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NACA 63-415 AIRFOIL (n63415-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63-415 AIRFOIL (n63415-il)
Reynolds number: 500,000
Max Cl/Cd: 90.74 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63415-il-500000-n5.txt
Download as CSV file: xf-n63415-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-415 AIRFOIL                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.8075   0.12235   0.11935  -0.0302   1.0000   0.0130
 -18.000  -0.8547   0.10829   0.10508  -0.0381   1.0000   0.0130
 -17.750  -0.8829   0.09863   0.09526  -0.0436   1.0000   0.0130
 -17.500  -0.9059   0.09028   0.08675  -0.0485   1.0000   0.0130
 -17.250  -0.9249   0.08295   0.07928  -0.0527   1.0000   0.0131
 -17.000  -0.9403   0.07656   0.07274  -0.0564   1.0000   0.0131
 -16.750  -0.9529   0.07082   0.06685  -0.0597   1.0000   0.0132
 -16.500  -0.9624   0.06581   0.06171  -0.0624   1.0000   0.0133
 -16.250  -0.9698   0.06130   0.05706  -0.0648   1.0000   0.0134
 -16.000  -0.9761   0.05714   0.05276  -0.0668   1.0000   0.0135
 -15.750  -0.9821   0.05325   0.04878  -0.0687   1.0000   0.0137
 -15.500  -0.9856   0.04985   0.04529  -0.0701   1.0000   0.0138
 -15.250  -0.9878   0.04675   0.04213  -0.0713   1.0000   0.0140
 -15.000  -0.9877   0.04400   0.03930  -0.0722   1.0000   0.0141
 -14.750  -0.9859   0.04154   0.03675  -0.0729   1.0000   0.0143
 -14.500  -0.9832   0.03923   0.03437  -0.0735   1.0000   0.0145
 -14.250  -0.9793   0.03713   0.03219  -0.0738   1.0000   0.0147
 -14.000  -0.9730   0.03533   0.03031  -0.0740   1.0000   0.0150
 -13.750  -0.9665   0.03361   0.02851  -0.0740   1.0000   0.0153
 -13.500  -0.9608   0.03188   0.02670  -0.0738   1.0000   0.0156
 -13.250  -0.9540   0.03032   0.02505  -0.0734   1.0000   0.0159
 -13.000  -0.9461   0.02892   0.02357  -0.0729   1.0000   0.0162
 -12.750  -0.9381   0.02762   0.02217  -0.0722   1.0000   0.0165
 -12.500  -0.9329   0.02622   0.02075  -0.0712   1.0000   0.0169
 -12.250  -0.9266   0.02506   0.01954  -0.0700   1.0000   0.0171
 -12.000  -0.9212   0.02404   0.01849  -0.0683   1.0000   0.0174
 -11.750  -0.9013   0.02306   0.01746  -0.0690   0.9877   0.0179
 -11.500  -0.8695   0.02198   0.01630  -0.0721   0.9686   0.0185
 -11.250  -0.8356   0.02099   0.01521  -0.0752   0.9517   0.0192
 -11.000  -0.8052   0.02015   0.01423  -0.0773   0.9334   0.0199
 -10.750  -0.7837   0.01936   0.01335  -0.0777   0.9138   0.0206
 -10.500  -0.7647   0.01880   0.01270  -0.0771   0.8977   0.0212
 -10.250  -0.7458   0.01829   0.01211  -0.0762   0.8839   0.0218
 -10.000  -0.7265   0.01780   0.01151  -0.0754   0.8719   0.0226
  -9.500  -0.6856   0.01684   0.01036  -0.0740   0.8506   0.0241
  -9.250  -0.6649   0.01634   0.00980  -0.0733   0.8414   0.0250
  -9.000  -0.6421   0.01595   0.00936  -0.0729   0.8323   0.0262
  -8.750  -0.6191   0.01556   0.00888  -0.0724   0.8242   0.0272
  -8.500  -0.5954   0.01519   0.00843  -0.0721   0.8159   0.0282
  -8.250  -0.5722   0.01475   0.00792  -0.0717   0.8085   0.0293
  -8.000  -0.5481   0.01433   0.00746  -0.0714   0.8007   0.0305
  -7.750  -0.5232   0.01401   0.00709  -0.0712   0.7934   0.0320
  -7.500  -0.4976   0.01370   0.00671  -0.0711   0.7865   0.0334
  -7.250  -0.4723   0.01335   0.00631  -0.0710   0.7793   0.0349
