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N-14 (n14-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: N-14 (n14-il)
Reynolds number: 1,000,000
Max Cl/Cd: 71.76 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n14-il-1000000.txt
Download as CSV file: xf-n14-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -1.1012   0.10667   0.10393  -0.0231   1.0000   0.0126
 -18.750  -1.1331   0.09722   0.09435  -0.0282   1.0000   0.0127
 -18.500  -1.1672   0.08767   0.08467  -0.0333   1.0000   0.0127
 -18.250  -1.1905   0.07997   0.07683  -0.0374   1.0000   0.0127
 -18.000  -1.2184   0.07169   0.06840  -0.0419   1.0000   0.0127
 -17.750  -1.2405   0.06442   0.06099  -0.0459   1.0000   0.0128
 -17.500  -1.2589   0.05805   0.05449  -0.0493   1.0000   0.0129
 -17.250  -1.2741   0.05251   0.04883  -0.0521   1.0000   0.0132
 -17.000  -1.2864   0.04782   0.04400  -0.0539   1.0000   0.0132
 -16.750  -1.2913   0.04436   0.04044  -0.0549   1.0000   0.0134
 -16.500  -1.2937   0.04141   0.03739  -0.0555   1.0000   0.0135
 -16.250  -1.2860   0.03970   0.03564  -0.0556   1.0000   0.0139
 -16.000  -1.2920   0.03674   0.03256  -0.0553   1.0000   0.0140
 -15.750  -1.2857   0.03512   0.03087  -0.0549   1.0000   0.0143
 -15.500  -1.2769   0.03380   0.02949  -0.0543   1.0000   0.0147
 -15.250  -1.2781   0.03171   0.02728  -0.0530   1.0000   0.0149
 -15.000  -1.2685   0.03060   0.02610  -0.0521   1.0000   0.0152
 -14.750  -1.2632   0.02922   0.02461  -0.0506   1.0000   0.0154
 -14.500  -1.2581   0.02790   0.02320  -0.0490   1.0000   0.0158
 -14.250  -1.2579   0.02635   0.02157  -0.0466   1.0000   0.0163
 -14.000  -1.2501   0.02539   0.02056  -0.0447   1.0000   0.0166
 -13.750  -1.2400   0.02461   0.01975  -0.0429   1.0000   0.0170
 -13.500  -1.2274   0.02404   0.01914  -0.0411   1.0000   0.0174
 -13.250  -1.2161   0.02342   0.01846  -0.0391   1.0000   0.0178
 -13.000  -1.2045   0.02284   0.01783  -0.0370   1.0000   0.0183
 -12.750  -1.1948   0.02221   0.01712  -0.0345   1.0000   0.0186
 -12.500  -1.1806   0.02188   0.01673  -0.0325   1.0000   0.0190
 -12.250  -1.1693   0.02144   0.01623  -0.0299   1.0000   0.0193
 -12.000  -1.1725   0.02037   0.01510  -0.0250   1.0000   0.0200
 -11.750  -1.1668   0.01989   0.01459  -0.0212   1.0000   0.0205
 -11.500  -1.1568   0.01958   0.01426  -0.0180   1.0000   0.0209
 -11.250  -1.1435   0.01923   0.01389  -0.0155   1.0000   0.0214
 -11.000  -1.1304   0.01882   0.01343  -0.0129   1.0000   0.0220
 -10.750  -1.1158   0.01850   0.01306  -0.0106   1.0000   0.0226
 -10.500  -1.1016   0.01813   0.01264  -0.0082   1.0000   0.0230
 -10.250  -1.0847   0.01793   0.01241  -0.0062   1.0000   0.0234
 -10.000  -1.0751   0.01724   0.01165  -0.0030   1.0000   0.0239
  -9.750  -1.0661   0.01654   0.01091   0.0003   1.0000   0.0248
  -9.500  -1.0519   0.01617   0.01054   0.0028   1.0000   0.0255
  -9.250  -1.0373   0.01585   0.01019   0.0052   1.0000   0.0260
  -9.000  -1.0163   0.01550   0.00982   0.0062   0.9996   0.0267
  -8.750  -0.9837   0.01520   0.00949   0.0049   0.9982   0.0277
  -8.500  -0.9516   0.01487   0.00912   0.0037   0.9966   0.0283
  -8.250  -0.9194   0.01451   0.00872   0.0024   0.9951   0.0289
  -8.000  -0.8908   0.01366   0.00783   0.0017   0.9935   0.0303
  -7.750  -0.8616   0.01324   0.00740   0.0011   0.9910   0.0314
  -7.500  -0.8305   0.01287   0.00701   0.0001   0.9887   0.0324
  -7.250  -0.7984   0.01252   0.00664  -0.0010   0.9867   0.0334
