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NACA 64A210 (naca64a210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64A210 (naca64a210-il)
Reynolds number: 1,000,000
Max Cl/Cd: 73.18 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca64a210-il-1000000-n5.txt
Download as CSV file: xf-naca64a210-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64A210                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -1.0383   0.04718   0.04513  -0.0468   1.0000   0.0040
 -13.500  -1.0663   0.04041   0.03809  -0.0506   1.0000   0.0040
 -13.250  -1.0797   0.03653   0.03399  -0.0510   1.0000   0.0041
 -13.000  -1.0857   0.03383   0.03109  -0.0497   1.0000   0.0041
 -12.750  -1.0825   0.03152   0.02859  -0.0486   1.0000   0.0042
 -12.500  -1.0744   0.02951   0.02639  -0.0477   1.0000   0.0043
 -12.250  -1.0633   0.02772   0.02441  -0.0468   1.0000   0.0044
 -12.000  -1.0500   0.02612   0.02263  -0.0459   1.0000   0.0046
 -11.750  -1.0351   0.02466   0.02100  -0.0450   1.0000   0.0047
 -11.500  -1.0187   0.02338   0.01956  -0.0441   1.0000   0.0048
 -11.250  -1.0011   0.02227   0.01830  -0.0433   1.0000   0.0050
 -11.000  -0.9828   0.02130   0.01718  -0.0424   1.0000   0.0051
 -10.750  -0.9643   0.02042   0.01619  -0.0413   1.0000   0.0052
 -10.500  -0.9488   0.01927   0.01489  -0.0399   1.0000   0.0055
 -10.250  -0.9283   0.01863   0.01420  -0.0391   0.9995   0.0057
 -10.000  -0.8990   0.01803   0.01353  -0.0401   0.9970   0.0059
  -9.750  -0.8691   0.01740   0.01282  -0.0412   0.9946   0.0062
  -9.500  -0.8408   0.01676   0.01210  -0.0419   0.9909   0.0065
  -9.250  -0.8115   0.01611   0.01135  -0.0428   0.9873   0.0068
  -9.000  -0.7828   0.01546   0.01059  -0.0436   0.9831   0.0071
  -8.750  -0.7542   0.01487   0.00991  -0.0443   0.9782   0.0074
  -8.500  -0.7254   0.01436   0.00932  -0.0449   0.9731   0.0076
  -8.250  -0.6989   0.01363   0.00849  -0.0451   0.9663   0.0080
  -8.000  -0.6722   0.01314   0.00796  -0.0453   0.9595   0.0085
  -7.750  -0.6454   0.01284   0.00761  -0.0453   0.9521   0.0089
  -7.500  -0.6193   0.01253   0.00725  -0.0452   0.9444   0.0094
  -7.250  -0.5938   0.01215   0.00681  -0.0449   0.9363   0.0098
  -7.000  -0.5683   0.01177   0.00635  -0.0446   0.9281   0.0102
  -6.750  -0.5428   0.01142   0.00592  -0.0443   0.9204   0.0106
  -6.500  -0.5169   0.01110   0.00554  -0.0441   0.9123   0.0109
  -6.250  -0.4909   0.01083   0.00519  -0.0439   0.9048   0.0111
  -6.000  -0.4660   0.01026   0.00454  -0.0435   0.8967   0.0120
  -5.750  -0.4399   0.00994   0.00417  -0.0433   0.8894   0.0126
  -5.500  -0.4135   0.00967   0.00385  -0.0431   0.8818   0.0131
  -5.250  -0.3869   0.00942   0.00354  -0.0430   0.8746   0.0137
  -5.000  -0.3601   0.00920   0.00327  -0.0429   0.8670   0.0145
  -4.750  -0.3331   0.00900   0.00302  -0.0428   0.8599   0.0152
  -4.500  -0.3061   0.00881   0.00278  -0.0427   0.8521   0.0156
  -4.250  -0.2792   0.00856   0.00246  -0.0426   0.8447   0.0170
  -4.000  -0.2522   0.00837   0.00225  -0.0425   0.8365   0.0189
  -3.750  -0.2249   0.00821   0.00207  -0.0425   0.8284   0.0210
  -3.500  -0.1976   0.00807   0.00189  -0.0424   0.8197   0.0243
  -3.250  -0.1703   0.00792   0.00173  -0.0424   0.8101   0.0301
  -3.000  -0.1431   0.00776   0.00159  -0.0423   0.8009   0.0401
  -2.750  -0.1160   0.00761   0.00145  -0.0423   0.7911   0.0552
  -2.500  -0.0889   0.00743   0.00133  -0.0422   0.7809   0.0793
  -2.250  -0.0621   0.00720   0.00119  -0.0422   0.7716   0.1211
  -2.000  -0.0363   0.00679   0.00105  -0.0421   0.7626   0.2095
  -1.750  -0.0115   0.00618   0.00088  -0.0419   0.7531   0.3483
  -1.500   0.0137   0.00574   0.00079  -0.0417   0.7441   0.4646
  -1.250   0.0406   0.00559   0.00075  -0.0416   0.7351   0.5152
  -1.000   0.0674   0.00543   0.00074  -0.0415   0.7265   0.5692
  -0.750   0.0942   0.00532   0.00074  -0.0413   0.7179   0.6160
  -0.500   0.1216   0.00527   0.00074  -0.0412   0.7086   0.6419
  -0.250   0.1493   0.00525   0.00075  -0.0412   0.7000   0.6594
   0.250   0.2051   0.00526   0.00076  -0.0413   0.6829   0.6813
   0.500   0.2330   0.00529   0.00078  -0.0413   0.6744   0.6898
   0.750   0.2609   0.00531   0.00080  -0.0414   0.6653   0.6992
