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NACA 63 (naca633418-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: NACA 63 (naca633418-il)
Reynolds number: 200,000
Max Cl/Cd: 69.31 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633418-il-200000.txt
Download as CSV file: xf-naca633418-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63                                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6517   0.10280   0.09862  -0.0575   1.0000   0.0490
 -15.750  -0.6982   0.09056   0.08622  -0.0650   1.0000   0.0484
 -15.500  -0.7383   0.08088   0.07635  -0.0708   1.0000   0.0477
 -15.250  -0.7759   0.07285   0.06809  -0.0753   1.0000   0.0474
 -15.000  -0.8048   0.06664   0.06166  -0.0783   1.0000   0.0472
 -14.750  -0.8287   0.06146   0.05626  -0.0803   1.0000   0.0472
 -14.500  -0.8479   0.05704   0.05161  -0.0814   1.0000   0.0472
 -14.250  -0.8627   0.05333   0.04769  -0.0819   1.0000   0.0474
 -14.000  -0.8737   0.05006   0.04421  -0.0820   1.0000   0.0476
 -13.750  -0.8832   0.04718   0.04111  -0.0816   1.0000   0.0481
 -13.500  -0.8889   0.04469   0.03840  -0.0809   1.0000   0.0484
 -13.250  -0.8945   0.04248   0.03598  -0.0797   1.0000   0.0489
 -13.000  -0.9007   0.04067   0.03395  -0.0781   1.0000   0.0493
 -12.750  -0.8796   0.03862   0.03193  -0.0778   1.0000   0.0506
 -12.500  -0.8690   0.03743   0.03077  -0.0767   1.0000   0.0517
 -12.250  -0.8629   0.03623   0.02953  -0.0750   1.0000   0.0527
 -12.000  -0.8621   0.03526   0.02852  -0.0725   1.0000   0.0537
 -11.750  -0.8904   0.03523   0.02850  -0.0656   0.9991   0.0538
 -11.500  -0.8568   0.03343   0.02647  -0.0688   0.9921   0.0556
 -11.250  -0.8207   0.03164   0.02457  -0.0711   0.9869   0.0576
 -11.000  -0.7824   0.03036   0.02336  -0.0741   0.9823   0.0603
 -10.750  -0.7483   0.02910   0.02199  -0.0768   0.9748   0.0633
 -10.500  -0.7097   0.02768   0.02054  -0.0794   0.9705   0.0666
 -10.250  -0.6745   0.02655   0.01945  -0.0819   0.9634   0.0701
 -10.000  -0.6390   0.02547   0.01821  -0.0849   0.9556   0.0743
  -9.750  -0.6080   0.02423   0.01711  -0.0866   0.9467   0.0793
  -9.500  -0.5762   0.02326   0.01601  -0.0887   0.9376   0.0849
  -9.250  -0.5587   0.02217   0.01502  -0.0884   0.9242   0.0904
  -9.000  -0.5430   0.02150   0.01423  -0.0875   0.9113   0.0962
  -8.750  -0.5359   0.02064   0.01343  -0.0853   0.8990   0.1023
  -8.500  -0.5234   0.02001   0.01273  -0.0836   0.8880   0.1105
  -8.250  -0.5133   0.01929   0.01205  -0.0817   0.8774   0.1202
  -8.000  -0.5011   0.01852   0.01131  -0.0800   0.8685   0.1341
  -7.750  -0.4889   0.01777   0.01065  -0.0783   0.8586   0.1540
  -7.500  -0.4759   0.01685   0.00988  -0.0769   0.8509   0.1861
  -7.250  -0.4632   0.01587   0.00922  -0.0756   0.8421   0.2381
  -7.000  -0.4475   0.01495   0.00864  -0.0746   0.8347   0.3089
  -6.750  -0.4269   0.01449   0.00842  -0.0739   0.8278   0.3726
  -6.500  -0.4028   0.01435   0.00835  -0.0734   0.8202   0.4146
  -6.250  -0.3765   0.01433   0.00829  -0.0731   0.8147   0.4433
  -6.000  -0.3504   0.01440   0.00834  -0.0728   0.8076   0.4653