  -7.000  -0.7651   0.01222   0.00631  -0.0024   0.9851   0.0343
  -6.750  -0.7310   0.01192   0.00600  -0.0039   0.9839   0.0350
  -6.500  -0.7015   0.01138   0.00542  -0.0045   0.9814   0.0368
  -6.250  -0.6733   0.01101   0.00504  -0.0047   0.9773   0.0385
  -6.000  -0.6406   0.01069   0.00471  -0.0059   0.9748   0.0404
  -5.750  -0.6064   0.01040   0.00441  -0.0074   0.9730   0.0419
  -5.500  -0.5723   0.01002   0.00403  -0.0088   0.9714   0.0455
  -5.250  -0.5420   0.00967   0.00371  -0.0095   0.9683   0.0507
  -5.000  -0.5161   0.00913   0.00343  -0.0093   0.9629   0.0912
  -4.750  -0.4814   0.00891   0.00326  -0.0108   0.9601   0.1028
  -4.500  -0.4441   0.00876   0.00310  -0.0129   0.9578   0.1079
  -4.250  -0.4130   0.00857   0.00290  -0.0136   0.9510   0.1121
  -4.000  -0.3790   0.00834   0.00270  -0.0150   0.9451   0.1168
  -3.750  -0.3448   0.00816   0.00251  -0.0164   0.9384   0.1204
  -3.500  -0.3117   0.00801   0.00234  -0.0176   0.9296   0.1234
  -3.250  -0.2815   0.00783   0.00218  -0.0181   0.9204   0.1302
  -3.000  -0.2507   0.00768   0.00203  -0.0187   0.9105   0.1364
  -2.750  -0.2256   0.00743   0.00187  -0.0182   0.8984   0.1624
  -2.500  -0.2042   0.00702   0.00172  -0.0169   0.8864   0.2346
  -2.250  -0.1811   0.00675   0.00161  -0.0159   0.8755   0.2863
  -2.000  -0.1588   0.00648   0.00149  -0.0148   0.8641   0.3389
  -1.750  -0.1376   0.00621   0.00140  -0.0134   0.8529   0.3934
  -1.500  -0.1182   0.00584   0.00130  -0.0116   0.8434   0.4723
  -1.250  -0.0986   0.00554   0.00123  -0.0099   0.8341   0.5457
  -1.000  -0.0779   0.00532   0.00118  -0.0082   0.8239   0.5991
  -0.750  -0.0570   0.00516   0.00114  -0.0066   0.8127   0.6464
  -0.500  -0.0355   0.00503   0.00113  -0.0051   0.8018   0.6884
  -0.250  -0.0127   0.00494   0.00112  -0.0038   0.7910   0.7201
   0.000   0.0104   0.00489   0.00112  -0.0026   0.7789   0.7455
   0.250   0.0343   0.00488   0.00113  -0.0015   0.7662   0.7672
   0.500   0.0582   0.00486   0.00113  -0.0004   0.7514   0.7846
   0.750   0.0818   0.00486   0.00114   0.0007   0.7318   0.8015
   1.000   0.1042   0.00492   0.00114   0.0021   0.7006   0.8151
   1.250   0.1250   0.00505   0.00115   0.0038   0.6559   0.8271
   1.500   0.1460   0.00522   0.00119   0.0054   0.6108   0.8390
   1.750   0.1664   0.00544   0.00125   0.0071   0.5561   0.8501
   2.000   0.1860   0.00573   0.00133   0.0089   0.4913   0.8621
   2.250   0.2066   0.00603   0.00144   0.0105   0.4279   0.8749
   2.500   0.2288   0.00628   0.00157   0.0118   0.3808   0.8903
   2.750   0.2535   0.00648   0.00169   0.0125   0.3488   0.9051
   3.000   0.2810   0.00665   0.00183   0.0126   0.3265   0.9177
   3.250   0.3084   0.00683   0.00195   0.0128   0.3065   0.9285
   3.500   0.3391   0.00702   0.00210   0.0121   0.2864   0.9370
   3.750   0.3694   0.00726   0.00225   0.0116   0.2596   0.9445
   4.000   0.4007   0.00757   0.00242   0.0107   0.2222   0.9496
   4.250   0.4250   0.00794   0.00260   0.0113   0.1787   0.9568
   4.500   0.4592   0.00834   0.00286   0.0098   0.1470   0.9592
   4.750   0.4944   0.00872   0.00312   0.0080   0.1239   0.9622
   5.000   0.5256   0.00907   0.00338   0.0071   0.1004   0.9658
   5.250   0.5507   0.00958   0.00368   0.0075   0.0656   0.9709
   5.500   0.5848   0.00992   0.00398   0.0061   0.0577   0.9720
   5.750   0.6179   0.01030   0.00432   0.0048   0.0527   0.9735
