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NACA 64-012A AIRFOIL (n64012a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 64-012A AIRFOIL (n64012a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 61.91 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n64012a-il-1000000.txt
Download as CSV file: xf-n64012a-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64-012A AIRFOIL                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.9398   0.10817   0.10633   0.0037   1.0000   0.0098
 -15.500  -0.9636   0.09691   0.09493  -0.0032   1.0000   0.0097
 -15.250  -0.9799   0.08825   0.08615  -0.0088   1.0000   0.0096
 -15.000  -0.9972   0.08028   0.07806  -0.0140   1.0000   0.0096
 -14.750  -1.0140   0.07316   0.07080  -0.0185   1.0000   0.0096
 -14.500  -1.0341   0.06620   0.06369  -0.0225   1.0000   0.0096
 -14.250  -1.0565   0.05948   0.05678  -0.0259   1.0000   0.0096
 -14.000  -1.0802   0.05319   0.05026  -0.0283   1.0000   0.0096
 -13.750  -1.1057   0.04720   0.04403  -0.0297   1.0000   0.0096
 -13.500  -1.1308   0.04171   0.03825  -0.0298   1.0000   0.0097
 -13.250  -1.1466   0.03757   0.03387  -0.0289   1.0000   0.0098
 -13.000  -1.1524   0.03470   0.03082  -0.0276   1.0000   0.0100
 -12.750  -1.1511   0.03271   0.02871  -0.0262   1.0000   0.0101
 -12.500  -1.1461   0.03117   0.02707  -0.0248   1.0000   0.0103
 -12.250  -1.1387   0.02992   0.02573  -0.0232   1.0000   0.0104
 -12.000  -1.1301   0.02879   0.02451  -0.0215   1.0000   0.0106
 -11.750  -1.1205   0.02771   0.02334  -0.0196   1.0000   0.0108
 -11.500  -1.1093   0.02665   0.02216  -0.0179   1.0000   0.0110
 -11.250  -1.0950   0.02557   0.02098  -0.0165   1.0000   0.0112
 -11.000  -1.0795   0.02450   0.01979  -0.0153   1.0000   0.0115
 -10.750  -1.0625   0.02353   0.01872  -0.0142   1.0000   0.0118
 -10.500  -1.0442   0.02270   0.01779  -0.0131   1.0000   0.0121
 -10.250  -1.0250   0.02194   0.01693  -0.0122   1.0000   0.0124
 -10.000  -1.0052   0.02120   0.01609  -0.0113   1.0000   0.0125
  -9.750  -0.9846   0.02056   0.01537  -0.0104   1.0000   0.0127
  -9.500  -0.9725   0.01836   0.01299  -0.0085   1.0000   0.0131
  -9.250  -0.9550   0.01734   0.01191  -0.0072   1.0000   0.0135
  -9.000  -0.9352   0.01667   0.01122  -0.0061   1.0000   0.0139
  -8.750  -0.9149   0.01612   0.01063  -0.0050   1.0000   0.0143
  -8.500  -0.8951   0.01558   0.01006  -0.0038   1.0000   0.0147
  -8.250  -0.8755   0.01510   0.00955  -0.0025   1.0000   0.0152
  -8.000  -0.8564   0.01467   0.00907  -0.0011   1.0000   0.0156
  -7.750  -0.8381   0.01422   0.00859   0.0005   1.0000   0.0160
  -7.500  -0.8202   0.01380   0.00813   0.0022   0.9999   0.0163
  -7.250  -0.7874   0.01315   0.00743   0.0007   0.9971   0.0167
  -7.000  -0.7558   0.01221   0.00641  -0.0008   0.9939   0.0178
  -6.750  -0.7235   0.01174   0.00594  -0.0022   0.9894   0.0188
  -6.500  -0.6897   0.01134   0.00552  -0.0038   0.9849   0.0199
