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N-13 (n13-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: N-13 (n13-il)
Reynolds number: 500,000
Max Cl/Cd: 60.75 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n13-il-500000-n5.txt
Download as CSV file: xf-n13-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: N-13                                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.9714   0.10566   0.10227  -0.0204   1.0000   0.0067
 -17.000  -0.9933   0.09750   0.09400  -0.0245   1.0000   0.0066
 -16.750  -1.0171   0.08912   0.08548  -0.0287   1.0000   0.0066
 -16.500  -1.0369   0.08155   0.07777  -0.0327   1.0000   0.0067
 -16.250  -1.0574   0.07429   0.07036  -0.0364   1.0000   0.0066
 -16.000  -1.0736   0.06794   0.06388  -0.0396   1.0000   0.0066
 -15.750  -1.0869   0.06228   0.05807  -0.0424   1.0000   0.0067
 -15.500  -1.0986   0.05718   0.05283  -0.0448   1.0000   0.0067
 -15.250  -1.1113   0.05225   0.04774  -0.0467   1.0000   0.0067
 -15.000  -1.1179   0.04843   0.04379  -0.0479   1.0000   0.0068
 -14.750  -1.1229   0.04501   0.04023  -0.0486   1.0000   0.0069
 -14.500  -1.1255   0.04209   0.03717  -0.0489   1.0000   0.0069
 -14.250  -1.1292   0.03925   0.03420  -0.0488   1.0000   0.0070
 -14.000  -1.1319   0.03672   0.03154  -0.0482   1.0000   0.0070
 -13.750  -1.1326   0.03457   0.02927  -0.0472   1.0000   0.0071
 -13.500  -1.1384   0.03220   0.02679  -0.0455   1.0000   0.0073
 -13.250  -1.1387   0.03046   0.02494  -0.0436   1.0000   0.0074
 -13.000  -1.1375   0.02894   0.02332  -0.0413   1.0000   0.0076
 -12.750  -1.1345   0.02765   0.02193  -0.0389   1.0000   0.0077
 -12.500  -1.1281   0.02665   0.02086  -0.0366   1.0000   0.0081
 -12.250  -1.1222   0.02569   0.01982  -0.0340   1.0000   0.0082
 -12.000  -1.1180   0.02469   0.01873  -0.0309   1.0000   0.0084
 -11.750  -1.1114   0.02390   0.01786  -0.0279   1.0000   0.0087
 -11.500  -1.1046   0.02319   0.01707  -0.0248   1.0000   0.0090
 -11.250  -1.0986   0.02253   0.01633  -0.0213   1.0000   0.0093
 -11.000  -1.0928   0.02192   0.01564  -0.0176   1.0000   0.0095
 -10.750  -1.0835   0.02135   0.01497  -0.0145   1.0000   0.0097
 -10.500  -1.0754   0.02054   0.01409  -0.0113   1.0000   0.0100
 -10.250  -1.0657   0.01979   0.01327  -0.0083   1.0000   0.0105
 -10.000  -1.0539   0.01915   0.01258  -0.0056   1.0000   0.0111
  -9.750  -1.0411   0.01859   0.01197  -0.0030   1.0000   0.0116
  -9.500  -1.0281   0.01807   0.01138  -0.0004   1.0000   0.0122
  -9.000  -0.9816   0.01696   0.01012   0.0004   0.9976   0.0141
  -8.750  -0.9528   0.01631   0.00945  -0.0004   0.9951   0.0161
  -8.500  -0.9252   0.01575   0.00886  -0.0008   0.9926   0.0187
  -8.250  -0.8983   0.01521   0.00837  -0.0011   0.9895   0.0239
  -8.000  -0.8695   0.01478   0.00800  -0.0017   0.9868   0.0321
  -7.750  -0.8396   0.01450   0.00768  -0.0025   0.9843   0.0370
  -7.500  -0.8151   0.01410   0.00727  -0.0021   0.9795   0.0401
  -7.000  -0.7612   0.01348   0.00658  -0.0022   0.9713   0.0452
  -6.750  -0.7344   0.01324   0.00629  -0.0022   0.9663   0.0470
  -6.500  -0.7074   0.01283   0.00585  -0.0023   0.9621   0.0506
