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NACA 63A210 (naca63a210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63A210 (naca63a210-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.44 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca63a210-il-1000000-n5.txt
Download as CSV file: xf-naca63a210-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63A210                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9660   0.08120   0.07798  -0.0158   0.4369   0.0043
 -14.000  -1.0470   0.05614   0.05258  -0.0341   0.4370   0.0040
 -13.750  -1.0740   0.04779   0.04402  -0.0408   0.4371   0.0040
 -13.500  -1.0913   0.04232   0.03834  -0.0442   0.4371   0.0040
 -13.250  -1.1011   0.03852   0.03435  -0.0455   0.4372   0.0040
 -13.000  -1.1047   0.03579   0.03143  -0.0451   0.4372   0.0041
 -12.750  -1.1129   0.03299   0.02838  -0.0431   0.4372   0.0041
 -12.500  -1.1094   0.03052   0.02565  -0.0419   0.4372   0.0043
 -12.250  -1.0974   0.02887   0.02383  -0.0410   0.4373   0.0045
 -12.000  -1.0810   0.02770   0.02253  -0.0404   0.4373   0.0046
 -11.750  -1.0625   0.02673   0.02144  -0.0398   0.4374   0.0048
 -11.500  -1.0427   0.02590   0.02051  -0.0394   0.4374   0.0049
 -11.250  -1.0221   0.02511   0.01962  -0.0389   0.4375   0.0051
 -11.000  -1.0012   0.02432   0.01870  -0.0385   0.4376   0.0052
 -10.750  -0.9799   0.02352   0.01778  -0.0380   0.4376   0.0054
 -10.500  -0.9583   0.02272   0.01686  -0.0376   0.4377   0.0056
 -10.250  -0.9360   0.02201   0.01603  -0.0372   0.4377   0.0059
 -10.000  -0.9131   0.02135   0.01526  -0.0369   0.4378   0.0061
  -9.750  -0.8898   0.02074   0.01455  -0.0366   0.4379   0.0063
  -9.500  -0.8660   0.02017   0.01387  -0.0363   0.4380   0.0065
  -9.250  -0.8420   0.01962   0.01322  -0.0360   0.4380   0.0066
  -9.000  -0.8204   0.01853   0.01198  -0.0355   0.4381   0.0069
  -8.750  -0.7962   0.01794   0.01130  -0.0352   0.4382   0.0072
  -8.500  -0.7712   0.01752   0.01082  -0.0350   0.4383   0.0075
  -8.250  -0.7459   0.01713   0.01037  -0.0348   0.4383   0.0078
  -8.000  -0.7206   0.01672   0.00990  -0.0346   0.4384   0.0082
  -7.750  -0.6952   0.01630   0.00941  -0.0344   0.4385   0.0086
  -7.500  -0.6696   0.01592   0.00897  -0.0343   0.4386   0.0090
  -7.250  -0.6437   0.01559   0.00857  -0.0341   0.4387   0.0094
  -7.000  -0.6176   0.01529   0.00821  -0.0340   0.4388   0.0097
  -6.750  -0.5915   0.01496   0.00781  -0.0338   0.4389   0.0099
  -6.500  -0.5664   0.01442   0.00718  -0.0335   0.4390   0.0103
  -6.250  -0.5412   0.01388   0.00656  -0.0332   0.4391   0.0110
  -6.000  -0.5150   0.01354   0.00619  -0.0331   0.4392   0.0116
  -5.750  -0.4885   0.01327   0.00587  -0.0330   0.4393   0.0121
  -5.500  -0.4619   0.01302   0.00559  -0.0329   0.4393   0.0127
  -5.250  -0.4350   0.01280   0.00533  -0.0328   0.4391   0.0134
  -5.000  -0.4081   0.01259   0.00508  -0.0328   0.4388   0.0140
