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NACA 63 (naca633418-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63 (naca633418-il)
Reynolds number: 500,000
Max Cl/Cd: 91.56 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633418-il-500000-n5.txt
Download as CSV file: xf-naca633418-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.9379   0.10794   0.10395  -0.0455   1.0000   0.0184
 -19.500  -0.9454   0.10294   0.09887  -0.0481   1.0000   0.0185
 -19.250  -0.9530   0.09800   0.09384  -0.0507   1.0000   0.0187
 -19.000  -0.9596   0.09335   0.08910  -0.0531   1.0000   0.0188
 -18.750  -0.9650   0.08894   0.08459  -0.0553   1.0000   0.0189
 -18.500  -0.9700   0.08466   0.08022  -0.0574   1.0000   0.0191
 -18.250  -0.9739   0.08059   0.07607  -0.0593   1.0000   0.0193
 -18.000  -0.9772   0.07675   0.07213  -0.0611   1.0000   0.0195
 -17.750  -0.9798   0.07306   0.06836  -0.0627   1.0000   0.0196
 -17.500  -0.9811   0.06961   0.06483  -0.0642   1.0000   0.0198
 -17.250  -0.9817   0.06632   0.06145  -0.0655   1.0000   0.0201
 -17.000  -0.9809   0.06329   0.05832  -0.0667   1.0000   0.0203
 -16.750  -0.9801   0.06030   0.05525  -0.0678   1.0000   0.0205
 -16.500  -0.9805   0.05726   0.05216  -0.0689   1.0000   0.0208
 -16.250  -0.9801   0.05440   0.04924  -0.0698   1.0000   0.0210
 -16.000  -0.9783   0.05174   0.04654  -0.0706   1.0000   0.0213
 -15.750  -0.9748   0.04932   0.04407  -0.0713   1.0000   0.0216
 -15.500  -0.9717   0.04694   0.04163  -0.0718   1.0000   0.0218
 -15.250  -0.9670   0.04479   0.03942  -0.0722   1.0000   0.0222
 -15.000  -0.9616   0.04277   0.03735  -0.0725   1.0000   0.0225
 -14.750  -0.9562   0.04083   0.03534  -0.0727   1.0000   0.0229
 -14.500  -0.9507   0.03899   0.03344  -0.0728   1.0000   0.0233
 -14.250  -0.9442   0.03728   0.03167  -0.0727   1.0000   0.0237
 -14.000  -0.9375   0.03564   0.02996  -0.0725   1.0000   0.0240
 -13.750  -0.9331   0.03385   0.02815  -0.0723   1.0000   0.0244
 -13.500  -0.9273   0.03224   0.02651  -0.0719   1.0000   0.0248
 -13.250  -0.9205   0.03076   0.02501  -0.0714   1.0000   0.0253
 -12.750  -0.8447   0.02750   0.02157  -0.0823   0.9336   0.0271
 -12.500  -0.8129   0.02623   0.02014  -0.0860   0.9060   0.0281
 -12.250  -0.8003   0.02503   0.01883  -0.0860   0.8820   0.0288
 -12.000  -0.7896   0.02405   0.01775  -0.0852   0.8643   0.0298
 -11.500  -0.7678   0.02225   0.01576  -0.0832   0.8380   0.0315
 -11.250  -0.7561   0.02143   0.01484  -0.0821   0.8276   0.0323
 -11.000  -0.7463   0.02052   0.01387  -0.0809   0.8170   0.0334
 -10.750  -0.7350   0.01972   0.01302  -0.0797   0.8081   0.0343
 -10.500  -0.7233   0.01898   0.01221  -0.0784   0.7993   0.0356
 -10.250  -0.7113   0.01831   0.01146  -0.0770   0.7914   0.0368
 -10.000  -0.7014   0.01765   0.01074  -0.0752   0.7830   0.0381
  -9.750  -0.6924   0.01710   0.01014  -0.0731   0.7756   0.0397
  -9.500  -0.6758   0.01660   0.00960  -0.0721   0.7686   0.0415
  -9.250  -0.6573   0.01618   0.00911  -0.0712   0.7619   0.0434
  -9.000  -0.6383   0.01572   0.00862  -0.0703   0.7556   0.0458
  -8.750  -0.6171   0.01533   0.00819  -0.0697   0.7488   0.0485
  -8.500  -0.5958   0.01494   0.00777  -0.0691   0.7427   0.0517
  -8.250  -0.5731   0.01458   0.00738  -0.0687   0.7372   0.0555
