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NACA 0012-64 (naca001264-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 0012-64 (naca001264-il)
Reynolds number: 1,000,000
Max Cl/Cd: 63 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca001264-il-1000000.txt
Download as CSV file: xf-naca001264-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0012-64                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.1202   0.11676   0.11433  -0.0124   1.0000   0.0145
 -19.000  -1.1663   0.10394   0.10134  -0.0194   1.0000   0.0144
 -18.750  -1.2069   0.09241   0.08963  -0.0258   1.0000   0.0144
 -18.500  -1.2395   0.08249   0.07954  -0.0313   1.0000   0.0144
 -18.250  -1.2650   0.07414   0.07102  -0.0360   1.0000   0.0144
 -18.000  -1.2831   0.06734   0.06406  -0.0398   1.0000   0.0145
 -17.750  -1.2957   0.06179   0.05836  -0.0426   1.0000   0.0145
 -17.500  -1.3040   0.05713   0.05356  -0.0447   1.0000   0.0146
 -17.250  -1.3131   0.05267   0.04897  -0.0464   1.0000   0.0147
 -17.000  -1.3309   0.04759   0.04372  -0.0477   1.0000   0.0150
 -16.750  -1.3396   0.04386   0.03989  -0.0482   1.0000   0.0152
 -16.500  -1.3413   0.04112   0.03706  -0.0482   1.0000   0.0154
 -16.250  -1.3380   0.03901   0.03488  -0.0480   1.0000   0.0157
 -16.000  -1.3320   0.03725   0.03305  -0.0476   1.0000   0.0159
 -15.750  -1.3252   0.03564   0.03138  -0.0471   1.0000   0.0162
 -15.500  -1.3176   0.03417   0.02983  -0.0463   1.0000   0.0165
 -15.250  -1.3097   0.03278   0.02835  -0.0454   1.0000   0.0168
 -15.000  -1.3010   0.03149   0.02698  -0.0444   1.0000   0.0171
 -14.750  -1.2916   0.03031   0.02571  -0.0433   1.0000   0.0175
 -14.500  -1.2805   0.02929   0.02459  -0.0421   1.0000   0.0178
 -14.250  -1.2675   0.02847   0.02369  -0.0410   1.0000   0.0180
 -14.000  -1.2656   0.02676   0.02186  -0.0387   1.0000   0.0184
 -13.750  -1.2572   0.02565   0.02071  -0.0369   1.0000   0.0189
 -13.500  -1.2438   0.02496   0.01997  -0.0355   1.0000   0.0193
 -13.250  -1.2294   0.02436   0.01934  -0.0341   1.0000   0.0197
 -13.000  -1.2153   0.02375   0.01868  -0.0325   1.0000   0.0201
 -12.750  -1.2010   0.02315   0.01803  -0.0309   1.0000   0.0205
 -12.500  -1.1869   0.02258   0.01739  -0.0291   1.0000   0.0210
 -12.250  -1.1727   0.02206   0.01680  -0.0272   1.0000   0.0214
 -12.000  -1.1587   0.02165   0.01632  -0.0251   1.0000   0.0217
 -11.750  -1.1453   0.02140   0.01601  -0.0227   1.0000   0.0219
 -11.500  -1.1449   0.02016   0.01469  -0.0182   1.0000   0.0226
 -11.250  -1.1349   0.01960   0.01411  -0.0153   1.0000   0.0231
 -11.000  -1.1234   0.01922   0.01371  -0.0125   1.0000   0.0236
 -10.750  -1.1121   0.01886   0.01333  -0.0095   1.0000   0.0240
 -10.500  -1.1008   0.01851   0.01294  -0.0066   1.0000   0.0244
 -10.250  -1.0893   0.01815   0.01254  -0.0036   1.0000   0.0249
 -10.000  -1.0771   0.01782   0.01216  -0.0008   1.0000   0.0254
  -9.750  -1.0638   0.01754   0.01184   0.0018   1.0000   0.0259
  -9.500  -1.0334   0.01724   0.01149   0.0008   0.9990   0.0263
  -9.250  -1.0071   0.01631   0.01049   0.0005   0.9976   0.0271
  -9.000  -0.9795   0.01555   0.00970  -0.0002   0.9962   0.0280
  -8.750  -0.9491   0.01511   0.00925  -0.0012   0.9951   0.0288
  -8.500  -0.9178   0.01471   0.00884  -0.0023   0.9941   0.0296
  -8.250  -0.8881   0.01431   0.00841  -0.0031   0.9927   0.0304
  -8.000  -0.8592   0.01391   0.00798  -0.0037   0.9906   0.0310
  -7.750  -0.8285   0.01360   0.00764  -0.0046   0.9888   0.0316
