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N-14 (n14-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: N-14 (n14-il)
Reynolds number: 1,000,000
Max Cl/Cd: 73.17 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n14-il-1000000-n5.txt
Download as CSV file: xf-n14-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.1134   0.11322   0.11047  -0.0194   1.0000   0.0082
 -19.250  -1.1672   0.09971   0.09676  -0.0266   1.0000   0.0079
 -19.000  -1.2174   0.08729   0.08416  -0.0332   1.0000   0.0078
 -18.750  -1.2587   0.07652   0.07319  -0.0391   1.0000   0.0077
 -18.500  -1.2912   0.06742   0.06391  -0.0442   1.0000   0.0078
 -18.250  -1.3125   0.06047   0.05679  -0.0481   1.0000   0.0077
 -18.000  -1.3299   0.05453   0.05071  -0.0511   1.0000   0.0077
 -17.750  -1.3418   0.04977   0.04581  -0.0531   1.0000   0.0078
 -17.500  -1.3514   0.04567   0.04160  -0.0545   1.0000   0.0080
 -17.250  -1.3574   0.04229   0.03811  -0.0552   1.0000   0.0081
 -17.000  -1.3612   0.03938   0.03508  -0.0554   1.0000   0.0081
 -16.750  -1.3620   0.03698   0.03257  -0.0552   1.0000   0.0084
 -16.500  -1.3627   0.03471   0.03021  -0.0546   1.0000   0.0086
 -16.250  -1.3609   0.03282   0.02821  -0.0537   1.0000   0.0088
 -16.000  -1.3579   0.03112   0.02642  -0.0526   1.0000   0.0089
 -15.750  -1.3534   0.02965   0.02486  -0.0513   1.0000   0.0092
 -15.500  -1.3501   0.02815   0.02328  -0.0497   1.0000   0.0095
 -15.250  -1.3450   0.02685   0.02192  -0.0480   1.0000   0.0099
 -15.000  -1.3386   0.02571   0.02071  -0.0462   1.0000   0.0102
 -14.750  -1.3312   0.02469   0.01963  -0.0443   1.0000   0.0105
 -14.500  -1.3227   0.02380   0.01867  -0.0423   1.0000   0.0110
 -14.250  -1.3137   0.02297   0.01777  -0.0401   1.0000   0.0114
 -14.000  -1.3041   0.02222   0.01695  -0.0379   1.0000   0.0118
 -13.750  -1.2943   0.02152   0.01620  -0.0356   1.0000   0.0124
 -13.500  -1.2841   0.02088   0.01553  -0.0332   1.0000   0.0130
 -13.250  -1.2737   0.02030   0.01491  -0.0307   1.0000   0.0136
 -13.000  -1.2630   0.01980   0.01438  -0.0281   1.0000   0.0144
 -12.750  -1.2530   0.01934   0.01386  -0.0252   1.0000   0.0149
 -12.500  -1.2438   0.01891   0.01338  -0.0220   1.0000   0.0154
 -12.250  -1.2348   0.01852   0.01297  -0.0187   1.0000   0.0162
 -12.000  -1.2240   0.01815   0.01258  -0.0157   1.0000   0.0169
 -11.750  -1.2103   0.01776   0.01217  -0.0133   1.0000   0.0176
 -11.500  -1.1960   0.01740   0.01177  -0.0110   1.0000   0.0183
 -11.250  -1.1810   0.01707   0.01140  -0.0087   1.0000   0.0189
 -11.000  -1.1657   0.01674   0.01102  -0.0065   1.0000   0.0193
 -10.750  -1.1515   0.01634   0.01060  -0.0041   1.0000   0.0202
 -10.500  -1.1266   0.01596   0.01021  -0.0039   0.9993   0.0209
 -10.250  -1.0979   0.01560   0.00984  -0.0045   0.9982   0.0218
 -10.000  -1.0692   0.01527   0.00948  -0.0051   0.9969   0.0226
  -9.750  -1.0403   0.01496   0.00913  -0.0057   0.9955   0.0233
  -9.500  -1.0109   0.01465   0.00879  -0.0064   0.9942   0.0238
  -9.250  -0.9835   0.01435   0.00846  -0.0066   0.9925   0.0242
  -9.000  -0.9573   0.01387   0.00794  -0.0067   0.9903   0.0251
  -8.750  -0.9292   0.01346   0.00753  -0.0071   0.9882   0.0260
  -8.500  -0.8999   0.01311   0.00715  -0.0077   0.9864   0.0267
  -8.250  -0.8697   0.01280   0.00684  -0.0085   0.9850   0.0276
  -8.000  -0.8403   0.01250   0.00653  -0.0090   0.9833   0.0283
  -7.750  -0.8151   0.01222   0.00622  -0.0087   0.9794   0.0290
