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NACA 0012-64 (naca001264-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NACA 0012-64 (naca001264-il)
Reynolds number: 500,000
Max Cl/Cd: 50.85 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca001264-il-500000.txt
Download as CSV file: xf-naca001264-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.6742   0.17732   0.17473   0.0125   1.0000   0.0275
 -16.000  -0.9991   0.08308   0.07993  -0.0373   1.0000   0.0221
 -15.750  -1.0281   0.07406   0.07069  -0.0434   1.0000   0.0221
 -15.500  -1.0555   0.06647   0.06288  -0.0477   1.0000   0.0221
 -15.250  -1.0806   0.06005   0.05625  -0.0503   1.0000   0.0222
 -15.000  -1.0994   0.05497   0.05099  -0.0515   1.0000   0.0223
 -14.750  -1.1090   0.05133   0.04724  -0.0518   1.0000   0.0225
 -14.500  -1.1130   0.04860   0.04442  -0.0516   1.0000   0.0228
 -14.250  -1.1162   0.04617   0.04189  -0.0510   1.0000   0.0230
 -14.000  -1.1178   0.04405   0.03967  -0.0500   1.0000   0.0233
 -13.750  -1.1192   0.04207   0.03757  -0.0486   1.0000   0.0236
 -13.500  -1.1182   0.04035   0.03575  -0.0470   1.0000   0.0240
 -13.250  -1.1181   0.03863   0.03389  -0.0450   1.0000   0.0244
 -13.000  -1.1180   0.03696   0.03206  -0.0427   1.0000   0.0249
 -12.750  -1.1174   0.03547   0.03039  -0.0400   1.0000   0.0254
 -12.500  -1.1162   0.03420   0.02893  -0.0369   1.0000   0.0259
 -12.250  -1.1150   0.03333   0.02788  -0.0333   1.0000   0.0263
 -12.000  -1.1150   0.03132   0.02564  -0.0298   1.0000   0.0268
 -11.750  -1.1047   0.02962   0.02389  -0.0278   1.0000   0.0275
 -11.500  -1.0933   0.02874   0.02298  -0.0257   1.0000   0.0280
 -11.250  -1.0824   0.02797   0.02214  -0.0232   1.0000   0.0286
 -11.000  -1.0715   0.02719   0.02127  -0.0206   1.0000   0.0292
 -10.750  -1.0600   0.02645   0.02045  -0.0181   1.0000   0.0299
 -10.500  -1.0485   0.02576   0.01964  -0.0154   1.0000   0.0306
 -10.250  -1.0371   0.02516   0.01893  -0.0127   1.0000   0.0313
 -10.000  -1.0256   0.02472   0.01836  -0.0098   1.0000   0.0317
  -9.750  -1.0121   0.02286   0.01639  -0.0077   1.0000   0.0326
  -9.500  -0.9989   0.02196   0.01547  -0.0054   1.0000   0.0333
  -9.250  -0.9857   0.02140   0.01489  -0.0029   1.0000   0.0341
  -9.000  -0.9722   0.02090   0.01436  -0.0004   1.0000   0.0349
  -8.750  -0.9582   0.02039   0.01379   0.0020   1.0000   0.0357
  -8.500  -0.9438   0.01984   0.01318   0.0043   1.0000   0.0365
  -8.250  -0.9289   0.01931   0.01258   0.0066   1.0000   0.0372
  -8.000  -0.9135   0.01887   0.01207   0.0088   1.0000   0.0378
  -7.750  -0.8988   0.01819   0.01133   0.0111   1.0000   0.0385
  -7.500  -0.8739   0.01719   0.01032   0.0110   0.9988   0.0400
  -7.250  -0.8430   0.01660   0.00972   0.0099   0.9969   0.0411
  -7.000  -0.8110   0.01609   0.00918   0.0086   0.9951   0.0424
  -6.750  -0.7783   0.01564   0.00869   0.0072   0.9935   0.0439
  -6.500  -0.7480   0.01525   0.00825   0.0064   0.9909   0.0452