  -6.250  -0.6579   0.01101   0.00516  -0.0049   0.9777   0.0210
  -6.000  -0.6262   0.01053   0.00463  -0.0060   0.9699   0.0228
  -5.750  -0.5980   0.01017   0.00426  -0.0063   0.9575   0.0251
  -5.500  -0.5709   0.00993   0.00398  -0.0062   0.9431   0.0273
  -5.250  -0.5464   0.00958   0.00361  -0.0056   0.9269   0.0326
  -5.000  -0.5216   0.00932   0.00332  -0.0050   0.9109   0.0396
  -4.750  -0.4968   0.00906   0.00307  -0.0044   0.8953   0.0512
  -4.500  -0.4719   0.00877   0.00282  -0.0040   0.8804   0.0714
  -4.250  -0.4476   0.00840   0.00256  -0.0035   0.8665   0.1087
  -4.000  -0.4242   0.00788   0.00228  -0.0029   0.8534   0.1741
  -3.750  -0.4020   0.00721   0.00197  -0.0022   0.8409   0.2707
  -3.500  -0.3816   0.00637   0.00163  -0.0012   0.8292   0.4068
  -3.250  -0.3576   0.00599   0.00149  -0.0007   0.8185   0.4865
  -3.000  -0.3314   0.00581   0.00141  -0.0004   0.8083   0.5268
  -2.750  -0.3043   0.00572   0.00134  -0.0003   0.7989   0.5502
  -2.500  -0.2772   0.00565   0.00127  -0.0001   0.7894   0.5691
  -2.250  -0.2497   0.00559   0.00123  -0.0001   0.7800   0.5874
  -2.000  -0.2224   0.00555   0.00118   0.0000   0.7712   0.6054
  -1.750  -0.1950   0.00549   0.00115   0.0001   0.7623   0.6248
  -1.500  -0.1676   0.00544   0.00114   0.0002   0.7541   0.6432
  -1.250  -0.1400   0.00542   0.00112   0.0002   0.7455   0.6567
  -1.000  -0.1120   0.00541   0.00110   0.0002   0.7371   0.6688
  -0.750  -0.0843   0.00540   0.00108   0.0002   0.7287   0.6799
  -0.500  -0.0562   0.00538   0.00107   0.0001   0.7205   0.6885
  -0.250  -0.0282   0.00540   0.00106   0.0001   0.7127   0.6966
   0.000   0.0000   0.00537   0.00106   0.0000   0.7044   0.7044
   0.250   0.0281   0.00540   0.00106  -0.0001   0.6966   0.7127
   0.500   0.0562   0.00538   0.00107  -0.0001   0.6884   0.7205
   0.750   0.0843   0.00540   0.00108  -0.0002   0.6799   0.7287
   1.000   0.1119   0.00541   0.00110  -0.0002   0.6688   0.7371
   1.250   0.1399   0.00542   0.00112  -0.0002   0.6568   0.7455
   1.500   0.1676   0.00544   0.00114  -0.0002   0.6432   0.7541
   1.750   0.1949   0.00549   0.00115  -0.0001   0.6249   0.7623
   2.000   0.2223   0.00555   0.00118   0.0000   0.6054   0.7712
   2.250   0.2497   0.00559   0.00123   0.0001   0.5874   0.7800
   2.500   0.2772   0.00565   0.00127   0.0002   0.5692   0.7894
   2.750   0.3043   0.00572   0.00134   0.0003   0.5502   0.7989
   3.000   0.3314   0.00581   0.00141   0.0004   0.5267   0.8083
   3.250   0.3575   0.00599   0.00149   0.0007   0.4862   0.8185
   3.500   0.3817   0.00636   0.00163   0.0012   0.4078   0.8292
   3.750   0.4021   0.00721   0.00197   0.0022   0.2710   0.8409
   4.000   0.4243   0.00788   0.00228   0.0029   0.1742   0.8534
   4.250   0.4477   0.00840   0.00256   0.0034   0.1088   0.8665
   4.500   0.4720   0.00877   0.00282   0.0039   0.0715   0.8805
   4.750   0.4969   0.00906   0.00307   0.0044   0.0512   0.8953
