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NACA 0010-65 (naca001065-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 0010-65 (naca001065-il)
Reynolds number: 1,000,000
Max Cl/Cd: 65.31 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca001065-il-1000000-n5.txt
Download as CSV file: xf-naca001065-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010-65                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.2134   0.06115   0.05851  -0.0552   1.0000   0.0047
 -17.000  -1.2490   0.05223   0.04934  -0.0601   1.0000   0.0046
 -16.750  -1.2699   0.04700   0.04393  -0.0612   1.0000   0.0047
 -16.500  -1.2844   0.04312   0.03989  -0.0609   1.0000   0.0047
 -16.250  -1.2943   0.04007   0.03669  -0.0597   1.0000   0.0047
 -16.000  -1.3011   0.03754   0.03401  -0.0580   1.0000   0.0048
 -15.750  -1.3050   0.03541   0.03175  -0.0559   1.0000   0.0049
 -15.500  -1.3069   0.03355   0.02976  -0.0536   1.0000   0.0050
 -15.250  -1.3068   0.03194   0.02801  -0.0511   1.0000   0.0050
 -15.000  -1.3053   0.03050   0.02645  -0.0484   1.0000   0.0051
 -14.750  -1.3027   0.02924   0.02506  -0.0455   1.0000   0.0052
 -14.500  -1.2997   0.02810   0.02381  -0.0424   1.0000   0.0053
 -14.250  -1.2967   0.02710   0.02270  -0.0390   1.0000   0.0054
 -14.000  -1.2941   0.02621   0.02171  -0.0353   1.0000   0.0055
 -13.750  -1.2922   0.02545   0.02085  -0.0312   1.0000   0.0056
 -13.500  -1.2922   0.02481   0.02012  -0.0265   1.0000   0.0057
 -13.250  -1.2936   0.02427   0.01949  -0.0213   1.0000   0.0058
 -13.000  -1.2816   0.02323   0.01834  -0.0192   0.9993   0.0061
 -12.750  -1.2614   0.02223   0.01725  -0.0187   0.9982   0.0064
 -12.500  -1.2400   0.02137   0.01629  -0.0183   0.9971   0.0067
 -12.250  -1.2179   0.02060   0.01544  -0.0181   0.9961   0.0071
 -12.000  -1.1948   0.01988   0.01463  -0.0179   0.9953   0.0074
 -11.750  -1.1706   0.01921   0.01386  -0.0179   0.9946   0.0077
 -11.500  -1.1475   0.01861   0.01317  -0.0176   0.9935   0.0080
 -11.250  -1.1254   0.01794   0.01243  -0.0171   0.9920   0.0085
 -11.000  -1.1022   0.01732   0.01174  -0.0167   0.9907   0.0091
 -10.750  -1.0778   0.01676   0.01114  -0.0166   0.9896   0.0098
 -10.500  -1.0522   0.01625   0.01057  -0.0167   0.9885   0.0105
 -10.250  -1.0259   0.01576   0.01002  -0.0169   0.9876   0.0112
 -10.000  -0.9990   0.01530   0.00955  -0.0173   0.9869   0.0126
  -9.750  -0.9716   0.01490   0.00914  -0.0177   0.9862   0.0139
  -9.500  -0.9437   0.01452   0.00870  -0.0182   0.9857   0.0149
  -9.250  -0.9150   0.01418   0.00837  -0.0188   0.9852   0.0164
  -9.000  -0.8907   0.01393   0.00812  -0.0184   0.9832   0.0178
  -8.750  -0.8649   0.01368   0.00786  -0.0183   0.9815   0.0190
  -8.500  -0.8378   0.01346   0.00760  -0.0185   0.9802   0.0198
  -8.250  -0.8100   0.01325   0.00735  -0.0188   0.9790   0.0203
  -8.000  -0.7835   0.01279   0.00687  -0.0189   0.9778   0.0215
  -7.750  -0.7555   0.01250   0.00657  -0.0193   0.9768   0.0226
  -7.500  -0.7270   0.01225   0.00632  -0.0198   0.9759   0.0236
  -7.250  -0.6987   0.01199   0.00603  -0.0202   0.9750   0.0245
  -7.000  -0.6736   0.01176   0.00577  -0.0198   0.9730   0.0253
