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NACA 16-015 (naca16015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 16-015 (naca16015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 50.55 at α=10.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca16015-il-1000000-n5.txt
Download as CSV file: xf-naca16015-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 16-015                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1066   0.08681   0.08379  -0.0692   1.0000   0.0049
 -19.500  -1.1393   0.07796   0.07475  -0.0732   1.0000   0.0048
 -19.250  -1.1638   0.07116   0.06779  -0.0757   1.0000   0.0048
 -19.000  -1.1830   0.06571   0.06220  -0.0770   1.0000   0.0049
 -18.750  -1.1993   0.06111   0.05747  -0.0774   1.0000   0.0049
 -18.500  -1.2129   0.05719   0.05342  -0.0772   1.0000   0.0049
 -18.250  -1.2247   0.05381   0.04993  -0.0764   1.0000   0.0050
 -18.000  -1.2352   0.05083   0.04684  -0.0750   1.0000   0.0050
 -17.750  -1.2366   0.04789   0.04378  -0.0752   0.9996   0.0051
 -17.500  -1.2357   0.04523   0.04099  -0.0752   0.9990   0.0052
 -17.250  -1.2330   0.04282   0.03847  -0.0750   0.9984   0.0052
 -17.000  -1.2285   0.04068   0.03621  -0.0748   0.9977   0.0053
 -16.750  -1.2231   0.03871   0.03414  -0.0743   0.9971   0.0054
 -16.500  -1.2158   0.03696   0.03229  -0.0738   0.9964   0.0054
 -16.250  -1.2096   0.03517   0.03038  -0.0731   0.9958   0.0056
 -16.000  -1.2024   0.03347   0.02858  -0.0724   0.9953   0.0058
 -15.750  -1.1924   0.03200   0.02703  -0.0718   0.9948   0.0060
 -15.500  -1.1803   0.03069   0.02564  -0.0713   0.9943   0.0061
 -15.250  -1.1693   0.02953   0.02441  -0.0702   0.9932   0.0064
 -15.000  -1.1572   0.02845   0.02325  -0.0692   0.9920   0.0065
 -14.750  -1.1437   0.02745   0.02217  -0.0684   0.9910   0.0068
 -14.500  -1.1286   0.02649   0.02114  -0.0678   0.9899   0.0070
 -14.250  -1.1124   0.02557   0.02014  -0.0672   0.9890   0.0072
 -14.000  -1.0949   0.02472   0.01920  -0.0668   0.9882   0.0074
 -13.750  -1.0767   0.02392   0.01834  -0.0665   0.9875   0.0075
 -13.500  -1.0592   0.02303   0.01738  -0.0660   0.9869   0.0079
 -13.250  -1.0400   0.02223   0.01654  -0.0658   0.9863   0.0083
 -13.000  -1.0198   0.02150   0.01576  -0.0657   0.9857   0.0088
 -12.750  -0.9988   0.02083   0.01503  -0.0656   0.9851   0.0092
 -12.500  -0.9817   0.02025   0.01439  -0.0645   0.9832   0.0097
 -12.250  -0.9635   0.01970   0.01379  -0.0636   0.9813   0.0101
 -12.000  -0.9443   0.01911   0.01316  -0.0629   0.9796   0.0107
 -11.750  -0.9236   0.01854   0.01257  -0.0625   0.9782   0.0117
 -11.500  -0.9021   0.01801   0.01202  -0.0622   0.9769   0.0125
 -11.250  -0.8803   0.01752   0.01149  -0.0619   0.9758   0.0133
 -11.000  -0.8584   0.01704   0.01097  -0.0616   0.9747   0.0143
 -10.750  -0.8391   0.01663   0.01055  -0.0607   0.9726   0.0156
 -10.500  -0.8197   0.01625   0.01016  -0.0597   0.9700   0.0168
 -10.250  -0.7987   0.01589   0.00977  -0.0590   0.9678   0.0179
 -10.000  -0.7775   0.01550   0.00937  -0.0583   0.9659   0.0193
  -9.750  -0.7555   0.01514   0.00901  -0.0578   0.9643   0.0208
  -9.500  -0.7325   0.01481   0.00865  -0.0575   0.9627   0.0221
  -9.250  -0.7118   0.01453   0.00834  -0.0566   0.9603   0.0230
  -9.000  -0.6906   0.01428   0.00806  -0.0558   0.9576   0.0237
  -8.750  -0.6699   0.01395   0.00770  -0.0549   0.9553   0.0248
  -8.500  -0.6488   0.01360   0.00734  -0.0540   0.9530   0.0262
  -8.250  -0.6266   0.01329   0.00700  -0.0534   0.9510   0.0274
  -8.000  -0.6035   0.01300   0.00670  -0.0530   0.9492   0.0285