   6.000   0.6509   0.01060   0.00464   0.0035   0.0499   0.9752
   6.250   0.6830   0.01086   0.00492   0.0025   0.0480   0.9775
   6.500   0.7115   0.01116   0.00523   0.0022   0.0458   0.9810
   6.750   0.7402   0.01159   0.00566   0.0018   0.0429   0.9836
   7.000   0.7737   0.01191   0.00599   0.0004   0.0413   0.9848
   7.250   0.8071   0.01214   0.00624  -0.0010   0.0398   0.9861
   7.500   0.8395   0.01242   0.00653  -0.0022   0.0382   0.9878
   7.750   0.8705   0.01277   0.00688  -0.0031   0.0363   0.9899
   8.000   0.8989   0.01330   0.00744  -0.0036   0.0345   0.9924
   8.250   0.9299   0.01350   0.00766  -0.0044   0.0333   0.9941
   8.500   0.9629   0.01374   0.00791  -0.0058   0.0319   0.9953
   8.750   0.9951   0.01404   0.00819  -0.0071   0.0301   0.9968
   9.000   1.0249   0.01462   0.00880  -0.0080   0.0284   0.9985
   9.250   1.0575   0.01479   0.00900  -0.0092   0.0272   0.9997
   9.500   1.0779   0.01502   0.00924  -0.0080   0.0260   1.0000
   9.750   1.0926   0.01530   0.00952  -0.0056   0.0250   1.0000
  10.000   1.1020   0.01590   0.01014  -0.0023   0.0236   1.0000
  10.250   1.1181   0.01612   0.01041  -0.0001   0.0230   1.0000
  10.500   1.1333   0.01640   0.01072   0.0022   0.0221   1.0000
  10.750   1.1488   0.01667   0.01101   0.0045   0.0211   1.0000
  11.000   1.1625   0.01705   0.01139   0.0070   0.0203   1.0000
  11.250   1.1707   0.01772   0.01210   0.0104   0.0192   1.0000
  11.500   1.1847   0.01806   0.01250   0.0128   0.0187   1.0000
  11.750   1.1968   0.01846   0.01293   0.0156   0.0181   1.0000
  12.000   1.2045   0.01886   0.01338   0.0192   0.0176   1.0000
  12.250   1.2127   0.01928   0.01383   0.0226   0.0170   1.0000
  12.500   1.2200   0.01982   0.01440   0.0260   0.0164   1.0000
  12.750   1.2223   0.02069   0.01533   0.0299   0.0158   1.0000
  13.000   1.2307   0.02137   0.01609   0.0328   0.0155   1.0000
  13.250   1.2419   0.02196   0.01674   0.0350   0.0151   1.0000
  13.500   1.2519   0.02265   0.01751   0.0373   0.0147   1.0000
  13.750   1.2609   0.02345   0.01837   0.0396   0.0144   1.0000
  14.000   1.2713   0.02421   0.01918   0.0415   0.0139   1.0000
  14.250   1.2800   0.02512   0.02014   0.0434   0.0135   1.0000
  14.500   1.2836   0.02642   0.02151   0.0456   0.0132   1.0000
  14.750   1.2822   0.02815   0.02333   0.0478   0.0128   1.0000
  15.000   1.2794   0.03013   0.02542   0.0498   0.0126   1.0000
  15.250   1.2890   0.03127   0.02665   0.0508   0.0123   1.0000
  15.500   1.2901   0.03318   0.02867   0.0519   0.0122   1.0000
  15.750   1.2922   0.03510   0.03069   0.0527   0.0120   1.0000
  16.000   1.2936   0.03723   0.03292   0.0532   0.0118   1.0000
  16.250   1.2921   0.03979   0.03559   0.0534   0.0116   1.0000
  16.500   1.2873   0.04290   0.03881   0.0530   0.0115   1.0000
  16.750   1.2858   0.04588   0.04189   0.0523   0.0113   1.0000
  17.000   1.2770   0.04997   0.04611   0.0509   0.0112   1.0000
  17.250   1.2672   0.05453   0.05079   0.0490   0.0112   1.0000
  17.500   1.2528   0.06009   0.05649   0.0462   0.0111   1.0000
  17.750   1.2375   0.06614   0.06266   0.0430   0.0109   1.0000
  18.000   1.2174   0.07314   0.06981   0.0392   0.0110   1.0000
  18.250   1.1981   0.08006   0.07685   0.0355   0.0109   1.0000
  18.500   1.1703   0.08842   0.08535   0.0311   0.0109   1.0000
  18.750   1.1398   0.09729   0.09436   0.0265   0.0109   1.0000
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