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NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(3)-618 (naca633618-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.1 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633618-il-1000000-n5.txt
Download as CSV file: xf-naca633618-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(3)-618                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.9806   0.09141   0.08793  -0.0668   1.0000   0.0114
 -19.500  -0.9955   0.08558   0.08198  -0.0699   1.0000   0.0115
 -19.250  -1.0091   0.08004   0.07635  -0.0729   1.0000   0.0115
 -19.000  -1.0212   0.07486   0.07106  -0.0756   1.0000   0.0116
 -18.750  -1.0319   0.07002   0.06613  -0.0781   1.0000   0.0117
 -18.500  -1.0410   0.06553   0.06156  -0.0803   1.0000   0.0119
 -18.250  -1.0463   0.06167   0.05762  -0.0822   1.0000   0.0120
 -18.000  -1.0504   0.05805   0.05392  -0.0838   1.0000   0.0122
 -17.750  -1.0533   0.05468   0.05048  -0.0853   1.0000   0.0124
 -17.500  -1.0549   0.05156   0.04730  -0.0865   1.0000   0.0127
 -17.250  -1.0546   0.04873   0.04439  -0.0876   1.0000   0.0127
 -17.000  -1.0529   0.04615   0.04176  -0.0885   1.0000   0.0130
 -16.750  -1.0504   0.04374   0.03929  -0.0892   1.0000   0.0133
 -16.500  -1.0471   0.04149   0.03698  -0.0897   1.0000   0.0135
 -16.250  -1.0441   0.03930   0.03473  -0.0902   1.0000   0.0136
 -16.000  -1.0392   0.03741   0.03278  -0.0904   1.0000   0.0139
 -15.750  -1.0353   0.03549   0.03081  -0.0905   1.0000   0.0142
 -15.500  -1.0313   0.03366   0.02895  -0.0904   1.0000   0.0145
 -15.250  -1.0251   0.03188   0.02713  -0.0902   0.9897   0.0148
 -15.000  -0.9962   0.03002   0.02521  -0.0946   0.9672   0.0154
 -14.750  -0.9531   0.02826   0.02339  -0.1014   0.9539   0.0162
 -14.500  -0.9044   0.02658   0.02163  -0.1092   0.9410   0.0171
 -14.250  -0.8603   0.02513   0.02008  -0.1157   0.9185   0.0182
 -14.000  -0.8409   0.02411   0.01890  -0.1168   0.8898   0.0190
 -13.500  -0.8200   0.02222   0.01680  -0.1152   0.8534   0.0202
 -13.250  -0.8086   0.02138   0.01590  -0.1143   0.8403   0.0214
 -13.000  -0.7972   0.02056   0.01500  -0.1134   0.8288   0.0220
 -12.750  -0.7845   0.01981   0.01418  -0.1125   0.8179   0.0228
 -12.500  -0.7725   0.01905   0.01335  -0.1114   0.8084   0.0234
 -12.250  -0.7599   0.01832   0.01258  -0.1104   0.7994   0.0242
 -12.000  -0.7470   0.01766   0.01186  -0.1093   0.7913   0.0250
 -11.750  -0.7340   0.01703   0.01117  -0.1080   0.7830   0.0257
 -11.250  -0.7127   0.01593   0.00995  -0.1046   0.7679   0.0268
 -11.000  -0.6980   0.01540   0.00938  -0.1035   0.7604   0.0277
 -10.750  -0.6793   0.01497   0.00890  -0.1028   0.7539   0.0284
 -10.500  -0.6582   0.01461   0.00851  -0.1023   0.7472   0.0294
 -10.250  -0.6363   0.01429   0.00813  -0.1019   0.7408   0.0302
 -10.000  -0.6133   0.01399   0.00777  -0.1015   0.7352   0.0308
  -9.750  -0.5906   0.01361   0.00737  -0.1012   0.7292   0.0318
  -9.500  -0.5669   0.01330   0.00702  -0.1009   0.7225   0.0327
  -9.250  -0.5423   0.01302   0.00670  -0.1008   0.7170   0.0337
  -9.000  -0.5169   0.01275   0.00640  -0.1007   0.7116   0.0347
  -8.750  -0.4912   0.01252   0.00612  -0.1007   0.7055   0.0354
  -8.500  -0.4658   0.01223   0.00580  -0.1006   0.7000   0.0366
  -8.250  -0.4395   0.01196   0.00552  -0.1007   0.6945   0.0381
  -8.000  -0.4128   0.01174   0.00527  -0.1007   0.6889   0.0397
  -7.500  -0.3590   0.01128   0.00476  -0.1010   0.6784   0.0430