  -8.000  -0.5500   0.01420   0.00700  -0.0684   0.7309   0.0599
  -7.500  -0.5023   0.01352   0.00628  -0.0678   0.7191   0.0718
  -7.250  -0.4776   0.01318   0.00595  -0.0677   0.7132   0.0793
  -7.000  -0.4528   0.01285   0.00562  -0.0675   0.7074   0.0887
  -6.750  -0.4276   0.01251   0.00530  -0.0674   0.7019   0.1005
  -6.500  -0.4021   0.01215   0.00499  -0.0674   0.6960   0.1160
  -6.250  -0.3766   0.01179   0.00468  -0.0674   0.6904   0.1355
  -6.000  -0.3509   0.01141   0.00437  -0.0675   0.6853   0.1594
  -5.750  -0.3249   0.01098   0.00406  -0.0676   0.6796   0.1903
  -5.500  -0.2989   0.01054   0.00375  -0.0678   0.6738   0.2275
  -5.000  -0.2457   0.00966   0.00319  -0.0683   0.6636   0.3174
  -4.750  -0.2182   0.00933   0.00299  -0.0686   0.6580   0.3586
  -4.500  -0.1901   0.00914   0.00286  -0.0688   0.6527   0.3897
  -4.250  -0.1614   0.00901   0.00277  -0.0692   0.6479   0.4138
  -4.000  -0.1324   0.00891   0.00269  -0.0695   0.6429   0.4320
  -3.750  -0.1035   0.00885   0.00262  -0.0697   0.6378   0.4469
  -3.500  -0.0746   0.00881   0.00257  -0.0700   0.6329   0.4604
  -3.250  -0.0452   0.00877   0.00252  -0.0703   0.6279   0.4730
  -3.000  -0.0160   0.00873   0.00249  -0.0706   0.6228   0.4848
  -2.750   0.0130   0.00872   0.00246  -0.0709   0.6182   0.4944
  -2.500   0.0423   0.00872   0.00243  -0.0711   0.6140   0.5031
  -2.250   0.0717   0.00870   0.00240  -0.0715   0.6093   0.5097
  -2.000   0.1009   0.00870   0.00239  -0.0717   0.6043   0.5162
  -1.750   0.1301   0.00872   0.00236  -0.0720   0.5996   0.5223
  -1.500   0.1594   0.00872   0.00235  -0.0723   0.5953   0.5273
  -1.250   0.1887   0.00871   0.00235  -0.0726   0.5909   0.5326
  -1.000   0.2180   0.00873   0.00235  -0.0729   0.5865   0.5379
  -0.750   0.2471   0.00877   0.00234  -0.0732   0.5821   0.5426
  -0.500   0.2762   0.00877   0.00236  -0.0734   0.5778   0.5471
  -0.250   0.3055   0.00878   0.00238  -0.0737   0.5731   0.5520
   0.000   0.3347   0.00882   0.00239  -0.0740   0.5688   0.5570
   0.250   0.3636   0.00887   0.00241  -0.0743   0.5647   0.5613
   0.500   0.3927   0.00888   0.00245  -0.0745   0.5606   0.5657
   0.750   0.4219   0.00891   0.00250  -0.0748   0.5560   0.5708
   1.000   0.4509   0.00896   0.00254  -0.0751   0.5515   0.5757
   1.250   0.4796   0.00902   0.00258  -0.0753   0.5474   0.5798
   1.500   0.5086   0.00905   0.00265  -0.0755   0.5432   0.5844
   1.750   0.5375   0.00909   0.00271  -0.0758   0.5386   0.5896
   2.000   0.5663   0.00916   0.00277  -0.0760   0.5339   0.5946
   2.250   0.5946   0.00924   0.00284  -0.0761   0.5292   0.5990
   2.500   0.6235   0.00928   0.00294  -0.0764   0.5246   0.6037
   2.750   0.6521   0.00934   0.00302  -0.0766   0.5194   0.6087
   3.000   0.6804   0.00943   0.00310  -0.0767   0.5144   0.6139
   3.250   0.7086   0.00951   0.00321  -0.0769   0.5097   0.6188
   3.500   0.7370   0.00957   0.00332  -0.0770   0.5043   0.6239
   3.750   0.7650   0.00966   0.00343  -0.0771   0.4987   0.6289
   4.000   0.7928   0.00977   0.00354  -0.0772   0.4934   0.6336
   4.250   0.8208   0.00984   0.00367  -0.0773   0.4868   0.6388
   4.500   0.8477   0.00997   0.00380  -0.0772   0.4788   0.6444
   4.750   0.8753   0.01008   0.00393  -0.0773   0.4706   0.6498
   5.000   0.9020   0.01021   0.00408  -0.0772   0.4626   0.6545