   5.000   0.5217   0.00932   0.00333   0.0050   0.0396   0.9109
   5.250   0.5465   0.00958   0.00361   0.0055   0.0326   0.9269
   5.500   0.5711   0.00993   0.00398   0.0061   0.0272   0.9430
   5.750   0.5981   0.01017   0.00426   0.0062   0.0251   0.9575
   6.000   0.6262   0.01053   0.00463   0.0060   0.0227   0.9700
   6.250   0.6580   0.01101   0.00515   0.0049   0.0209   0.9778
   6.500   0.6898   0.01134   0.00552   0.0037   0.0199   0.9849
   6.750   0.7235   0.01174   0.00594   0.0021   0.0188   0.9894
   7.000   0.7559   0.01221   0.00641   0.0008   0.0178   0.9940
   7.250   0.7874   0.01318   0.00745  -0.0007   0.0167   0.9972
   7.500   0.8204   0.01380   0.00813  -0.0023   0.0163   1.0000
   7.750   0.8379   0.01422   0.00859  -0.0005   0.0160   1.0000
   8.000   0.8563   0.01466   0.00907   0.0011   0.0156   1.0000
   8.250   0.8754   0.01510   0.00955   0.0026   0.0152   1.0000
   8.500   0.8951   0.01558   0.01006   0.0038   0.0147   1.0000
   8.750   0.9151   0.01611   0.01062   0.0050   0.0143   1.0000
   9.000   0.9354   0.01668   0.01122   0.0060   0.0139   1.0000
   9.250   0.9553   0.01734   0.01192   0.0071   0.0135   1.0000
   9.500   0.9728   0.01838   0.01302   0.0084   0.0131   1.0000
   9.750   0.9851   0.02056   0.01537   0.0103   0.0127   1.0000
  10.000   1.0058   0.02120   0.01610   0.0112   0.0125   1.0000
  10.250   1.0256   0.02195   0.01694   0.0121   0.0124   1.0000
  10.500   1.0449   0.02271   0.01780   0.0130   0.0121   1.0000
  10.750   1.0633   0.02354   0.01873   0.0140   0.0118   1.0000
  11.000   1.0803   0.02451   0.01981   0.0151   0.0115   1.0000
  11.250   1.0959   0.02558   0.02099   0.0163   0.0112   1.0000
  11.500   1.1103   0.02665   0.02216   0.0177   0.0110   1.0000
  11.750   1.1216   0.02773   0.02335   0.0194   0.0108   1.0000
  12.000   1.1314   0.02880   0.02452   0.0212   0.0106   1.0000
  12.250   1.1401   0.02991   0.02573   0.0229   0.0104   1.0000
  12.500   1.1473   0.03119   0.02709   0.0245   0.0103   1.0000
  12.750   1.1524   0.03273   0.02873   0.0260   0.0101   1.0000
  13.000   1.1536   0.03475   0.03087   0.0273   0.0100   1.0000
  13.250   1.1473   0.03769   0.03399   0.0286   0.0098   1.0000
  13.500   1.1306   0.04194   0.03850   0.0295   0.0097   1.0000
  13.750   1.1067   0.04731   0.04414   0.0294   0.0096   1.0000
  14.000   1.0791   0.05361   0.05070   0.0279   0.0096   1.0000
  14.250   1.0557   0.05990   0.05721   0.0254   0.0096   1.0000
  14.500   1.0335   0.06665   0.06415   0.0219   0.0095   1.0000
  14.750   1.0139   0.07359   0.07125   0.0178   0.0096   1.0000
  15.000   0.9968   0.08083   0.07862   0.0133   0.0096   1.0000
  15.250   0.9809   0.08859   0.08650   0.0082   0.0096   1.0000
  15.500   0.9644   0.09733   0.09536   0.0025   0.0097   1.0000
  15.750   0.9388   0.10916   0.10734  -0.0047   0.0098   1.0000
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