  -7.250  -0.3315   0.01107   0.00453  -0.1012   0.6727   0.0448
  -7.000  -0.3040   0.01089   0.00431  -0.1013   0.6673   0.0467
  -6.750  -0.2763   0.01067   0.00409  -0.1016   0.6626   0.0499
  -6.500  -0.2481   0.01048   0.00389  -0.1018   0.6575   0.0538
  -6.250  -0.2201   0.01028   0.00369  -0.1021   0.6520   0.0594
  -6.000  -0.1921   0.01008   0.00349  -0.1024   0.6466   0.0667
  -5.750  -0.1635   0.00986   0.00330  -0.1028   0.6424   0.0762
  -5.500  -0.1349   0.00965   0.00312  -0.1032   0.6372   0.0884
  -5.250  -0.1064   0.00942   0.00294  -0.1036   0.6318   0.1047
  -5.000  -0.0777   0.00919   0.00277  -0.1040   0.6271   0.1256
  -4.750  -0.0485   0.00893   0.00259  -0.1046   0.6224   0.1493
  -4.500  -0.0193   0.00871   0.00244  -0.1051   0.6177   0.1732
  -4.250   0.0098   0.00846   0.00228  -0.1056   0.6128   0.2054
  -4.000   0.0393   0.00817   0.00212  -0.1063   0.6085   0.2447
  -3.750   0.0691   0.00789   0.00197  -0.1070   0.6037   0.2864
  -3.500   0.0989   0.00763   0.00185  -0.1077   0.5985   0.3300
  -3.000   0.1587   0.00728   0.00172  -0.1090   0.5902   0.4098
  -2.750   0.1887   0.00721   0.00169  -0.1095   0.5860   0.4320
  -2.500   0.2185   0.00717   0.00167  -0.1099   0.5813   0.4480
  -2.250   0.2480   0.00717   0.00166  -0.1103   0.5765   0.4573
  -2.000   0.2778   0.00717   0.00166  -0.1107   0.5724   0.4664
  -1.750   0.3077   0.00715   0.00166  -0.1112   0.5681   0.4772
  -1.500   0.3373   0.00718   0.00166  -0.1115   0.5638   0.4859
  -1.250   0.3667   0.00719   0.00168  -0.1119   0.5596   0.4927
  -1.000   0.3963   0.00721   0.00169  -0.1122   0.5560   0.4983
  -0.750   0.4260   0.00723   0.00170  -0.1126   0.5521   0.5031
  -0.500   0.4556   0.00725   0.00172  -0.1130   0.5475   0.5088
  -0.250   0.4848   0.00729   0.00175  -0.1133   0.5430   0.5146
   0.000   0.5141   0.00734   0.00178  -0.1136   0.5393   0.5200
   0.250   0.5438   0.00736   0.00181  -0.1140   0.5358   0.5247
   0.500   0.5732   0.00739   0.00185  -0.1144   0.5316   0.5297
   0.750   0.6023   0.00744   0.00190  -0.1147   0.5271   0.5346
   1.000   0.6312   0.00751   0.00194  -0.1149   0.5227   0.5388
   1.250   0.6607   0.00754   0.00199  -0.1153   0.5190   0.5426
   1.500   0.6898   0.00759   0.00205  -0.1156   0.5141   0.5471
   1.750   0.7186   0.00766   0.00211  -0.1158   0.5090   0.5520
   2.000   0.7473   0.00773   0.00218  -0.1160   0.5046   0.5567
   2.250   0.7764   0.00778   0.00225  -0.1164   0.5004   0.5609
   2.500   0.8053   0.00784   0.00232  -0.1166   0.4958   0.5656
   2.750   0.8337   0.00793   0.00241  -0.1168   0.4910   0.5703
   3.000   0.8622   0.00801   0.00249  -0.1170   0.4868   0.5747
   3.250   0.8910   0.00807   0.00258  -0.1173   0.4823   0.5787
   3.500   0.9193   0.00816   0.00268  -0.1175   0.4768   0.5839
   3.750   0.9469   0.00827   0.00279  -0.1175   0.4707   0.5894
   4.000   0.9752   0.00836   0.00289  -0.1177   0.4638   0.5944
   4.250   1.0021   0.00852   0.00302  -0.1177   0.4548   0.5988
   4.500   1.0301   0.00861   0.00314  -0.1178   0.4472   0.6039
   4.750   1.0569   0.00876   0.00328  -0.1177   0.4391   0.6090
   5.000   1.0841   0.00889   0.00342  -0.1177   0.4304   0.6139
   5.250   1.1099   0.00909   0.00359  -0.1175   0.4188   0.6189
   5.500   1.1350   0.00933   0.00379  -0.1172   0.4032   0.6248
   5.750   1.1595   0.00959   0.00400  -0.1168   0.3866   0.6306
   6.000   1.1830   0.00989   0.00424  -0.1162   0.3670   0.6353