  -6.250  -0.7188   0.01454   0.00752   0.0057   0.9882   0.0470
  -6.000  -0.6868   0.01404   0.00704   0.0044   0.9860   0.0494
  -5.750  -0.6530   0.01368   0.00666   0.0029   0.9843   0.0519
  -5.500  -0.6184   0.01329   0.00626   0.0011   0.9829   0.0555
  -5.250  -0.5914   0.01288   0.00589   0.0011   0.9787   0.0610
  -5.000  -0.5603   0.01245   0.00552   0.0001   0.9757   0.0708
  -4.750  -0.5272   0.01202   0.00517  -0.0013   0.9735   0.0893
  -4.500  -0.4932   0.01157   0.00486  -0.0030   0.9718   0.1158
  -4.250  -0.4586   0.01107   0.00459  -0.0049   0.9705   0.1569
  -4.000  -0.4335   0.01063   0.00435  -0.0046   0.9655   0.2023
  -3.750  -0.4036   0.01008   0.00408  -0.0054   0.9621   0.2647
  -3.500  -0.3741   0.00931   0.00377  -0.0064   0.9595   0.3691
  -3.250  -0.3462   0.00851   0.00349  -0.0068   0.9571   0.4922
  -3.000  -0.3249   0.00799   0.00334  -0.0056   0.9516   0.5807
  -2.750  -0.3003   0.00761   0.00324  -0.0048   0.9466   0.6505
  -2.500  -0.2716   0.00735   0.00315  -0.0048   0.9432   0.7028
  -2.250  -0.2413   0.00716   0.00310  -0.0051   0.9406   0.7413
  -2.000  -0.2188   0.00709   0.00308  -0.0037   0.9332   0.7670
  -1.750  -0.1898   0.00698   0.00301  -0.0037   0.9289   0.7844
  -1.500  -0.1595   0.00689   0.00294  -0.0039   0.9254   0.8003
  -1.250  -0.1352   0.00686   0.00296  -0.0029   0.9182   0.8169
  -1.000  -0.1072   0.00680   0.00293  -0.0026   0.9130   0.8331
  -0.750  -0.0794   0.00678   0.00292  -0.0022   0.9081   0.8477
  -0.500  -0.0544   0.00678   0.00295  -0.0013   0.9005   0.8618
  -0.250  -0.0258   0.00679   0.00299  -0.0009   0.8948   0.8742
   0.000   0.0000   0.00682   0.00304   0.0000   0.8850   0.8850
   0.250   0.0259   0.00679   0.00299   0.0009   0.8742   0.8948
   0.750   0.0794   0.00678   0.00292   0.0022   0.8477   0.9080
   1.000   0.1072   0.00680   0.00293   0.0026   0.8331   0.9130
   1.250   0.1352   0.00686   0.00296   0.0029   0.8169   0.9182
   1.500   0.1595   0.00689   0.00294   0.0039   0.8004   0.9254
   1.750   0.1898   0.00698   0.00301   0.0037   0.7844   0.9289
   2.000   0.2188   0.00708   0.00308   0.0037   0.7670   0.9332
   2.250   0.2413   0.00716   0.00310   0.0051   0.7415   0.9406
   2.500   0.2716   0.00735   0.00315   0.0048   0.7027   0.9432
   2.750   0.3002   0.00761   0.00324   0.0048   0.6503   0.9466
   3.000   0.3249   0.00799   0.00334   0.0056   0.5809   0.9516
   3.250   0.3462   0.00851   0.00349   0.0069   0.4920   0.9571
   3.500   0.3741   0.00930   0.00377   0.0064   0.3694   0.9595
   3.750   0.4037   0.01008   0.00408   0.0054   0.2648   0.9621
   4.000   0.4334   0.01063   0.00435   0.0046   0.2022   0.9655
   4.250   0.4586   0.01107   0.00459   0.0048   0.1569   0.9705
   4.500   0.4933   0.01157   0.00486   0.0030   0.1158   0.9718
   4.750   0.5272   0.01201   0.00517   0.0013   0.0893   0.9735
   5.000   0.5603   0.01245   0.00551  -0.0001   0.0708   0.9757