   5.250   0.9291   0.01032   0.00424  -0.0771   0.4542   0.6597
   5.500   0.9547   0.01051   0.00440  -0.0768   0.4425   0.6654
   5.750   0.9794   0.01072   0.00459  -0.0764   0.4252   0.6707
   6.000   1.0033   0.01096   0.00481  -0.0759   0.4062   0.6761
   6.250   1.0273   0.01122   0.00504  -0.0753   0.3902   0.6818
   6.500   1.0504   0.01152   0.00530  -0.0747   0.3716   0.6871
   6.750   1.0712   0.01190   0.00562  -0.0737   0.3482   0.6925
   7.000   1.0890   0.01242   0.00603  -0.0723   0.3189   0.6985
   7.250   1.1039   0.01306   0.00653  -0.0704   0.2868   0.7045
   7.500   1.1160   0.01378   0.00711  -0.0681   0.2542   0.7099
   7.750   1.1264   0.01445   0.00767  -0.0656   0.2271   0.7160
   8.000   1.1329   0.01515   0.00826  -0.0623   0.2028   0.7225
   8.250   1.1397   0.01590   0.00894  -0.0593   0.1816   0.7289
   8.500   1.1461   0.01672   0.00971  -0.0564   0.1613   0.7359
   8.750   1.1532   0.01759   0.01052  -0.0539   0.1445   0.7427
   9.000   1.1600   0.01852   0.01142  -0.0515   0.1293   0.7497
   9.250   1.1669   0.01952   0.01239  -0.0493   0.1154   0.7576
   9.500   1.1738   0.02059   0.01344  -0.0472   0.1027   0.7652
   9.750   1.1813   0.02168   0.01453  -0.0454   0.0924   0.7739
  10.000   1.1888   0.02283   0.01569  -0.0437   0.0832   0.7823
  10.250   1.1963   0.02403   0.01690  -0.0421   0.0755   0.7920
  10.500   1.2036   0.02528   0.01819  -0.0405   0.0689   0.8018
  10.750   1.2122   0.02650   0.01945  -0.0392   0.0634   0.8131
  11.000   1.2191   0.02785   0.02084  -0.0378   0.0587   0.8254
  11.250   1.2273   0.02911   0.02219  -0.0366   0.0549   0.8400
  11.500   1.2331   0.03055   0.02369  -0.0352   0.0516   0.8585
  11.750   1.2396   0.03181   0.02508  -0.0337   0.0490   0.8858
  12.000   1.2497   0.03325   0.02664  -0.0333   0.0462   0.9449
  12.500   1.2654   0.03650   0.02996  -0.0322   0.0414   1.0000
  12.750   1.2724   0.03830   0.03178  -0.0317   0.0394   1.0000
  13.000   1.2802   0.04009   0.03361  -0.0312   0.0377   1.0000
  13.250   1.2879   0.04192   0.03549  -0.0309   0.0360   1.0000
  13.500   1.2947   0.04389   0.03749  -0.0306   0.0345   1.0000
  13.750   1.3006   0.04598   0.03961  -0.0304   0.0331   1.0000
  14.000   1.3080   0.04799   0.04168  -0.0303   0.0319   1.0000
  14.250   1.3145   0.05011   0.04384  -0.0302   0.0306   1.0000
  14.500   1.3197   0.05243   0.04621  -0.0302   0.0296   1.0000
  14.750   1.3242   0.05487   0.04869  -0.0303   0.0287   1.0000
  15.000   1.3304   0.05717   0.05105  -0.0305   0.0279   1.0000
  15.250   1.3356   0.05962   0.05358  -0.0307   0.0270   1.0000
  15.500   1.3407   0.06215   0.05615  -0.0310   0.0261   1.0000
  15.750   1.3441   0.06490   0.05896  -0.0314   0.0254   1.0000
  16.000   1.3464   0.06784   0.06193  -0.0319   0.0247   1.0000
  16.250   1.3505   0.07063   0.06481  -0.0324   0.0242   1.0000
  16.500   1.3545   0.07346   0.06772  -0.0330   0.0236   1.0000
  16.750   1.3575   0.07648   0.07081  -0.0337   0.0230   1.0000
  17.000   1.3596   0.07963   0.07403  -0.0345   0.0225   1.0000
  17.250   1.3617   0.08285   0.07731  -0.0354   0.0220   1.0000
  17.500   1.3620   0.08640   0.08093  -0.0365   0.0215   1.0000
  17.750   1.3612   0.09014   0.08473  -0.0377   0.0212   1.0000
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