  -7.500  -0.7988   0.01305   0.00704  -0.0054   0.9871   0.0325
  -7.250  -0.7685   0.01249   0.00646  -0.0063   0.9857   0.0337
  -7.000  -0.7362   0.01210   0.00606  -0.0076   0.9846   0.0348
  -6.750  -0.7031   0.01176   0.00572  -0.0090   0.9837   0.0360
  -6.500  -0.6692   0.01146   0.00541  -0.0106   0.9830   0.0372
  -6.250  -0.6406   0.01120   0.00512  -0.0109   0.9801   0.0380
  -6.000  -0.6117   0.01079   0.00470  -0.0114   0.9773   0.0402
  -5.750  -0.5811   0.01047   0.00440  -0.0122   0.9750   0.0426
  -5.500  -0.5495   0.01020   0.00413  -0.0131   0.9730   0.0451
  -5.250  -0.5190   0.00986   0.00384  -0.0139   0.9709   0.0516
  -5.000  -0.4938   0.00956   0.00362  -0.0134   0.9665   0.0630
  -4.750  -0.4680   0.00927   0.00339  -0.0131   0.9619   0.0784
  -4.500  -0.4411   0.00897   0.00317  -0.0130   0.9581   0.0937
  -4.250  -0.4155   0.00870   0.00298  -0.0126   0.9539   0.1122
  -4.000  -0.3918   0.00841   0.00280  -0.0118   0.9480   0.1383
  -3.750  -0.3672   0.00809   0.00261  -0.0112   0.9431   0.1719
  -3.500  -0.3429   0.00777   0.00245  -0.0105   0.9378   0.2099
  -3.250  -0.3198   0.00740   0.00227  -0.0096   0.9315   0.2591
  -3.000  -0.2972   0.00692   0.00206  -0.0087   0.9260   0.3320
  -2.750  -0.2763   0.00640   0.00188  -0.0074   0.9192   0.4209
  -2.500  -0.2546   0.00593   0.00172  -0.0062   0.9128   0.5053
  -2.250  -0.2326   0.00553   0.00160  -0.0050   0.9064   0.5838
  -2.000  -0.2091   0.00527   0.00152  -0.0041   0.8994   0.6383
  -1.750  -0.1846   0.00507   0.00146  -0.0033   0.8933   0.6855
  -1.500  -0.1593   0.00494   0.00143  -0.0026   0.8861   0.7176
  -1.250  -0.1329   0.00485   0.00139  -0.0022   0.8794   0.7403
  -1.000  -0.1059   0.00480   0.00137  -0.0019   0.8721   0.7571
  -0.750  -0.0793   0.00474   0.00134  -0.0015   0.8632   0.7767
  -0.500  -0.0530   0.00470   0.00133  -0.0010   0.8516   0.7947
  -0.250  -0.0265   0.00467   0.00131  -0.0005   0.8383   0.8094
   0.000   0.0000   0.00467   0.00130   0.0000   0.8238   0.8239
   0.250   0.0265   0.00467   0.00131   0.0005   0.8093   0.8382
   0.500   0.0530   0.00470   0.00133   0.0010   0.7947   0.8515
   0.750   0.0794   0.00474   0.00134   0.0015   0.7767   0.8632
   1.000   0.1060   0.00480   0.00137   0.0019   0.7570   0.8721
   1.250   0.1329   0.00485   0.00139   0.0022   0.7403   0.8794
   1.500   0.1593   0.00494   0.00143   0.0026   0.7176   0.8861
   1.750   0.1846   0.00507   0.00146   0.0033   0.6854   0.8933
   2.000   0.2091   0.00527   0.00152   0.0041   0.6382   0.8994
   2.250   0.2327   0.00553   0.00160   0.0050   0.5843   0.9064
   2.500   0.2546   0.00594   0.00172   0.0062   0.5048   0.9127
   2.750   0.2763   0.00640   0.00189   0.0074   0.4204   0.9192
   3.000   0.2972   0.00692   0.00206   0.0087   0.3322   0.9260
   3.250   0.3199   0.00740   0.00227   0.0096   0.2591   0.9315
   3.500   0.3429   0.00777   0.00245   0.0105   0.2097   0.9378
   3.750   0.3672   0.00809   0.00261   0.0111   0.1719   0.9431
   4.000   0.3919   0.00841   0.00280   0.0117   0.1383   0.9480
   4.250   0.4155   0.00870   0.00298   0.0126   0.1123   0.9539
   4.500   0.4412   0.00897   0.00317   0.0130   0.0937   0.9581
   4.750   0.4680   0.00927   0.00339   0.0131   0.0784   0.9619
   5.000   0.4939   0.00956   0.00362   0.0134   0.0630   0.9665
   5.250   0.5190   0.00986   0.00384   0.0139   0.0516   0.9709
   5.500   0.5496   0.01020   0.00413   0.0131   0.0450   0.9730