  -7.750  -0.5821   0.01277   0.00645  -0.0521   0.9467   0.0296
  -7.500  -0.5602   0.01255   0.00621  -0.0513   0.9440   0.0304
  -7.250  -0.5377   0.01233   0.00595  -0.0507   0.9414   0.0310
  -7.000  -0.5160   0.01202   0.00563  -0.0498   0.9390   0.0328
  -6.750  -0.4932   0.01175   0.00535  -0.0492   0.9369   0.0347
  -6.500  -0.4698   0.01150   0.00509  -0.0487   0.9350   0.0367
  -6.250  -0.4477   0.01130   0.00489  -0.0479   0.9323   0.0384
  -6.000  -0.4253   0.01110   0.00468  -0.0472   0.9295   0.0410
  -5.750  -0.4031   0.01086   0.00447  -0.0464   0.9269   0.0462
  -5.500  -0.3805   0.01062   0.00426  -0.0456   0.9244   0.0546
  -5.250  -0.3580   0.01034   0.00403  -0.0449   0.9221   0.0689
  -5.000  -0.3353   0.01007   0.00382  -0.0443   0.9198   0.0859
  -4.750  -0.3144   0.00983   0.00366  -0.0432   0.9170   0.1036
  -4.500  -0.2934   0.00958   0.00349  -0.0421   0.9140   0.1256
  -4.250  -0.2725   0.00930   0.00331  -0.0410   0.9111   0.1525
  -4.000  -0.2514   0.00900   0.00312  -0.0400   0.9085   0.1853
  -3.750  -0.2308   0.00865   0.00291  -0.0388   0.9060   0.2277
  -3.500  -0.2141   0.00828   0.00275  -0.0369   0.9028   0.2812
  -3.250  -0.2007   0.00781   0.00255  -0.0342   0.8989   0.3521
  -3.000  -0.1887   0.00730   0.00234  -0.0311   0.8953   0.4296
  -2.750  -0.1770   0.00680   0.00210  -0.0279   0.8920   0.5040
  -2.500  -0.1720   0.00636   0.00193  -0.0231   0.8877   0.5753
  -2.250  -0.1748   0.00599   0.00181  -0.0163   0.8824   0.6419
  -2.000  -0.1722   0.00565   0.00169  -0.0106   0.8782   0.7051
  -1.750  -0.1627   0.00544   0.00166  -0.0065   0.8746   0.7544
  -1.500  -0.1489   0.00533   0.00170  -0.0033   0.8706   0.7915
  -1.250  -0.1291   0.00529   0.00173  -0.0015   0.8673   0.8160
  -1.000  -0.1049   0.00528   0.00174  -0.0007   0.8646   0.8313
  -0.750  -0.0757   0.00528   0.00175  -0.0012   0.8623   0.8389
  -0.500  -0.0536   0.00529   0.00177  -0.0001   0.8589   0.8451
  -0.250  -0.0288   0.00529   0.00177   0.0004   0.8554   0.8494
   0.000   0.0000   0.00529   0.00178   0.0000   0.8523   0.8523
   0.250   0.0288   0.00529   0.00177  -0.0004   0.8494   0.8554
   0.500   0.0536   0.00529   0.00177   0.0001   0.8451   0.8589
   0.750   0.0757   0.00528   0.00175   0.0012   0.8389   0.8623
   1.000   0.1049   0.00528   0.00174   0.0007   0.8313   0.8645
   1.250   0.1291   0.00529   0.00173   0.0015   0.8161   0.8673
   1.500   0.1488   0.00533   0.00170   0.0033   0.7913   0.8706
   1.750   0.1631   0.00543   0.00166   0.0064   0.7558   0.8746
   2.000   0.1717   0.00565   0.00169   0.0107   0.7036   0.8783
   2.250   0.1758   0.00598   0.00180   0.0161   0.6436   0.8823
   2.500   0.1716   0.00637   0.00193   0.0232   0.5736   0.8877
   2.750   0.1775   0.00679   0.00209   0.0278   0.5054   0.8919
   3.000   0.1889   0.00730   0.00234   0.0311   0.4296   0.8953
   3.250   0.2011   0.00780   0.00255   0.0341   0.3532   0.8989
   3.500   0.2142   0.00828   0.00275   0.0368   0.2807   0.9028
   3.750   0.2310   0.00865   0.00291   0.0388   0.2274   0.9060
   4.000   0.2515   0.00900   0.00312   0.0399   0.1847   0.9085
   4.250   0.2727   0.00930   0.00331   0.0410   0.1523   0.9110
   4.500   0.2938   0.00957   0.00348   0.0420   0.1263   0.9140
   4.750   0.3146   0.00984   0.00366   0.0431   0.1032   0.9170
   5.000   0.3356   0.01007   0.00382   0.0442   0.0858   0.9198
   5.250   0.3583   0.01034   0.00403   0.0449   0.0687   0.9221
   5.500   0.3809   0.01062   0.00425   0.0456   0.0545   0.9244
   5.750   0.4035   0.01086   0.00447   0.0463   0.0462   0.9269