  -6.750  -0.6496   0.01154   0.00553  -0.0192   0.9704   0.0260
  -6.500  -0.6235   0.01133   0.00530  -0.0190   0.9684   0.0266
  -6.250  -0.5965   0.01111   0.00506  -0.0191   0.9667   0.0270
  -6.000  -0.5691   0.01090   0.00482  -0.0192   0.9652   0.0272
  -5.750  -0.5429   0.01055   0.00443  -0.0191   0.9637   0.0281
  -5.500  -0.5160   0.01023   0.00408  -0.0191   0.9624   0.0291
  -5.250  -0.4935   0.01000   0.00384  -0.0180   0.9592   0.0301
  -5.000  -0.4686   0.00979   0.00362  -0.0175   0.9566   0.0314
  -4.750  -0.4426   0.00959   0.00342  -0.0173   0.9543   0.0324
  -4.500  -0.4161   0.00939   0.00322  -0.0171   0.9523   0.0332
  -4.250  -0.3889   0.00921   0.00302  -0.0171   0.9505   0.0341
  -4.000  -0.3615   0.00905   0.00284  -0.0171   0.9488   0.0350
  -3.750  -0.3372   0.00892   0.00271  -0.0165   0.9457   0.0358
  -3.500  -0.3119   0.00876   0.00257  -0.0160   0.9428   0.0390
  -3.250  -0.2860   0.00859   0.00243  -0.0157   0.9401   0.0441
  -3.000  -0.2600   0.00837   0.00229  -0.0154   0.9377   0.0587
  -2.750  -0.2331   0.00818   0.00216  -0.0153   0.9356   0.0738
  -2.500  -0.2071   0.00803   0.00206  -0.0150   0.9331   0.0862
  -2.250  -0.1825   0.00786   0.00198  -0.0145   0.9297   0.1034
  -2.000  -0.1580   0.00763   0.00188  -0.0139   0.9265   0.1374
  -1.750  -0.1328   0.00740   0.00179  -0.0134   0.9236   0.1735
  -1.500  -0.1076   0.00712   0.00168  -0.0130   0.9210   0.2245
  -1.250  -0.0846   0.00677   0.00159  -0.0122   0.9177   0.2960
  -1.000  -0.0664   0.00624   0.00146  -0.0103   0.9108   0.4125
  -0.750  -0.0593   0.00514   0.00119  -0.0060   0.9007   0.6464
  -0.500  -0.0447   0.00465   0.00108  -0.0030   0.8877   0.7556
  -0.250  -0.0237   0.00445   0.00103  -0.0012   0.8690   0.8095
   0.000   0.0000   0.00440   0.00101   0.0000   0.8425   0.8429
   0.250   0.0238   0.00445   0.00103   0.0012   0.8096   0.8691
   0.500   0.0447   0.00465   0.00108   0.0030   0.7548   0.8874
   0.750   0.0596   0.00514   0.00119   0.0060   0.6481   0.9006
   1.000   0.0663   0.00624   0.00146   0.0103   0.4114   0.9108
   1.250   0.0847   0.00677   0.00159   0.0122   0.2959   0.9178
   1.500   0.1076   0.00711   0.00168   0.0130   0.2251   0.9210
   1.750   0.1329   0.00740   0.00179   0.0134   0.1741   0.9236
   2.000   0.1581   0.00763   0.00188   0.0139   0.1378   0.9264
   2.250   0.1826   0.00786   0.00198   0.0144   0.1033   0.9297
   2.500   0.2072   0.00803   0.00206   0.0150   0.0863   0.9331
   2.750   0.2332   0.00818   0.00216   0.0153   0.0741   0.9356
   3.000   0.2601   0.00837   0.00229   0.0154   0.0587   0.9377
   3.250   0.2861   0.00859   0.00243   0.0157   0.0442   0.9401
   3.500   0.3119   0.00876   0.00257   0.0160   0.0390   0.9428
   3.750   0.3373   0.00892   0.00271   0.0164   0.0358   0.9457
   4.000   0.3616   0.00905   0.00284   0.0171   0.0350   0.9488
   4.250   0.3890   0.00921   0.00302   0.0171   0.0341   0.9505
   4.500   0.4161   0.00939   0.00322   0.0171   0.0332   0.9523
   4.750   0.4427   0.00959   0.00342   0.0173   0.0324   0.9543
   5.000   0.4687   0.00979   0.00362   0.0175   0.0314   0.9566
   5.250   0.4936   0.01000   0.00384   0.0180   0.0301   0.9592