   1.000   0.2885   0.00535   0.00084  -0.0414   0.6525   0.7082
   1.500   0.3429   0.00550   0.00091  -0.0412   0.6140   0.7266
   1.750   0.3696   0.00562   0.00097  -0.0410   0.5856   0.7360
   2.000   0.3956   0.00583   0.00104  -0.0407   0.5439   0.7460
   2.250   0.4212   0.00607   0.00113  -0.0404   0.4945   0.7554
   2.500   0.4456   0.00647   0.00127  -0.0399   0.4199   0.7650
   3.000   0.4907   0.00782   0.00183  -0.0386   0.2063   0.7864
   3.250   0.5137   0.00845   0.00211  -0.0380   0.1162   0.7972
   3.500   0.5389   0.00878   0.00233  -0.0377   0.0776   0.8092
   3.750   0.5646   0.00900   0.00253  -0.0374   0.0566   0.8240
   4.000   0.5899   0.00920   0.00273  -0.0371   0.0411   0.8435
   4.250   0.6147   0.00934   0.00293  -0.0365   0.0321   0.8733
   4.500   0.6385   0.00943   0.00315  -0.0356   0.0262   0.9212
   4.750   0.6708   0.00965   0.00341  -0.0367   0.0204   0.9675
   5.000   0.7057   0.00993   0.00367  -0.0386   0.0169   0.9936
   5.250   0.7335   0.01023   0.00397  -0.0388   0.0146   1.0000
   5.500   0.7587   0.01048   0.00424  -0.0384   0.0138   1.0000
   5.750   0.7839   0.01076   0.00454  -0.0380   0.0130   1.0000
   6.000   0.8088   0.01106   0.00485  -0.0376   0.0123   1.0000
   6.250   0.8335   0.01139   0.00520  -0.0372   0.0118   1.0000
   6.500   0.8580   0.01176   0.00559  -0.0368   0.0113   1.0000
   6.750   0.8819   0.01219   0.00607  -0.0362   0.0109   1.0000
   7.000   0.9050   0.01273   0.00666  -0.0355   0.0105   1.0000
   7.250   0.9281   0.01326   0.00725  -0.0349   0.0102   1.0000
   7.500   0.9523   0.01363   0.00766  -0.0344   0.0101   1.0000
   7.750   0.9763   0.01402   0.00809  -0.0340   0.0098   1.0000
   8.000   0.9997   0.01448   0.00860  -0.0334   0.0096   1.0000
   8.250   1.0228   0.01498   0.00916  -0.0328   0.0093   1.0000
   8.500   1.0455   0.01550   0.00973  -0.0322   0.0090   1.0000
   8.750   1.0682   0.01601   0.01029  -0.0316   0.0087   1.0000
   9.000   1.0911   0.01648   0.01080  -0.0310   0.0083   1.0000
   9.250   1.1140   0.01693   0.01128  -0.0305   0.0080   1.0000
   9.500   1.1358   0.01748   0.01187  -0.0298   0.0077   1.0000
   9.750   1.1558   0.01825   0.01272  -0.0289   0.0074   1.0000
  10.000   1.1720   0.01946   0.01405  -0.0274   0.0070   1.0000
  10.250   1.1928   0.02005   0.01471  -0.0266   0.0069   1.0000
  10.500   1.2131   0.02067   0.01542  -0.0258   0.0068   1.0000
  10.750   1.2325   0.02136   0.01620  -0.0248   0.0067   1.0000
  11.000   1.2514   0.02206   0.01698  -0.0238   0.0065   1.0000
  11.250   1.2698   0.02276   0.01776  -0.0228   0.0062   1.0000
  11.500   1.2875   0.02344   0.01852  -0.0217   0.0060   1.0000
  11.750   1.3038   0.02410   0.01927  -0.0203   0.0057   1.0000
  12.000   1.3191   0.02478   0.02002  -0.0188   0.0055   1.0000
  12.250   1.3336   0.02550   0.02080  -0.0174   0.0053   1.0000
  12.500   1.3470   0.02629   0.02166  -0.0158   0.0052   1.0000
  12.750   1.3596   0.02715   0.02259  -0.0143   0.0051   1.0000
  13.000   1.3704   0.02817   0.02368  -0.0127   0.0049   1.0000
  13.250   1.3781   0.02948   0.02509  -0.0110   0.0048   1.0000
  13.500   1.3823   0.03115   0.02690  -0.0091   0.0046   1.0000
  13.750   1.3884   0.03270   0.02857  -0.0077   0.0046   1.0000
  14.000   1.3934   0.03438   0.03039  -0.0063   0.0045   1.0000
  14.250   1.3965   0.03633   0.03249  -0.0051   0.0044   1.0000
  14.500   1.3985   0.03844   0.03473  -0.0041   0.0043   1.0000
  14.750   1.3985   0.04086   0.03729  -0.0033   0.0043   1.0000
  15.000   1.3964   0.04361   0.04019  -0.0028   0.0042   1.0000
  15.250   1.3930   0.04667   0.04339  -0.0026   0.0041   1.0000
  15.500   1.3880   0.05006   0.04692  -0.0029   0.0040   1.0000
  15.750   1.3801   0.05400   0.05101  -0.0035   0.0040   1.0000
  16.000   1.3691   0.05861   0.05578  -0.0048   0.0039   1.0000
  16.250   1.3560   0.06377   0.06109  -0.0066   0.0039   1.0000
  16.500   1.3372   0.07027   0.06776  -0.0094   0.0039   1.0000
  16.750   1.3129   0.07823   0.07589  -0.0134   0.0039   1.0000
  17.000   1.2798   0.08874   0.08661  -0.0193   0.0039   1.0000
  17.250   1.2145   0.10776   0.10592  -0.0303   0.0041   1.0000
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