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NACA 0012 AIRFOILS (n0012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 0012 AIRFOILS (n0012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.44 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n0012-il-1000000-n5.txt
Download as CSV file: xf-n0012-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0012 AIRFOILS                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.2322   0.11416   0.11116   0.0052   1.0000   0.0103
 -19.000  -1.2711   0.10336   0.10020  -0.0004   1.0000   0.0103
 -18.750  -1.3084   0.09309   0.08977  -0.0057   1.0000   0.0103
 -18.500  -1.3433   0.08350   0.08002  -0.0106   1.0000   0.0102
 -18.250  -1.3730   0.07497   0.07133  -0.0150   1.0000   0.0102
 -18.000  -1.3978   0.06745   0.06366  -0.0188   1.0000   0.0102
 -17.750  -1.4170   0.06096   0.05702  -0.0221   1.0000   0.0103
 -17.500  -1.4317   0.05530   0.05123  -0.0249   1.0000   0.0103
 -17.250  -1.4420   0.05042   0.04621  -0.0272   1.0000   0.0104
 -17.000  -1.4487   0.04625   0.04192  -0.0289   1.0000   0.0105
 -16.750  -1.4524   0.04263   0.03818  -0.0303   1.0000   0.0106
 -16.500  -1.4536   0.03953   0.03497  -0.0312   1.0000   0.0107
 -16.250  -1.4526   0.03684   0.03218  -0.0316   1.0000   0.0109
 -16.000  -1.4496   0.03454   0.02978  -0.0317   1.0000   0.0110
 -15.750  -1.4453   0.03254   0.02768  -0.0314   1.0000   0.0111
 -15.500  -1.4413   0.03064   0.02568  -0.0308   1.0000   0.0113
 -15.250  -1.4375   0.02886   0.02382  -0.0298   1.0000   0.0115
 -15.000  -1.4313   0.02740   0.02228  -0.0286   1.0000   0.0117
 -14.750  -1.4233   0.02616   0.02097  -0.0272   1.0000   0.0119
 -14.500  -1.4140   0.02508   0.01983  -0.0257   1.0000   0.0122
 -14.250  -1.4035   0.02413   0.01881  -0.0240   1.0000   0.0124
 -14.000  -1.3922   0.02328   0.01790  -0.0222   1.0000   0.0127
 -13.750  -1.3800   0.02252   0.01708  -0.0204   1.0000   0.0129
 -13.500  -1.3670   0.02183   0.01633  -0.0185   1.0000   0.0132
 -13.250  -1.3515   0.02118   0.01561  -0.0170   1.0000   0.0135
 -13.000  -1.3339   0.02057   0.01494  -0.0158   1.0000   0.0137
 -12.750  -1.3161   0.01993   0.01424  -0.0145   1.0000   0.0140
 -12.500  -1.2980   0.01928   0.01355  -0.0134   1.0000   0.0144
 -12.250  -1.2785   0.01870   0.01294  -0.0123   1.0000   0.0149
 -12.000  -1.2583   0.01817   0.01238  -0.0114   1.0000   0.0154
 -11.750  -1.2374   0.01768   0.01184  -0.0105   1.0000   0.0160
 -11.500  -1.2159   0.01721   0.01134  -0.0096   1.0000   0.0165
 -11.250  -1.1940   0.01678   0.01086  -0.0088   1.0000   0.0168
 -11.000  -1.1728   0.01627   0.01032  -0.0079   1.0000   0.0175
 -10.750  -1.1510   0.01581   0.00984  -0.0071   1.0000   0.0182
 -10.500  -1.1288   0.01539   0.00940  -0.0062   1.0000   0.0189
 -10.250  -1.1063   0.01501   0.00899  -0.0054   1.0000   0.0196
 -10.000  -1.0836   0.01466   0.00860  -0.0046   1.0000   0.0202
  -9.750  -1.0617   0.01426   0.00819  -0.0037   1.0000   0.0212
  -9.500  -1.0398   0.01389   0.00782  -0.0027   1.0000   0.0223
  -9.250  -1.0178   0.01357   0.00748  -0.0016   1.0000   0.0233
  -9.000  -0.9958   0.01328   0.00716  -0.0006   1.0000   0.0242
  -8.750  -0.9743   0.01294   0.00682   0.0006   1.0000   0.0255
  -8.500  -0.9529   0.01263   0.00651   0.0018   1.0000   0.0269
  -8.250  -0.9313   0.01236   0.00623   0.0029   1.0000   0.0283
  -8.000  -0.9005   0.01203   0.00590   0.0021   0.9984   0.0303