  -7.500  -0.7859   0.01196   0.00593  -0.0091   0.9767   0.0296
  -7.250  -0.7556   0.01168   0.00563  -0.0098   0.9746   0.0300
  -7.000  -0.7249   0.01135   0.00528  -0.0106   0.9729   0.0306
  -6.750  -0.7016   0.01104   0.00494  -0.0098   0.9669   0.0316
  -6.500  -0.6722   0.01073   0.00463  -0.0102   0.9633   0.0326
  -6.000  -0.6105   0.01020   0.00410  -0.0118   0.9549   0.0350
  -5.750  -0.5758   0.00994   0.00383  -0.0135   0.9502   0.0363
  -5.500  -0.5386   0.00970   0.00358  -0.0156   0.9461   0.0375
  -5.250  -0.5065   0.00944   0.00332  -0.0167   0.9378   0.0410
  -5.000  -0.4707   0.00918   0.00307  -0.0186   0.9306   0.0452
  -4.750  -0.4379   0.00890   0.00280  -0.0198   0.9173   0.0556
  -4.500  -0.4091   0.00859   0.00262  -0.0201   0.9024   0.0881
  -4.250  -0.3814   0.00846   0.00249  -0.0201   0.8873   0.0960
  -4.000  -0.3549   0.00839   0.00237  -0.0198   0.8741   0.0997
  -3.750  -0.3287   0.00834   0.00227  -0.0194   0.8628   0.1013
  -3.500  -0.3031   0.00829   0.00217  -0.0188   0.8514   0.1028
  -3.250  -0.2782   0.00821   0.00206  -0.0182   0.8402   0.1054
  -3.000  -0.2530   0.00813   0.00196  -0.0176   0.8309   0.1079
  -2.500  -0.2028   0.00799   0.00179  -0.0163   0.8116   0.1133
  -2.250  -0.1778   0.00794   0.00171  -0.0156   0.8000   0.1156
  -2.000  -0.1530   0.00790   0.00164  -0.0148   0.7868   0.1184
  -1.750  -0.1291   0.00782   0.00155  -0.0139   0.7712   0.1267
  -1.500  -0.1057   0.00771   0.00146  -0.0129   0.7550   0.1424
  -1.250  -0.0854   0.00737   0.00135  -0.0114   0.7412   0.2131
  -1.000  -0.0620   0.00726   0.00129  -0.0104   0.7240   0.2401
  -0.750  -0.0396   0.00720   0.00123  -0.0092   0.6969   0.2662
  -0.500  -0.0178   0.00713   0.00119  -0.0079   0.6688   0.2976
  -0.250   0.0038   0.00710   0.00115  -0.0066   0.6374   0.3256
   0.000   0.0254   0.00707   0.00113  -0.0052   0.6071   0.3573
   0.250   0.0449   0.00705   0.00112  -0.0035   0.5643   0.4026
   0.500   0.0645   0.00704   0.00112  -0.0018   0.5193   0.4490
   0.750   0.0814   0.00714   0.00114   0.0004   0.4477   0.5032
   1.000   0.0991   0.00726   0.00119   0.0024   0.3830   0.5511
   1.250   0.1188   0.00730   0.00123   0.0041   0.3435   0.5956
   1.500   0.1398   0.00727   0.00127   0.0055   0.3217   0.6386
   1.750   0.1610   0.00725   0.00131   0.0070   0.3023   0.6798
   2.000   0.1828   0.00725   0.00137   0.0083   0.2845   0.7133
   2.250   0.2040   0.00723   0.00144   0.0099   0.2698   0.7540
   2.500   0.2259   0.00724   0.00152   0.0112   0.2540   0.7859
   2.750   0.2474   0.00734   0.00161   0.0126   0.2260   0.8124
   3.000   0.2685   0.00754   0.00173   0.0141   0.1880   0.8336
   3.250   0.2906   0.00774   0.00186   0.0153   0.1590   0.8510
   3.500   0.3143   0.00789   0.00199   0.0162   0.1404   0.8646
   3.750   0.3391   0.00803   0.00212   0.0169   0.1283   0.8760
   4.000   0.3643   0.00818   0.00226   0.0175   0.1166   0.8889
   4.250   0.3903   0.00833   0.00241   0.0178   0.1049   0.9016
   4.500   0.4172   0.00854   0.00257   0.0180   0.0876   0.9136
   4.750   0.4454   0.00888   0.00280   0.0178   0.0608   0.9230
   5.000   0.4753   0.00911   0.00302   0.0172   0.0541   0.9322
   5.250   0.5099   0.00931   0.00324   0.0157   0.0514   0.9396
   5.500   0.5454   0.00956   0.00349   0.0139   0.0487   0.9485
   5.750   0.5803   0.00983   0.00376   0.0122   0.0461   0.9535
   6.000   0.6085   0.01010   0.00403   0.0120   0.0433   0.9593
