.750   0.0799   0.00664   0.00148   0.0009   0.6734   0.7423
   1.000   0.1003   0.00675   0.00150   0.0027   0.6330   0.7634
   1.250   0.1208   0.00690   0.00154   0.0045   0.5894   0.7819
   1.500   0.1398   0.00713   0.00162   0.0065   0.5318   0.8013
   1.750   0.1572   0.00747   0.00173   0.0088   0.4553   0.8242
   2.000   0.1772   0.00778   0.00188   0.0105   0.3959   0.8484
   2.250   0.2004   0.00800   0.00202   0.0115   0.3605   0.8676
   2.500   0.2256   0.00823   0.00216   0.0121   0.3288   0.8836
   2.750   0.2541   0.00842   0.00231   0.0120   0.3066   0.8952
   3.000   0.2830   0.00860   0.00245   0.0118   0.2877   0.9039
   3.250   0.3115   0.00878   0.00258   0.0116   0.2687   0.9122
   3.500   0.3416   0.00902   0.00273   0.0111   0.2406   0.9186
   3.750   0.3714   0.00935   0.00291   0.0105   0.2002   0.9252
   4.000   0.3990   0.00970   0.00312   0.0104   0.1658   0.9321
   4.250   0.4335   0.01008   0.00339   0.0088   0.1408   0.9380
   4.500   0.4624   0.01038   0.00363   0.0085   0.1251   0.9467
   4.750   0.4964   0.01070   0.00389   0.0070   0.1084   0.9493
   5.000   0.5274   0.01106   0.00414   0.0061   0.0843   0.9527
   5.250   0.5527   0.01148   0.00442   0.0064   0.0637   0.9584
   5.500   0.5824   0.01180   0.00472   0.0059   0.0582   0.9616
   5.750   0.6135   0.01215   0.00507   0.0050   0.0538   0.9640
   6.000   0.6437   0.01243   0.00538   0.0044   0.0519   0.9671
   6.250   0.6686   0.01271   0.00570   0.0049   0.0501   0.9725
   6.500   0.7002   0.01305   0.00605   0.0039   0.0478   0.9744
   6.750   0.7305   0.01344   0.00645   0.0031   0.0458   0.9768
   7.000   0.7584   0.01392   0.00695   0.0028   0.0436   0.9801
   7.250   0.7848   0.01424   0.00731   0.0029   0.0423   0.9841
   7.500   0.8163   0.01454   0.00766   0.0019   0.0407   0.9858
   7.750   0.8467   0.01488   0.00803   0.0010   0.0391   0.9880
   8.000   0.8760   0.01525   0.00842   0.0004   0.0374   0.9906
   8.250   0.9031   0.01575   0.00892   0.0001   0.0355   0.9934
   8.500   0.9324   0.01615   0.00936  -0.0006   0.0343   0.9955
   8.750   0.9626   0.01649   0.00976  -0.0015   0.0329   0.9976
   9.000   0.9928   0.01685   0.01017  -0.0024   0.0314   0.9994
   9.250   1.0139   0.01720   0.01054  -0.0014   0.0300   1.0000
   9.500   1.0269   0.01763   0.01096   0.0012   0.0286   1.0000
   9.750   1.0417   0.01795   0.01135   0.0036   0.0277   1.0000
  10.000   1.0561   0.01831   0.01176   0.0060   0.0265   1.0000
  10.250   1.0707   0.01865   0.01215   0.0083   0.0251   1.0000
  10.500   1.0847   0.01903   0.01254   0.0107   0.0239   1.0000
  10.750   1.0975   0.01949   0.01303   0.0133   0.0227   1.0000
  11.000   1.1101   0.01994   0.01355   0.0158   0.0216   1.0000
  11.250   1.1211   0.02036   0.01401   0.0188   0.0203   1.0000
  11.500   1.1300   0.02080   0.01448   0.0220   0.0193   1.0000
  11.750   1.1380   0.02134   0.01505   0.0253   0.0185   1.0000
  12.000   1.1469   0.02190   0.01569   0.0282   0.0177   1.0000
  12.250   1.1561   0.02251   0.01638   0.0310   0.0170   1.0000
  12.500   1.1659   0.02316   0.01708   0.0335   0.0159   1.0000
  12.750   1.1748   0.02391   0.01788   0.0361   0.0153   1.0000
  13.000   1.1820   0.02481   0.01882   0.0386   0.0145   1.0000
  13.250   1.1898   0.02572   0.01983   0.0409   0.0141   1.0000
  13.500   1.1974   0.02669   0.02089   0.0430   0.0136   1.0000
  13.750   1.2039   0.02778   0.02209   0.0450   0.0131   1.0000
  14.000   1.2094   0.02902   0.02341   0.0469   0.0127   1.0000
  14.250   1.2139   0.03039   0.02488   0.0486   0.0124   1.0000
  14.500   1.2173   0.03193   0.02650   0.0501   0.0119   1.0000
  14.750   1.2182   0.03377   0.02843   0.0514   0.0116   1.0000
  15.000   1.2168   0.03594   0.03071   0.0525   0.0114   1.0000
  15.250   1.2139   0.03840   0.03329   0.0532   0.0112   1.0000
  15.500   1.2137   0.04078   0.03580   0.0535   0.0110   1.0000
  15.750   1.2093   0.04381   0.03897   0.0533   0.0109   1.0000
  16.000   1.2032   0.04728   0.04258   0.0525   0.0107   1.0000
  16.250   1.1952   0.05128   0.04673   0.0511   0.0106   1.0000
  16.500   1.1861   0.05577   0.05135   0.0492   0.0104   1.0000
  16.750   1.1718   0.06136   0.05710   0.0463   0.0104   1.0000
  17.000   1.1555   0.06765   0.06356   0.0429   0.0103   1.0000
  17.250   1.1356   0.07476   0.07083   0.0390   0.0102   1.0000
  17.500   1.1108   0.08276   0.07898   0.0347   0.0102   1.0000
  17.750   1.0858   0.09089   0.08725   0.0304   0.0102   1.0000
  18.000   1.0568   0.09983   0.09633   0.0257   0.0102   1.0000
  18.250   1.0233   0.10991   0.10656   0.0205   0.0104   1.0000
  18.500   0.9915   0.12004   0.11683   0.0152   0.0105   1.0000
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