  -7.750  -0.8690   0.01171   0.00559   0.0011   0.9965   0.0326
  -7.500  -0.8368   0.01143   0.00530   0.0000   0.9948   0.0347
  -7.250  -0.8051   0.01112   0.00501  -0.0010   0.9929   0.0379
  -7.000  -0.7742   0.01085   0.00475  -0.0017   0.9900   0.0410
  -6.750  -0.7427   0.01055   0.00448  -0.0027   0.9870   0.0451
  -6.500  -0.7107   0.01029   0.00424  -0.0037   0.9840   0.0492
  -6.250  -0.6808   0.01003   0.00400  -0.0042   0.9793   0.0545
  -6.000  -0.6509   0.00976   0.00377  -0.0047   0.9739   0.0606
  -5.750  -0.6204   0.00952   0.00355  -0.0053   0.9686   0.0672
  -5.250  -0.5637   0.00904   0.00315  -0.0055   0.9523   0.0847
  -5.000  -0.5365   0.00881   0.00296  -0.0054   0.9419   0.0960
  -4.750  -0.5098   0.00859   0.00278  -0.0051   0.9300   0.1079
  -4.500  -0.4834   0.00838   0.00260  -0.0047   0.9169   0.1219
  -4.250  -0.4572   0.00818   0.00243  -0.0043   0.9023   0.1376
  -4.000  -0.4309   0.00800   0.00228  -0.0038   0.8864   0.1545
  -3.750  -0.4047   0.00782   0.00212  -0.0034   0.8691   0.1731
  -3.500  -0.3784   0.00765   0.00198  -0.0031   0.8504   0.1944
  -3.250  -0.3519   0.00750   0.00185  -0.0027   0.8303   0.2158
  -3.000  -0.3254   0.00736   0.00173  -0.0023   0.8095   0.2384
  -2.750  -0.2987   0.00724   0.00162  -0.0021   0.7881   0.2625
  -2.500  -0.2720   0.00712   0.00153  -0.0018   0.7656   0.2864
  -2.250  -0.2451   0.00703   0.00144  -0.0015   0.7430   0.3111
  -2.000  -0.2182   0.00693   0.00137  -0.0013   0.7204   0.3359
  -1.750  -0.1910   0.00687   0.00130  -0.0011   0.6968   0.3603
  -1.500  -0.1640   0.00680   0.00125  -0.0009   0.6734   0.3859
  -1.000  -0.1095   0.00670   0.00116  -0.0006   0.6261   0.4352
  -0.750  -0.0821   0.00667   0.00114  -0.0004   0.6023   0.4588
  -0.500  -0.0548   0.00664   0.00112  -0.0003   0.5787   0.4830
  -0.250  -0.0274   0.00663   0.00110  -0.0001   0.5554   0.5071
   0.000   0.0000   0.00662   0.00110   0.0000   0.5313   0.5314
   0.250   0.0274   0.00663   0.00110   0.0001   0.5074   0.5554
   0.500   0.0548   0.00664   0.00112   0.0003   0.4831   0.5785
   0.750   0.0821   0.00667   0.00114   0.0004   0.4590   0.6023
   1.000   0.1096   0.00670   0.00116   0.0006   0.4351   0.6261
   1.250   0.1367   0.00675   0.00120   0.0007   0.4103   0.6495
   1.500   0.1640   0.00680   0.00125   0.0009   0.3850   0.6733
   1.750   0.1911   0.00687   0.00130   0.0011   0.3607   0.6966
   2.000   0.2182   0.00693   0.00137   0.0013   0.3357   0.7205
   2.250   0.2451   0.00703   0.00144   0.0015   0.3111   0.7429
   2.500   0.2720   0.00712   0.00153   0.0018   0.2866   0.7657
   2.750   0.2987   0.00724   0.00162   0.0021   0.2622   0.7881
   3.000   0.3254   0.00736   0.00173   0.0024   0.2384   0.8097
   3.250   0.3519   0.00751   0.00185   0.0027   0.2157   0.8303
   3.500   0.3784   0.00765   0.00198   0.0031   0.1946   0.8502
   3.750   0.4047   0.00782   0.00212   0.0034   0.1730   0.8690
   4.000   0.4309   0.00800   0.00228   0.0038   0.1545   0.8865
   4.250   0.4572   0.00818   0.00243   0.0043   0.1373   0.9024
   4.500   0.4835   0.00838   0.00260   0.0047   0.1222   0.9169
   4.750   0.5098   0.00859   0.00278   0.0050   0.1078   0.9299
   5.000   0.5365   0.00881   0.00296   0.0054   0.0959   0.9419
   5.250   0.5637   0.00904   0.00315   0.0055   0.0847   0.9524
   5.750   0.6204   0.00952   0.00356   0.0053   0.0671   0.9686
   6.000   0.6509   0.00976   0.00377   0.0047   0.0606   0.9739
   6.250   0.6809   0.01003   0.00400   0.0042   0.0545   0.9794