   5.500   0.5161   0.01023   0.00408   0.0190   0.0291   0.9624
   5.750   0.5430   0.01054   0.00442   0.0191   0.0281   0.9637
   6.000   0.5692   0.01090   0.00482   0.0192   0.0272   0.9652
   6.250   0.5966   0.01111   0.00506   0.0191   0.0270   0.9667
   6.500   0.6236   0.01133   0.00530   0.0190   0.0266   0.9684
   6.750   0.6497   0.01155   0.00553   0.0192   0.0260   0.9704
   7.000   0.6737   0.01176   0.00577   0.0198   0.0253   0.9730
   7.250   0.6988   0.01199   0.00603   0.0202   0.0245   0.9750
   7.500   0.7271   0.01225   0.00632   0.0197   0.0236   0.9759
   7.750   0.7556   0.01249   0.00657   0.0193   0.0226   0.9768
   8.000   0.7835   0.01279   0.00686   0.0189   0.0215   0.9778
   8.250   0.8101   0.01325   0.00735   0.0188   0.0203   0.9790
   8.500   0.8379   0.01345   0.00760   0.0185   0.0198   0.9802
   8.750   0.8650   0.01368   0.00786   0.0183   0.0190   0.9816
   9.000   0.8907   0.01392   0.00812   0.0184   0.0178   0.9833
   9.250   0.9152   0.01418   0.00837   0.0188   0.0165   0.9852
   9.500   0.9439   0.01452   0.00870   0.0181   0.0149   0.9857
   9.750   0.9718   0.01490   0.00914   0.0176   0.0140   0.9863
  10.000   0.9992   0.01530   0.00955   0.0172   0.0126   0.9869
  10.250   1.0260   0.01576   0.01002   0.0169   0.0112   0.9876
  10.500   1.0524   0.01625   0.01057   0.0167   0.0105   0.9885
  10.750   1.0780   0.01676   0.01114   0.0166   0.0098   0.9896
  11.000   1.1025   0.01732   0.01174   0.0167   0.0091   0.9908
  11.250   1.1257   0.01794   0.01243   0.0170   0.0085   0.9921
  11.500   1.1479   0.01860   0.01317   0.0175   0.0080   0.9935
  11.750   1.1711   0.01921   0.01387   0.0178   0.0077   0.9946
  12.000   1.1952   0.01988   0.01463   0.0178   0.0074   0.9953
  12.250   1.2183   0.02060   0.01543   0.0180   0.0071   0.9962
  12.500   1.2404   0.02137   0.01629   0.0183   0.0067   0.9971
  12.750   1.2617   0.02223   0.01725   0.0186   0.0064   0.9982
  13.000   1.2819   0.02323   0.01834   0.0191   0.0061   0.9993
  13.250   1.2938   0.02426   0.01948   0.0212   0.0058   1.0000
  13.500   1.2924   0.02481   0.02011   0.0264   0.0057   1.0000
  13.750   1.2925   0.02544   0.02084   0.0311   0.0056   1.0000
  14.000   1.2944   0.02621   0.02171   0.0352   0.0055   1.0000
  14.250   1.2973   0.02709   0.02269   0.0389   0.0054   1.0000
  14.500   1.3003   0.02810   0.02381   0.0423   0.0053   1.0000
  14.750   1.3035   0.02924   0.02507   0.0454   0.0052   1.0000
  15.000   1.3062   0.03051   0.02645   0.0482   0.0051   1.0000
  15.250   1.3077   0.03195   0.02802   0.0509   0.0050   1.0000
  15.500   1.3081   0.03356   0.02977   0.0534   0.0049   1.0000
  15.750   1.3062   0.03542   0.03176   0.0557   0.0049   1.0000
  16.000   1.3026   0.03754   0.03402   0.0577   0.0048   1.0000
  16.250   1.2959   0.04007   0.03669   0.0594   0.0047   1.0000
  16.500   1.2860   0.04313   0.03990   0.0606   0.0047   1.0000
  16.750   1.2716   0.04700   0.04394   0.0609   0.0046   1.0000
  17.000   1.2509   0.05223   0.04935   0.0598   0.0046   1.0000
  17.250   1.2152   0.06121   0.05857   0.0548   0.0047   1.0000
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