   5.750   0.5811   0.01047   0.00440   0.0122   0.0425   0.9750
   6.000   0.6117   0.01079   0.00470   0.0114   0.0401   0.9773
   6.250   0.6406   0.01120   0.00512   0.0109   0.0380   0.9802
   6.500   0.6693   0.01146   0.00541   0.0106   0.0372   0.9830
   6.750   0.7032   0.01176   0.00572   0.0090   0.0360   0.9838
   7.000   0.7363   0.01209   0.00606   0.0076   0.0348   0.9846
   7.250   0.7686   0.01249   0.00646   0.0063   0.0337   0.9857
   7.500   0.7989   0.01305   0.00704   0.0054   0.0325   0.9871
   7.750   0.8286   0.01360   0.00764   0.0046   0.0316   0.9888
   8.000   0.8593   0.01392   0.00798   0.0036   0.0310   0.9907
   8.250   0.8882   0.01431   0.00841   0.0031   0.0304   0.9927
   8.500   0.9179   0.01471   0.00884   0.0023   0.0296   0.9942
   8.750   0.9492   0.01510   0.00924   0.0011   0.0288   0.9951
   9.000   0.9796   0.01555   0.00970   0.0001   0.0280   0.9962
   9.250   1.0073   0.01631   0.01049  -0.0005   0.0271   0.9976
   9.500   1.0336   0.01723   0.01148  -0.0009   0.0263   0.9990
   9.750   1.0637   0.01753   0.01183  -0.0018   0.0259   1.0000
  10.000   1.0769   0.01782   0.01216   0.0009   0.0254   1.0000
  10.250   1.0891   0.01815   0.01254   0.0037   0.0249   1.0000
  10.500   1.1007   0.01851   0.01293   0.0066   0.0244   1.0000
  10.750   1.1120   0.01886   0.01332   0.0096   0.0240   1.0000
  11.000   1.1233   0.01922   0.01371   0.0125   0.0236   1.0000
  11.250   1.1349   0.01960   0.01411   0.0153   0.0231   1.0000
  11.500   1.1450   0.02016   0.01469   0.0182   0.0226   1.0000
  11.750   1.1457   0.02139   0.01601   0.0226   0.0219   1.0000
  12.000   1.1592   0.02165   0.01632   0.0250   0.0217   1.0000
  12.250   1.1733   0.02206   0.01679   0.0270   0.0214   1.0000
  12.500   1.1876   0.02257   0.01738   0.0289   0.0209   1.0000
  12.750   1.2018   0.02315   0.01802   0.0307   0.0205   1.0000
  13.000   1.2161   0.02374   0.01868   0.0324   0.0201   1.0000
  13.250   1.2304   0.02435   0.01933   0.0339   0.0197   1.0000
  13.500   1.2449   0.02494   0.01996   0.0353   0.0193   1.0000
  13.750   1.2583   0.02564   0.02069   0.0367   0.0189   1.0000
  14.000   1.2665   0.02676   0.02186   0.0386   0.0184   1.0000
  14.250   1.2688   0.02846   0.02367   0.0408   0.0180   1.0000
  14.500   1.2821   0.02925   0.02455   0.0419   0.0177   1.0000
  14.750   1.2930   0.03030   0.02569   0.0430   0.0174   1.0000
  15.000   1.3026   0.03146   0.02695   0.0442   0.0171   1.0000
  15.250   1.3113   0.03275   0.02832   0.0452   0.0168   1.0000
  15.500   1.3197   0.03411   0.02977   0.0460   0.0165   1.0000
  15.750   1.3272   0.03559   0.03132   0.0468   0.0162   1.0000
  16.000   1.3342   0.03718   0.03298   0.0473   0.0159   1.0000
  16.250   1.3402   0.03895   0.03481   0.0477   0.0157   1.0000
  16.500   1.3431   0.04110   0.03704   0.0479   0.0154   1.0000
  16.750   1.3415   0.04384   0.03986   0.0479   0.0152   1.0000
  17.000   1.3323   0.04763   0.04377   0.0474   0.0149   1.0000
  17.250   1.3135   0.05287   0.04917   0.0460   0.0147   1.0000
  17.500   1.3072   0.05697   0.05340   0.0444   0.0146   1.0000
  17.750   1.2991   0.06160   0.05817   0.0423   0.0145   1.0000
  18.000   1.2862   0.06720   0.06393   0.0394   0.0144   1.0000
  18.250   1.2682   0.07399   0.07087   0.0357   0.0144   1.0000
  18.500   1.2437   0.08221   0.07925   0.0311   0.0143   1.0000
  18.750   1.2104   0.09223   0.08945   0.0254   0.0144   1.0000
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