   6.500   0.7108   0.01029   0.00424   0.0036   0.0492   0.9840
   6.750   0.7428   0.01055   0.00448   0.0026   0.0451   0.9870
   7.000   0.7743   0.01085   0.00475   0.0017   0.0410   0.9900
   7.250   0.8051   0.01112   0.00501   0.0010   0.0379   0.9929
   7.500   0.8369   0.01143   0.00530  -0.0001   0.0347   0.9948
   7.750   0.8691   0.01171   0.00559  -0.0012   0.0326   0.9966
   8.000   0.9006   0.01203   0.00590  -0.0021   0.0303   0.9985
   8.250   0.9312   0.01236   0.00623  -0.0029   0.0283   1.0000
   8.500   0.9528   0.01263   0.00651  -0.0017   0.0269   1.0000
   8.750   0.9743   0.01294   0.00682  -0.0006   0.0255   1.0000
   9.000   0.9957   0.01328   0.00716   0.0006   0.0242   1.0000
   9.250   1.0178   0.01357   0.00748   0.0016   0.0233   1.0000
   9.500   1.0398   0.01389   0.00782   0.0027   0.0223   1.0000
   9.750   1.0617   0.01426   0.00819   0.0036   0.0212   1.0000
  10.000   1.0836   0.01466   0.00860   0.0046   0.0202   1.0000
  10.250   1.1063   0.01501   0.00899   0.0054   0.0196   1.0000
  10.500   1.1288   0.01539   0.00940   0.0062   0.0189   1.0000
  10.750   1.1511   0.01581   0.00984   0.0071   0.0182   1.0000
  11.000   1.1729   0.01627   0.01031   0.0079   0.0175   1.0000
  11.250   1.1942   0.01678   0.01085   0.0088   0.0168   1.0000
  11.500   1.2161   0.01721   0.01134   0.0096   0.0165   1.0000
  11.750   1.2375   0.01768   0.01185   0.0104   0.0160   1.0000
  12.000   1.2585   0.01817   0.01238   0.0113   0.0154   1.0000
  12.250   1.2788   0.01870   0.01294   0.0123   0.0149   1.0000
  12.500   1.2982   0.01928   0.01355   0.0133   0.0144   1.0000
  12.750   1.3164   0.01993   0.01424   0.0145   0.0140   1.0000
  13.000   1.3343   0.02057   0.01494   0.0157   0.0137   1.0000
  13.250   1.3519   0.02118   0.01561   0.0169   0.0134   1.0000
  13.500   1.3675   0.02183   0.01632   0.0184   0.0132   1.0000
  13.750   1.3806   0.02252   0.01708   0.0203   0.0129   1.0000
  14.000   1.3928   0.02328   0.01790   0.0221   0.0127   1.0000
  14.250   1.4043   0.02412   0.01881   0.0239   0.0124   1.0000
  14.500   1.4148   0.02507   0.01982   0.0255   0.0122   1.0000
  14.750   1.4241   0.02615   0.02096   0.0271   0.0119   1.0000
  15.000   1.4322   0.02739   0.02227   0.0284   0.0117   1.0000
  15.250   1.4385   0.02885   0.02381   0.0297   0.0115   1.0000
  15.500   1.4424   0.03062   0.02566   0.0306   0.0113   1.0000
  15.750   1.4465   0.03252   0.02766   0.0312   0.0111   1.0000
  16.000   1.4511   0.03450   0.02973   0.0315   0.0110   1.0000
  16.250   1.4540   0.03682   0.03215   0.0314   0.0109   1.0000
  16.500   1.4551   0.03948   0.03492   0.0309   0.0107   1.0000
  16.750   1.4542   0.04256   0.03811   0.0301   0.0106   1.0000
  17.000   1.4508   0.04615   0.04182   0.0287   0.0105   1.0000
  17.250   1.4442   0.05033   0.04612   0.0270   0.0104   1.0000
  17.500   1.4341   0.05518   0.05110   0.0247   0.0103   1.0000
  17.750   1.4197   0.06081   0.05687   0.0219   0.0103   1.0000
  18.000   1.4004   0.06732   0.06353   0.0186   0.0102   1.0000
  18.250   1.3762   0.07477   0.07113   0.0148   0.0102   1.0000
  18.500   1.3466   0.08329   0.07981   0.0104   0.0102   1.0000
  18.750   1.3115   0.09292   0.08959   0.0054   0.0102   1.0000
  19.000   1.2739   0.10324   0.10008   0.0001   0.0103   1.0000
  19.250   1.2349   0.11407   0.11107  -0.0055   0.0103   1.0000
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