  -6.250  -0.6831   0.01248   0.00549  -0.0017   0.9563   0.0534
  -6.000  -0.6552   0.01215   0.00514  -0.0019   0.9528   0.0569
  -5.750  -0.6262   0.01182   0.00480  -0.0023   0.9496   0.0628
  -5.500  -0.5996   0.01140   0.00452  -0.0024   0.9454   0.0790
  -5.250  -0.5689   0.01116   0.00430  -0.0031   0.9424   0.0943
  -5.000  -0.5363   0.01092   0.00406  -0.0042   0.9397   0.1020
  -4.750  -0.5015   0.01074   0.00383  -0.0058   0.9375   0.1058
  -4.500  -0.4688   0.01051   0.00361  -0.0070   0.9342   0.1106
  -4.250  -0.4344   0.01029   0.00339  -0.0086   0.9312   0.1153
  -4.000  -0.3983   0.01009   0.00318  -0.0106   0.9287   0.1203
  -3.750  -0.3618   0.00987   0.00298  -0.0126   0.9262   0.1269
  -3.500  -0.3242   0.00966   0.00279  -0.0149   0.9234   0.1334
  -3.250  -0.2909   0.00942   0.00261  -0.0163   0.9185   0.1482
  -3.000  -0.2555   0.00909   0.00242  -0.0182   0.9124   0.1855
  -2.750  -0.2228   0.00883   0.00226  -0.0194   0.9053   0.2173
  -2.500  -0.1944   0.00852   0.00210  -0.0197   0.8973   0.2614
  -2.250  -0.1713   0.00814   0.00198  -0.0189   0.8890   0.3322
  -2.000  -0.1458   0.00790   0.00189  -0.0185   0.8810   0.3800
  -1.750  -0.1234   0.00772   0.00183  -0.0174   0.8717   0.4118
  -1.500  -0.1005   0.00753   0.00176  -0.0163   0.8614   0.4471
  -1.250  -0.0789   0.00733   0.00170  -0.0149   0.8490   0.4858
  -1.000  -0.0593   0.00710   0.00164  -0.0131   0.8335   0.5331
  -0.750  -0.0390   0.00692   0.00160  -0.0113   0.8118   0.5743
  -0.500  -0.0168   0.00684   0.00151  -0.0099   0.7773   0.6010
  -0.250   0.0053   0.00686   0.00144  -0.0084   0.7438   0.6235
   0.000   0.0270   0.00693   0.00142  -0.0069   0.7165   0.6421
   0.250   0.0486   0.00699   0.00144  -0.0055   0.6911   0.6622
   0.500   0.0708   0.00703   0.00146  -0.0041   0.6712   0.6822
   0.750   0.0941   0.00704   0.00149  -0.0030   0.6550   0.6996
   1.000   0.1173   0.00704   0.00152  -0.0019   0.6387   0.7170
   1.250   0.1405   0.00704   0.00155  -0.0008   0.6220   0.7347
   1.500   0.1637   0.00705   0.00159   0.0003   0.6028   0.7509
   1.750   0.1858   0.00709   0.00163   0.0016   0.5766   0.7692
   2.000   0.2073   0.00715   0.00168   0.0031   0.5410   0.7910
   2.250   0.2257   0.00740   0.00177   0.0052   0.4751   0.8149
   2.500   0.2471   0.00772   0.00195   0.0066   0.4153   0.8432
   2.750   0.2761   0.00803   0.00218   0.0063   0.3721   0.8731
   3.000   0.3080   0.00831   0.00241   0.0054   0.3395   0.8946
   3.250   0.3368   0.00864   0.00263   0.0052   0.3035   0.9156
   3.500   0.3667   0.00900   0.00287   0.0048   0.2691   0.9318
   3.750   0.3988   0.00939   0.00313   0.0037   0.2320   0.9398
   4.000   0.4245   0.00972   0.00334   0.0041   0.2030   0.9476
   4.250   0.4580   0.01008   0.00359   0.0027   0.1753   0.9508
   4.500   0.4876   0.01041   0.00383   0.0022   0.1520   0.9547
   4.750   0.5102   0.01069   0.00404   0.0032   0.1331   0.9606
   5.000   0.5435   0.01104   0.00430   0.0018   0.1124   0.9623
   5.250   0.5750   0.01140   0.00459   0.0008   0.0953   0.9644
   5.500   0.6051   0.01171   0.00487   0.0002   0.0843   0.9672