   6.250   0.6419   0.01031   0.00425   0.0107   0.0424   0.9616
   6.500   0.6746   0.01054   0.00450   0.0095   0.0412   0.9638
   6.750   0.7045   0.01078   0.00475   0.0089   0.0399   0.9669
   7.000   0.7283   0.01103   0.00499   0.0097   0.0382   0.9727
   7.250   0.7591   0.01135   0.00530   0.0088   0.0360   0.9741
   7.500   0.7894   0.01164   0.00561   0.0081   0.0347   0.9760
   7.750   0.8191   0.01189   0.00587   0.0075   0.0338   0.9782
   8.000   0.8469   0.01214   0.00614   0.0074   0.0326   0.9812
   8.250   0.8728   0.01241   0.00642   0.0076   0.0313   0.9843
   8.500   0.9031   0.01273   0.00673   0.0068   0.0298   0.9856
   8.750   0.9328   0.01307   0.00708   0.0061   0.0283   0.9872
   9.000   0.9621   0.01334   0.00738   0.0055   0.0273   0.9890
   9.250   0.9904   0.01364   0.00769   0.0051   0.0257   0.9910
   9.500   1.0174   0.01398   0.00803   0.0049   0.0242   0.9930
   9.750   1.0451   0.01434   0.00840   0.0046   0.0227   0.9946
  10.000   1.0741   0.01468   0.00877   0.0040   0.0213   0.9961
  10.250   1.1023   0.01507   0.00915   0.0035   0.0193   0.9975
  10.500   1.1303   0.01549   0.00959   0.0029   0.0178   0.9989
  10.750   1.1581   0.01594   0.01006   0.0024   0.0161   0.9999
  11.250   1.1866   0.01677   0.01092   0.0072   0.0140   1.0000
  11.500   1.1997   0.01718   0.01138   0.0098   0.0133   1.0000
  11.750   1.2119   0.01764   0.01187   0.0125   0.0126   1.0000
  12.000   1.2225   0.01812   0.01238   0.0155   0.0119   1.0000
  12.250   1.2293   0.01858   0.01288   0.0192   0.0114   1.0000
  12.500   1.2371   0.01903   0.01338   0.0227   0.0110   1.0000
  12.750   1.2463   0.01950   0.01391   0.0258   0.0107   1.0000
  13.000   1.2556   0.02005   0.01451   0.0287   0.0103   1.0000
  13.250   1.2654   0.02064   0.01516   0.0313   0.0100   1.0000
  13.500   1.2748   0.02131   0.01587   0.0339   0.0096   1.0000
  13.750   1.2838   0.02205   0.01667   0.0363   0.0093   1.0000
  14.000   1.2919   0.02290   0.01758   0.0387   0.0090   1.0000
  14.250   1.2991   0.02384   0.01859   0.0410   0.0086   1.0000
  14.500   1.3083   0.02471   0.01952   0.0430   0.0083   1.0000
  14.750   1.3162   0.02570   0.02060   0.0448   0.0082   1.0000
  15.000   1.3231   0.02682   0.02179   0.0466   0.0081   1.0000
  15.250   1.3291   0.02806   0.02312   0.0482   0.0080   1.0000
  15.500   1.3350   0.02937   0.02452   0.0496   0.0077   1.0000
  15.750   1.3386   0.03095   0.02618   0.0510   0.0075   1.0000
  16.000   1.3410   0.03271   0.02803   0.0521   0.0074   1.0000
  16.250   1.3427   0.03464   0.03005   0.0529   0.0073   1.0000
  16.500   1.3424   0.03688   0.03238   0.0535   0.0071   1.0000
  16.750   1.3406   0.03941   0.03501   0.0537   0.0070   1.0000
  17.000   1.3357   0.04249   0.03819   0.0534   0.0069   1.0000
  17.250   1.3283   0.04610   0.04192   0.0526   0.0067   1.0000
  17.500   1.3179   0.05038   0.04633   0.0511   0.0067   1.0000
  17.750   1.3038   0.05557   0.05165   0.0488   0.0065   1.0000
  18.000   1.2872   0.06150   0.05772   0.0457   0.0065   1.0000
  18.250   1.2659   0.06859   0.06498   0.0418   0.0065   1.0000
  18.500   1.2386   0.07686   0.07341   0.0373   0.0066   1.0000
  18.750   1.2023   0.08670   0.08343   0.0320   0.0066   1.0000
  19.000   1.1704   0.09581   0.09269   0.0273   0.0067   1.0000
  19.250   1.1197   0.10867   0.10574   0.0205   0.0067   1.0000
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