   5.250   0.5914   0.01288   0.00589  -0.0011   0.0610   0.9787
   5.500   0.6184   0.01329   0.00626  -0.0012   0.0554   0.9829
   5.750   0.6530   0.01368   0.00666  -0.0029   0.0519   0.9843
   6.000   0.6868   0.01404   0.00704  -0.0044   0.0493   0.9860
   6.250   0.7188   0.01454   0.00752  -0.0057   0.0470   0.9882
   6.500   0.7481   0.01524   0.00825  -0.0064   0.0452   0.9909
   6.750   0.7783   0.01564   0.00869  -0.0072   0.0439   0.9936
   7.000   0.8111   0.01609   0.00918  -0.0087   0.0424   0.9951
   7.250   0.8431   0.01660   0.00972  -0.0099   0.0411   0.9969
   7.500   0.8741   0.01719   0.01031  -0.0111   0.0399   0.9988
   7.750   0.8987   0.01818   0.01132  -0.0110   0.0385   1.0000
   8.000   0.9133   0.01887   0.01207  -0.0088   0.0378   1.0000
   8.250   0.9288   0.01931   0.01258  -0.0066   0.0372   1.0000
   8.500   0.9436   0.01984   0.01317  -0.0043   0.0365   1.0000
   8.750   0.9581   0.02038   0.01378  -0.0019   0.0358   1.0000
   9.000   0.9721   0.02090   0.01435   0.0005   0.0349   1.0000
   9.250   0.9856   0.02139   0.01488   0.0029   0.0341   1.0000
   9.500   0.9987   0.02195   0.01546   0.0054   0.0333   1.0000
   9.750   1.0120   0.02286   0.01638   0.0078   0.0326   1.0000
  10.000   1.0255   0.02472   0.01835   0.0098   0.0317   1.0000
  10.250   1.0370   0.02516   0.01892   0.0127   0.0313   1.0000
  10.500   1.0485   0.02576   0.01965   0.0154   0.0306   1.0000
  10.750   1.0600   0.02645   0.02044   0.0181   0.0299   1.0000
  11.000   1.0715   0.02720   0.02128   0.0206   0.0292   1.0000
  11.250   1.0825   0.02796   0.02213   0.0232   0.0286   1.0000
  11.500   1.0935   0.02875   0.02298   0.0256   0.0280   1.0000
  11.750   1.1050   0.02963   0.02390   0.0278   0.0275   1.0000
  12.000   1.1154   0.03133   0.02565   0.0297   0.0268   1.0000
  12.250   1.1154   0.03333   0.02789   0.0332   0.0263   1.0000
  12.500   1.1168   0.03422   0.02896   0.0368   0.0259   1.0000
  12.750   1.1180   0.03548   0.03040   0.0399   0.0254   1.0000
  13.000   1.1187   0.03700   0.03210   0.0425   0.0249   1.0000
  13.250   1.1189   0.03864   0.03391   0.0449   0.0244   1.0000
  13.500   1.1192   0.04036   0.03576   0.0469   0.0240   1.0000
  13.750   1.1204   0.04205   0.03755   0.0484   0.0236   1.0000
  14.000   1.1190   0.04405   0.03967   0.0498   0.0233   1.0000
  14.250   1.1177   0.04613   0.04185   0.0507   0.0230   1.0000
  14.500   1.1151   0.04852   0.04433   0.0513   0.0228   1.0000
  14.750   1.1104   0.05134   0.04725   0.0516   0.0225   1.0000
  15.000   1.1008   0.05498   0.05101   0.0513   0.0223   1.0000
  15.250   1.0814   0.06015   0.05636   0.0500   0.0221   1.0000
  15.500   1.0554   0.06673   0.06315   0.0473   0.0221   1.0000
  15.750   1.0285   0.07430   0.07093   0.0429   0.0221   1.0000
  16.000   0.9995   0.08335   0.08021   0.0368   0.0221   1.0000
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