  -7.000  -0.4467   0.01301   0.00593  -0.0709   0.7728   0.0366
  -6.750  -0.4205   0.01272   0.00559  -0.0708   0.7658   0.0385
  -6.500  -0.3939   0.01248   0.00528  -0.0708   0.7593   0.0405
  -6.250  -0.3674   0.01215   0.00495  -0.0708   0.7528   0.0435
  -6.000  -0.3405   0.01190   0.00467  -0.0709   0.7460   0.0470
  -5.750  -0.3135   0.01164   0.00438  -0.0709   0.7400   0.0515
  -5.500  -0.2862   0.01137   0.00411  -0.0710   0.7333   0.0582
  -5.250  -0.2591   0.01110   0.00385  -0.0712   0.7268   0.0692
  -5.000  -0.2317   0.01080   0.00359  -0.0713   0.7210   0.0859
  -4.750  -0.2043   0.01046   0.00334  -0.0716   0.7144   0.1108
  -4.250  -0.1494   0.00970   0.00284  -0.0722   0.7022   0.1906
  -4.000  -0.1219   0.00925   0.00259  -0.0726   0.6959   0.2479
  -3.750  -0.0942   0.00883   0.00236  -0.0730   0.6902   0.3111
  -3.500  -0.0659   0.00846   0.00220  -0.0734   0.6838   0.3738
  -3.250  -0.0373   0.00828   0.00211  -0.0738   0.6777   0.4130
  -3.000  -0.0085   0.00815   0.00205  -0.0741   0.6723   0.4466
  -2.750   0.0204   0.00804   0.00202  -0.0743   0.6660   0.4790
  -2.500   0.0492   0.00800   0.00199  -0.0746   0.6600   0.5023
  -2.250   0.0783   0.00797   0.00196  -0.0748   0.6545   0.5162
  -2.000   0.1074   0.00794   0.00195  -0.0751   0.6487   0.5298
  -1.750   0.1363   0.00795   0.00193  -0.0753   0.6430   0.5419
  -1.500   0.1655   0.00795   0.00191  -0.0755   0.6373   0.5504
  -1.250   0.1946   0.00795   0.00190  -0.0757   0.6313   0.5574
  -1.000   0.2234   0.00797   0.00189  -0.0759   0.6260   0.5646
  -0.500   0.2816   0.00799   0.00190  -0.0764   0.6146   0.5783
  -0.250   0.3104   0.00803   0.00191  -0.0766   0.6091   0.5851
   0.000   0.3396   0.00804   0.00193  -0.0769   0.6039   0.5910
   0.250   0.3686   0.00806   0.00196  -0.0771   0.5983   0.5969
   0.500   0.3973   0.00812   0.00198  -0.0773   0.5928   0.6032
   0.750   0.4263   0.00814   0.00203  -0.0775   0.5873   0.6090
   1.000   0.4552   0.00817   0.00207  -0.0777   0.5816   0.6150
   1.500   0.5127   0.00827   0.00218  -0.0781   0.5701   0.6269
   1.750   0.5413   0.00833   0.00225  -0.0783   0.5637   0.6334
   2.000   0.5699   0.00840   0.00232  -0.0784   0.5579   0.6397
   2.250   0.5985   0.00844   0.00240  -0.0786   0.5517   0.6453
   2.500   0.6269   0.00852   0.00249  -0.0787   0.5455   0.6519
   2.750   0.6554   0.00859   0.00258  -0.0789   0.5395   0.6583
   3.000   0.6837   0.00866   0.00269  -0.0790   0.5325   0.6648
   3.250   0.7118   0.00875   0.00279  -0.0791   0.5245   0.6713
   3.500   0.7394   0.00885   0.00289  -0.0791   0.5130   0.6775
   3.750   0.7672   0.00895   0.00302  -0.0791   0.5018   0.6845
   4.000   0.7947   0.00908   0.00314  -0.0791   0.4915   0.6914
   4.250   0.8216   0.00922   0.00329  -0.0790   0.4771   0.6976
   4.500   0.8480   0.00940   0.00344  -0.0788   0.4569   0.7047
   4.750   0.8738   0.00963   0.00361  -0.0785   0.4341   0.7114
   5.000   0.8984   0.00993   0.00383  -0.0781   0.4038   0.7184
   5.250   0.9216   0.01037   0.00411  -0.0775   0.3659   0.7255
   5.500   0.9437   0.01087   0.00446  -0.0767   0.3244   0.7323
   5.750   0.9646   0.01147   0.00488  -0.0758   0.2816   0.7398
   6.000   0.9849   0.01212   0.00535  -0.0749   0.2404   0.7466
   6.250   1.0047   0.01276   0.00584  -0.0738   0.2015   0.7542