   5.750   0.6313   0.01201   0.00514   0.0004   0.0767   0.9711
   6.000   0.6590   0.01232   0.00545   0.0002   0.0698   0.9740
   6.250   0.6908   0.01263   0.00577  -0.0008   0.0644   0.9757
   6.500   0.7212   0.01295   0.00608  -0.0016   0.0592   0.9777
   6.750   0.7492   0.01332   0.00643  -0.0019   0.0538   0.9804
   7.000   0.7752   0.01358   0.00674  -0.0017   0.0506   0.9836
   7.250   0.8046   0.01391   0.00707  -0.0023   0.0469   0.9853
   7.500   0.8342   0.01431   0.00746  -0.0030   0.0429   0.9870
   7.750   0.8638   0.01460   0.00781  -0.0037   0.0403   0.9889
   8.000   0.8916   0.01495   0.00816  -0.0040   0.0372   0.9910
   8.250   0.9181   0.01536   0.00859  -0.0041   0.0340   0.9932
   8.500   0.9473   0.01571   0.00900  -0.0048   0.0312   0.9951
   8.750   0.9774   0.01617   0.00944  -0.0057   0.0274   0.9972
   9.000   1.0079   0.01659   0.00990  -0.0067   0.0237   0.9992
   9.250   1.0299   0.01708   0.01039  -0.0060   0.0205   1.0000
   9.500   1.0435   0.01750   0.01085  -0.0034   0.0184   1.0000
   9.750   1.0558   0.01798   0.01136  -0.0007   0.0167   1.0000
  10.000   1.0672   0.01849   0.01191   0.0023   0.0153   1.0000
  10.250   1.0786   0.01896   0.01244   0.0052   0.0142   1.0000
  10.500   1.0887   0.01947   0.01302   0.0083   0.0135   1.0000
  10.750   1.0971   0.02007   0.01365   0.0116   0.0126   1.0000
  11.000   1.1029   0.02069   0.01432   0.0155   0.0117   1.0000
  11.250   1.1067   0.02123   0.01493   0.0197   0.0114   1.0000
  11.500   1.1122   0.02176   0.01556   0.0234   0.0110   1.0000
  11.750   1.1185   0.02236   0.01624   0.0269   0.0106   1.0000
  12.000   1.1248   0.02306   0.01702   0.0302   0.0102   1.0000
  12.250   1.1314   0.02382   0.01786   0.0333   0.0097   1.0000
  12.500   1.1374   0.02469   0.01881   0.0362   0.0095   1.0000
  12.750   1.1431   0.02563   0.01984   0.0389   0.0093   1.0000
  13.000   1.1461   0.02681   0.02111   0.0417   0.0089   1.0000
  13.250   1.1496   0.02803   0.02242   0.0441   0.0087   1.0000
  13.500   1.1490   0.02961   0.02411   0.0466   0.0084   1.0000
  13.750   1.1529   0.03098   0.02560   0.0484   0.0082   1.0000
  14.000   1.1551   0.03257   0.02731   0.0501   0.0081   1.0000
  14.250   1.1552   0.03445   0.02932   0.0515   0.0079   1.0000
  14.500   1.1545   0.03655   0.03155   0.0525   0.0079   1.0000
  14.750   1.1530   0.03894   0.03406   0.0530   0.0076   1.0000
  15.000   1.1524   0.04142   0.03666   0.0531   0.0075   1.0000
  15.250   1.1446   0.04492   0.04031   0.0526   0.0074   1.0000
  15.500   1.1388   0.04844   0.04395   0.0517   0.0072   1.0000
  15.750   1.1282   0.05285   0.04851   0.0500   0.0072   1.0000
  16.000   1.1189   0.05748   0.05327   0.0479   0.0071   1.0000
  16.250   1.0999   0.06395   0.05992   0.0445   0.0071   1.0000
  16.500   1.0778   0.07139   0.06753   0.0403   0.0072   1.0000
  16.750   1.0570   0.07878   0.07506   0.0363   0.0072   1.0000
  17.000   1.0265   0.08802   0.08448   0.0314   0.0073   1.0000
  17.250   0.9989   0.09695   0.09354   0.0268   0.0073   1.0000
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