  -5.750  -0.3236   0.01448   0.00835  -0.0724   0.8008   0.4836
  -5.500  -0.2958   0.01459   0.00838  -0.0721   0.7957   0.4991
  -5.250  -0.2691   0.01473   0.00849  -0.0719   0.7887   0.5127
  -5.000  -0.2417   0.01482   0.00849  -0.0717   0.7824   0.5259
  -4.750  -0.2135   0.01497   0.00859  -0.0713   0.7776   0.5368
  -4.500  -0.1866   0.01512   0.00872  -0.0710   0.7707   0.5472
  -4.250  -0.1589   0.01525   0.00877  -0.0709   0.7647   0.5586
  -4.000  -0.1308   0.01540   0.00892  -0.0704   0.7599   0.5671
  -3.750  -0.1034   0.01553   0.00894  -0.0704   0.7537   0.5781
  -3.500  -0.0763   0.01569   0.00917  -0.0698   0.7475   0.5847
  -3.250  -0.0476   0.01573   0.00911  -0.0698   0.7427   0.5935
  -3.000  -0.0199   0.01579   0.00914  -0.0696   0.7377   0.5997
  -2.750   0.0071   0.01588   0.00925  -0.0694   0.7312   0.6056
  -2.500   0.0361   0.01581   0.00904  -0.0697   0.7261   0.6134
  -2.250   0.0648   0.01582   0.00900  -0.0696   0.7220   0.6180
  -2.000   0.0912   0.01590   0.00915  -0.0693   0.7155   0.6231
  -1.750   0.1198   0.01587   0.00904  -0.0696   0.7102   0.6298
  -1.500   0.1488   0.01581   0.00890  -0.0698   0.7060   0.6350
  -1.250   0.1760   0.01588   0.00900  -0.0696   0.7007   0.6394
  -1.000   0.2036   0.01591   0.00902  -0.0697   0.6947   0.6451
  -0.750   0.2333   0.01583   0.00884  -0.0702   0.6902   0.6515
  -0.500   0.2620   0.01586   0.00884  -0.0702   0.6865   0.6554
  -0.250   0.2880   0.01596   0.00902  -0.0700   0.6805   0.6604
   0.000   0.3166   0.01596   0.00898  -0.0703   0.6751   0.6666
   0.250   0.3460   0.01590   0.00887  -0.0706   0.6709   0.6716
   0.500   0.3736   0.01601   0.00899  -0.0705   0.6667   0.6761
   0.750   0.4002   0.01611   0.00915  -0.0704   0.6609   0.6817
   1.000   0.4299   0.01609   0.00907  -0.0710   0.6561   0.6882
   1.250   0.4583   0.01610   0.00908  -0.0709   0.6522   0.6922
   1.500   0.4847   0.01625   0.00929  -0.0708   0.6472   0.6975
   1.750   0.5124   0.01633   0.00939  -0.0710   0.6417   0.7041
   2.000   0.5409   0.01633   0.00939  -0.0711   0.6372   0.7090
   2.250   0.5702   0.01639   0.00942  -0.0712   0.6336   0.7138
   2.500   0.5955   0.01657   0.00970  -0.0711   0.6277   0.7203
   2.750   0.6233   0.01662   0.00978  -0.0712   0.6224   0.7265
   3.000   0.6514   0.01665   0.00983  -0.0711   0.6183   0.7313
   3.250   0.6796   0.01677   0.00996  -0.0712   0.6137   0.7374
   3.500   0.7055   0.01691   0.01018  -0.0712   0.6076   0.7441
   3.750   0.7322   0.01695   0.01028  -0.0708   0.6027   0.7493
   4.000   0.7626   0.01699   0.01028  -0.0712   0.5987   0.7560
   4.250   0.7869   0.01718   0.01059  -0.0709   0.5924   0.7626
   4.500   0.8124   0.01724   0.01073  -0.0704   0.5867   0.7680
   4.750   0.8427   0.01724   0.01070  -0.0708   0.5822   0.7752
   5.000   0.8668   0.01740   0.01097  -0.0703   0.5758   0.7818
   5.250   0.8918   0.01741   0.01108  -0.0697   0.5691   0.7882
   5.500   0.9243   0.01734   0.01091  -0.0704   0.5636   0.7960
   5.750   0.9438   0.01743   0.01120  -0.0689   0.5553   0.8020
   6.000   0.9719   0.01735   0.01112  -0.0688   0.5487   0.8098