   6.000   0.4257   0.01110   0.00468   0.0471   0.0410   0.9295
   6.250   0.4482   0.01130   0.00488   0.0478   0.0384   0.9323
   6.500   0.4703   0.01150   0.00509   0.0486   0.0367   0.9349
   6.750   0.4938   0.01175   0.00535   0.0491   0.0348   0.9369
   7.000   0.5166   0.01202   0.00563   0.0497   0.0328   0.9389
   7.250   0.5383   0.01233   0.00595   0.0505   0.0309   0.9414
   7.500   0.5609   0.01255   0.00620   0.0512   0.0303   0.9440
   7.750   0.5828   0.01277   0.00645   0.0520   0.0296   0.9467
   8.000   0.6042   0.01300   0.00670   0.0528   0.0286   0.9492
   8.250   0.6273   0.01328   0.00700   0.0533   0.0273   0.9510
   8.500   0.6496   0.01360   0.00734   0.0539   0.0262   0.9530
   8.750   0.6706   0.01395   0.00770   0.0547   0.0248   0.9552
   9.000   0.6915   0.01428   0.00805   0.0556   0.0237   0.9576
   9.250   0.7127   0.01453   0.00834   0.0564   0.0230   0.9602
   9.500   0.7334   0.01481   0.00864   0.0573   0.0220   0.9627
   9.750   0.7564   0.01514   0.00900   0.0576   0.0207   0.9642
  10.000   0.7784   0.01549   0.00936   0.0581   0.0193   0.9659
  10.250   0.7997   0.01588   0.00976   0.0588   0.0179   0.9677
  10.500   0.8207   0.01625   0.01016   0.0595   0.0168   0.9700
  10.750   0.8401   0.01662   0.01054   0.0605   0.0155   0.9726
  11.000   0.8594   0.01704   0.01096   0.0614   0.0142   0.9747
  11.250   0.8814   0.01752   0.01148   0.0617   0.0133   0.9758
  11.500   0.9033   0.01801   0.01201   0.0620   0.0125   0.9770
  11.750   0.9248   0.01853   0.01256   0.0623   0.0116   0.9783
  12.000   0.9455   0.01910   0.01315   0.0627   0.0107   0.9797
  12.250   0.9648   0.01969   0.01378   0.0634   0.0101   0.9813
  12.500   0.9828   0.02024   0.01438   0.0643   0.0096   0.9833
  12.750   1.0003   0.02082   0.01502   0.0653   0.0092   0.9851
  13.000   1.0213   0.02149   0.01575   0.0654   0.0088   0.9857
  13.250   1.0416   0.02222   0.01652   0.0655   0.0084   0.9863
  13.500   1.0608   0.02303   0.01738   0.0657   0.0079   0.9869
  13.750   1.0785   0.02391   0.01832   0.0661   0.0075   0.9876
  14.000   1.0967   0.02471   0.01919   0.0665   0.0074   0.9883
  14.250   1.1142   0.02555   0.02012   0.0669   0.0072   0.9891
  14.500   1.1305   0.02647   0.02112   0.0674   0.0070   0.9901
  14.750   1.1457   0.02742   0.02215   0.0680   0.0067   0.9911
  15.000   1.1591   0.02843   0.02324   0.0689   0.0066   0.9922
  15.250   1.1714   0.02950   0.02437   0.0699   0.0063   0.9934
  15.500   1.1828   0.03068   0.02562   0.0708   0.0062   0.9944
  15.750   1.1951   0.03198   0.02700   0.0713   0.0059   0.9949
  16.000   1.2051   0.03345   0.02855   0.0719   0.0057   0.9954
  16.250   1.2120   0.03516   0.03037   0.0727   0.0055   0.9959
  16.500   1.2187   0.03692   0.03224   0.0733   0.0054   0.9966
  16.750   1.2260   0.03867   0.03409   0.0738   0.0054   0.9972
  17.000   1.2316   0.04061   0.03614   0.0743   0.0053   0.9979
  17.250   1.2360   0.04276   0.03841   0.0745   0.0052   0.9985
  17.500   1.2391   0.04514   0.04091   0.0747   0.0051   0.9992
  17.750   1.2401   0.04782   0.04370   0.0746   0.0051   0.9997
  18.000   1.2363   0.05067   0.04668   0.0750   0.0050   1.0000
  18.250   1.2263   0.05360   0.04972   0.0764   0.0050   1.0000
  18.500   1.2149   0.05695   0.05318   0.0772   0.0049   1.0000
  18.750   1.2011   0.06088   0.05724   0.0774   0.0049   1.0000
  19.000   1.1854   0.06542   0.06190   0.0770   0.0049   1.0000
  19.250   1.1665   0.07083   0.06746   0.0756   0.0048   1.0000
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