  -4.750  -0.3811   0.01238   0.00481  -0.0327   0.4385   0.0144
  -4.500  -0.3540   0.01218   0.00458  -0.0326   0.4383   0.0147
  -4.250  -0.3270   0.01194   0.00429  -0.0325   0.4381   0.0161
  -4.000  -0.2998   0.01174   0.00409  -0.0325   0.4379   0.0181
  -3.750  -0.2725   0.01159   0.00393  -0.0325   0.4376   0.0208
  -3.500  -0.2452   0.01141   0.00376  -0.0324   0.4375   0.0269
  -3.250  -0.2177   0.01128   0.00363  -0.0324   0.4375   0.0338
  -3.000  -0.1903   0.01113   0.00351  -0.0324   0.4375   0.0433
  -2.750  -0.1629   0.01097   0.00340  -0.0325   0.4375   0.0586
  -2.500  -0.1357   0.01077   0.00328  -0.0325   0.4375   0.0865
  -2.250  -0.1088   0.01049   0.00317  -0.0325   0.4375   0.1345
  -2.000  -0.0822   0.01018   0.00306  -0.0324   0.4375   0.1977
  -1.750  -0.0568   0.00961   0.00292  -0.0324   0.4373   0.3240
  -1.500  -0.0308   0.00921   0.00284  -0.0323   0.4370   0.4224
  -1.250  -0.0041   0.00897   0.00282  -0.0322   0.4365   0.4912
  -1.000   0.0229   0.00879   0.00282  -0.0322   0.4361   0.5485
  -0.750   0.0502   0.00868   0.00284  -0.0321   0.4356   0.5909
  -0.500   0.0778   0.00862   0.00285  -0.0321   0.4354   0.6172
  -0.250   0.1056   0.00859   0.00287  -0.0321   0.4352   0.6390
   0.000   0.1336   0.00857   0.00290  -0.0322   0.4349   0.6555
   0.250   0.1616   0.00857   0.00293  -0.0322   0.4348   0.6673
   0.500   0.1898   0.00858   0.00296  -0.0323   0.4346   0.6784
   0.750   0.2177   0.00858   0.00301  -0.0323   0.4336   0.6893
   1.000   0.2457   0.00860   0.00306  -0.0323   0.4314   0.6995
   1.250   0.2737   0.00863   0.00313  -0.0324   0.4293   0.7101
   1.500   0.3016   0.00865   0.00319  -0.0324   0.4268   0.7206
   1.750   0.3295   0.00868   0.00326  -0.0324   0.4235   0.7307
   2.000   0.3574   0.00872   0.00334  -0.0325   0.4198   0.7411
   2.250   0.3852   0.00871   0.00339  -0.0324   0.4127   0.7513
   2.500   0.4133   0.00872   0.00347  -0.0324   0.3923   0.7615
   2.750   0.4403   0.00886   0.00332  -0.0323   0.3297   0.7723
   3.000   0.4667   0.00890   0.00303  -0.0321   0.2423   0.7831
   3.250   0.4927   0.00909   0.00299  -0.0320   0.1688   0.7947
   3.500   0.5186   0.00931   0.00303  -0.0318   0.1136   0.8080
   3.750   0.5441   0.00955   0.00316  -0.0315   0.0699   0.8240
   4.000   0.5698   0.00969   0.00332  -0.0311   0.0503   0.8458
   4.250   0.5945   0.00979   0.00350  -0.0305   0.0381   0.8819
   4.500   0.6197   0.00987   0.00369  -0.0299   0.0292   0.9368
   4.750   0.6558   0.01009   0.00390  -0.0319   0.0224   0.9767
   5.000   0.6899   0.01032   0.00413  -0.0335   0.0178   0.9972
   5.250   0.7168   0.01058   0.00438  -0.0334   0.0147   1.0000
   5.500   0.7424   0.01083   0.00464  -0.0331   0.0133   1.0000
   5.750   0.7681   0.01108   0.00491  -0.0328   0.0126   1.0000
   6.000   0.7936   0.01135   0.00521  -0.0324   0.0120   1.0000