   6.250   1.2032   0.01037   0.00459  -0.1151   0.3376   0.6406
   6.500   1.2194   0.01102   0.00506  -0.1133   0.2990   0.6466
   6.750   1.2343   0.01171   0.00556  -0.1114   0.2637   0.6524
   7.000   1.2500   0.01229   0.00603  -0.1096   0.2380   0.6580
   7.250   1.2648   0.01283   0.00649  -0.1076   0.2155   0.6641
   7.500   1.2745   0.01340   0.00697  -0.1046   0.1948   0.6701
   7.750   1.2847   0.01401   0.00750  -0.1018   0.1764   0.6760
   8.000   1.2937   0.01469   0.00812  -0.0990   0.1572   0.6827
   8.250   1.3024   0.01542   0.00878  -0.0963   0.1404   0.6894
   8.500   1.3098   0.01625   0.00954  -0.0936   0.1239   0.6952
   8.750   1.3178   0.01710   0.01035  -0.0911   0.1101   0.7022
   9.000   1.3264   0.01799   0.01121  -0.0888   0.0984   0.7093
   9.250   1.3344   0.01897   0.01217  -0.0866   0.0871   0.7160
   9.500   1.3429   0.01998   0.01317  -0.0846   0.0775   0.7233
   9.750   1.3518   0.02103   0.01421  -0.0828   0.0693   0.7301
  10.000   1.3604   0.02215   0.01534  -0.0811   0.0619   0.7374
  10.250   1.3684   0.02337   0.01656  -0.0794   0.0548   0.7457
  10.500   1.3770   0.02460   0.01780  -0.0779   0.0492   0.7531
  10.750   1.3851   0.02591   0.01913  -0.0765   0.0443   0.7612
  11.250   1.4022   0.02861   0.02189  -0.0739   0.0368   0.7779
  11.500   1.4103   0.03006   0.02337  -0.0728   0.0341   0.7870
  11.750   1.4193   0.03147   0.02484  -0.0718   0.0319   0.7974
  12.000   1.4276   0.03297   0.02640  -0.0708   0.0304   0.8076
  12.250   1.4364   0.03447   0.02796  -0.0699   0.0290   0.8191
  12.500   1.4449   0.03603   0.02960  -0.0691   0.0278   0.8316
  12.750   1.4526   0.03768   0.03132  -0.0682   0.0267   0.8463
  13.000   1.4595   0.03940   0.03312  -0.0674   0.0256   0.8646
  13.250   1.4662   0.04104   0.03488  -0.0664   0.0250   0.8938
  13.500   1.4715   0.04257   0.03657  -0.0652   0.0243   1.0000
  13.750   1.4790   0.04451   0.03856  -0.0648   0.0235   1.0000
  14.000   1.4860   0.04655   0.04063  -0.0645   0.0227   1.0000
  14.250   1.4924   0.04869   0.04281  -0.0642   0.0220   1.0000
  14.500   1.5001   0.05075   0.04491  -0.0640   0.0215   1.0000
  14.750   1.5078   0.05282   0.04703  -0.0639   0.0210   1.0000
  15.000   1.5141   0.05509   0.04935  -0.0638   0.0203   1.0000
  15.250   1.5205   0.05739   0.05169  -0.0638   0.0197   1.0000
  15.500   1.5254   0.05992   0.05427  -0.0639   0.0191   1.0000
  15.750   1.5308   0.06241   0.05680  -0.0640   0.0185   1.0000
  16.000   1.5365   0.06492   0.05937  -0.0642   0.0181   1.0000
  16.250   1.5424   0.06741   0.06192  -0.0644   0.0175   1.0000
  16.500   1.5467   0.07018   0.06474  -0.0647   0.0169   1.0000
  16.750   1.5509   0.07296   0.06757  -0.0651   0.0163   1.0000
  17.000   1.5536   0.07600   0.07066  -0.0656   0.0157   1.0000
  17.250   1.5581   0.07883   0.07354  -0.0661   0.0152   1.0000
  17.500   1.5614   0.08186   0.07664  -0.0667   0.0146   1.0000
  17.750   1.5644   0.08496   0.07980  -0.0674   0.0140   1.0000
  18.000   1.5663   0.08827   0.08316  -0.0682   0.0135   1.0000
  18.250   1.5679   0.09165   0.08659  -0.0691   0.0129   1.0000
  18.500   1.5699   0.09498   0.08999  -0.0700   0.0124   1.0000
  18.750   1.5709   0.09851   0.09358  -0.0710   0.0119   1.0000
  19.000   1.5718   0.10205   0.09719  -0.0721   0.0114   1.0000
  19.250   1.5713   0.10587   0.10107  -0.0734   0.0111   1.0000
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