   6.250   0.9956   0.01740   0.01127  -0.0681   0.5409   0.8172
   6.500   1.0203   0.01728   0.01119  -0.0673   0.5323   0.8246
   6.750   1.0437   0.01721   0.01119  -0.0665   0.5220   0.8329
   7.000   1.0685   0.01701   0.01096  -0.0655   0.5121   0.8406
   7.250   1.0879   0.01702   0.01111  -0.0641   0.5007   0.8499
   7.500   1.1085   0.01699   0.01115  -0.0627   0.4910   0.8585
   7.750   1.1290   0.01698   0.01120  -0.0613   0.4801   0.8681
   8.000   1.1453   0.01703   0.01137  -0.0593   0.4683   0.8789
   8.250   1.1612   0.01705   0.01144  -0.0570   0.4560   0.8900
   8.500   1.1755   0.01708   0.01151  -0.0546   0.4423   0.9031
   8.750   1.1865   0.01715   0.01162  -0.0516   0.4271   0.9190
   9.000   1.1940   0.01724   0.01177  -0.0482   0.4103   0.9413
   9.250   1.2087   0.01744   0.01206  -0.0467   0.3876   1.0000
   9.500   1.2212   0.01812   0.01263  -0.0456   0.3614   1.0000
   9.750   1.2283   0.01909   0.01348  -0.0439   0.3310   1.0000
  10.000   1.2295   0.02042   0.01463  -0.0416   0.3000   1.0000
  10.250   1.2271   0.02207   0.01610  -0.0392   0.2697   1.0000
  10.500   1.2222   0.02401   0.01788  -0.0369   0.2404   1.0000
  10.750   1.2155   0.02624   0.01994  -0.0347   0.2127   1.0000
  11.000   1.2082   0.02870   0.02223  -0.0328   0.1870   1.0000
  11.250   1.2019   0.03125   0.02464  -0.0311   0.1639   1.0000
  11.500   1.1958   0.03391   0.02718  -0.0298   0.1447   1.0000
  11.750   1.1906   0.03663   0.02980  -0.0286   0.1293   1.0000
  12.000   1.1876   0.03926   0.03236  -0.0277   0.1168   1.0000
  12.250   1.1862   0.04186   0.03492  -0.0270   0.1067   1.0000
  12.500   1.1838   0.04461   0.03760  -0.0264   0.0992   1.0000
  12.750   1.1866   0.04699   0.04000  -0.0260   0.0921   1.0000
  13.000   1.1876   0.04959   0.04256  -0.0256   0.0865   1.0000
  13.250   1.1924   0.05188   0.04488  -0.0254   0.0814   1.0000
  13.500   1.1947   0.05439   0.04731  -0.0250   0.0773   1.0000
  13.750   1.2019   0.05653   0.04954  -0.0249   0.0733   1.0000
  14.000   1.2075   0.05883   0.05183  -0.0249   0.0699   1.0000
  14.250   1.2152   0.06086   0.05385  -0.0245   0.0668   1.0000
  14.500   1.2232   0.06300   0.05607  -0.0246   0.0639   1.0000
  14.750   1.2311   0.06512   0.05818  -0.0246   0.0613   1.0000
  15.000   1.2437   0.06661   0.05960  -0.0241   0.0589   1.0000
  15.250   1.2516   0.06888   0.06201  -0.0242   0.0568   1.0000
  15.500   1.2606   0.07098   0.06417  -0.0243   0.0548   1.0000
  15.750   1.2718   0.07276   0.06592  -0.0243   0.0530   1.0000
  16.000   1.2871   0.07411   0.06725  -0.0239   0.0511   1.0000
  16.250   1.2929   0.07672   0.07004  -0.0242   0.0498   1.0000
  16.500   1.3001   0.07918   0.07262  -0.0246   0.0484   1.0000
  16.750   1.3085   0.08145   0.07496  -0.0249   0.0471   1.0000
  17.000   1.3206   0.08323   0.07671  -0.0250   0.0458   1.0000
  17.250   1.3357   0.08484   0.07834  -0.0247   0.0444   1.0000
  17.500   1.3335   0.08859   0.08231  -0.0257   0.0436   1.0000
  17.750   1.3333   0.09215   0.08607  -0.0267   0.0428   1.0000
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