   6.250   0.8188   0.01165   0.00553  -0.0321   0.0114   1.0000
   6.500   0.8439   0.01198   0.00589  -0.0317   0.0109   1.0000
   6.750   0.8687   0.01234   0.00629  -0.0313   0.0104   1.0000
   7.000   0.8929   0.01279   0.00678  -0.0307   0.0098   1.0000
   7.250   0.9161   0.01336   0.00742  -0.0300   0.0094   1.0000
   7.500   0.9392   0.01392   0.00806  -0.0293   0.0092   1.0000
   7.750   0.9630   0.01437   0.00858  -0.0288   0.0091   1.0000
   8.000   0.9869   0.01482   0.00908  -0.0283   0.0090   1.0000
   8.250   1.0108   0.01525   0.00955  -0.0278   0.0088   1.0000
   8.500   1.0345   0.01569   0.01005  -0.0273   0.0085   1.0000
   8.750   1.0576   0.01621   0.01063  -0.0268   0.0083   1.0000
   9.000   1.0801   0.01677   0.01125  -0.0261   0.0081   1.0000
   9.250   1.1024   0.01735   0.01190  -0.0254   0.0079   1.0000
   9.500   1.1244   0.01794   0.01257  -0.0247   0.0076   1.0000
   9.750   1.1463   0.01853   0.01323  -0.0240   0.0074   1.0000
  10.000   1.1682   0.01912   0.01388  -0.0234   0.0071   1.0000
  10.250   1.1897   0.01972   0.01453  -0.0227   0.0069   1.0000
  10.500   1.2108   0.02034   0.01521  -0.0220   0.0067   1.0000
  10.750   1.2307   0.02108   0.01600  -0.0211   0.0064   1.0000
  11.000   1.2446   0.02243   0.01749  -0.0195   0.0060   1.0000
  11.250   1.2625   0.02329   0.01844  -0.0184   0.0059   1.0000
  11.500   1.2823   0.02392   0.01917  -0.0175   0.0058   1.0000
  11.750   1.3001   0.02470   0.02005  -0.0165   0.0057   1.0000
  12.000   1.3167   0.02557   0.02101  -0.0153   0.0056   1.0000
  12.250   1.3319   0.02650   0.02206  -0.0140   0.0054   1.0000
  12.500   1.3454   0.02752   0.02318  -0.0125   0.0052   1.0000
  12.750   1.3560   0.02856   0.02433  -0.0106   0.0051   1.0000
  13.000   1.3643   0.02969   0.02558  -0.0085   0.0049   1.0000
  13.250   1.3711   0.03093   0.02692  -0.0065   0.0048   1.0000
  13.500   1.3770   0.03227   0.02837  -0.0047   0.0047   1.0000
  13.750   1.3818   0.03377   0.02997  -0.0031   0.0046   1.0000
  14.000   1.3856   0.03544   0.03175  -0.0018   0.0045   1.0000
  14.250   1.3883   0.03735   0.03376  -0.0008   0.0044   1.0000
  14.500   1.3893   0.03959   0.03613  -0.0002   0.0043   1.0000
  14.750   1.3892   0.04217   0.03882  -0.0001   0.0042   1.0000
  15.000   1.3874   0.04525   0.04202  -0.0006   0.0041   1.0000
  15.250   1.3815   0.04926   0.04616  -0.0022   0.0041   1.0000
  15.500   1.3736   0.05405   0.05109  -0.0047   0.0040   1.0000
  15.750   1.3616   0.05936   0.05653  -0.0073   0.0040   1.0000
  16.000   1.3438   0.06523   0.06253  -0.0098   0.0040   1.0000
  16.250   1.3237   0.07221   0.06966  -0.0133   0.0040   1.0000
  16.500   1.2959   0.08056   0.07817  -0.0176   0.0040   1.0000
  16.750   1.2599   0.09129   0.08910  -0.0233   0.0040   1.0000
  17.000   1.2006   0.10790   0.10595  -0.0323   0.0041   1.0000
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