   6.500   1.0239   0.01343   0.00635  -0.0727   0.1670   0.7618
   6.750   1.0429   0.01406   0.00687  -0.0715   0.1377   0.7696
   7.000   1.0616   0.01469   0.00739  -0.0704   0.1120   0.7777
   7.250   1.0799   0.01528   0.00792  -0.0690   0.0918   0.7863
   7.500   1.0971   0.01590   0.00847  -0.0676   0.0735   0.7955
   7.750   1.1133   0.01652   0.00904  -0.0660   0.0588   0.8052
   8.000   1.1290   0.01709   0.00960  -0.0643   0.0487   0.8152
   8.250   1.1427   0.01762   0.01014  -0.0622   0.0427   0.8267
   8.500   1.1559   0.01814   0.01070  -0.0600   0.0389   0.8387
   8.750   1.1689   0.01868   0.01130  -0.0579   0.0362   0.8516
   9.000   1.1814   0.01923   0.01193  -0.0558   0.0340   0.8665
   9.250   1.1917   0.01985   0.01263  -0.0534   0.0321   0.8851
   9.500   1.2003   0.02046   0.01334  -0.0507   0.0308   0.9126
   9.750   1.2120   0.02104   0.01404  -0.0489   0.0295   1.0000
  10.000   1.2257   0.02189   0.01491  -0.0477   0.0280   1.0000
  10.250   1.2378   0.02287   0.01591  -0.0464   0.0266   1.0000
  10.500   1.2501   0.02387   0.01695  -0.0452   0.0257   1.0000
  10.750   1.2632   0.02485   0.01798  -0.0442   0.0246   1.0000
  11.000   1.2753   0.02593   0.01910  -0.0431   0.0234   1.0000
  11.250   1.2860   0.02714   0.02035  -0.0421   0.0224   1.0000
  11.500   1.2955   0.02849   0.02173  -0.0411   0.0214   1.0000
  11.750   1.3070   0.02971   0.02303  -0.0402   0.0206   1.0000
  12.000   1.3175   0.03105   0.02443  -0.0394   0.0196   1.0000
  12.250   1.3268   0.03252   0.02594  -0.0387   0.0189   1.0000
  12.500   1.3350   0.03414   0.02760  -0.0379   0.0181   1.0000
  12.750   1.3424   0.03586   0.02938  -0.0372   0.0176   1.0000
  13.000   1.3506   0.03755   0.03114  -0.0366   0.0170   1.0000
  13.250   1.3580   0.03935   0.03302  -0.0361   0.0164   1.0000
  13.500   1.3651   0.04124   0.03498  -0.0357   0.0159   1.0000
  13.750   1.3710   0.04326   0.03706  -0.0353   0.0154   1.0000
  14.000   1.3763   0.04543   0.03929  -0.0350   0.0151   1.0000
  14.250   1.3803   0.04782   0.04173  -0.0349   0.0147   1.0000
  14.500   1.3837   0.05032   0.04431  -0.0348   0.0144   1.0000
  14.750   1.3877   0.05283   0.04691  -0.0349   0.0142   1.0000
  15.000   1.3912   0.05548   0.04966  -0.0350   0.0139   1.0000
  15.250   1.3941   0.05826   0.05253  -0.0353   0.0136   1.0000
  15.500   1.3968   0.06114   0.05550  -0.0357   0.0134   1.0000
  15.750   1.3990   0.06413   0.05858  -0.0362   0.0131   1.0000
  16.000   1.4005   0.06732   0.06186  -0.0368   0.0129   1.0000
  16.250   1.4016   0.07062   0.06525  -0.0376   0.0128   1.0000
  16.500   1.4017   0.07413   0.06885  -0.0385   0.0126   1.0000
  16.750   1.4019   0.07771   0.07252  -0.0396   0.0123   1.0000
  17.000   1.4005   0.08160   0.07650  -0.0408   0.0122   1.0000
  17.250   1.3980   0.08574   0.08073  -0.0422   0.0120   1.0000
  17.500   1.3944   0.09013   0.08521  -0.0438   0.0119   1.0000
  17.750   1.3902   0.09469   0.08987  -0.0456   0.0117   1.0000
  18.000   1.3875   0.09911   0.09441  -0.0474   0.0116   1.0000
  18.250   1.3845   0.10366   0.09908  -0.0493   0.0115   1.0000
  18.500   1.3805   0.10843   0.10396  -0.0515   0.0114   1.0000
  18.750   1.3762   0.11332   0.10896  -0.0537   0.0113   1.0000
  19.000   1.3714   0.11836   0.11412  -0.0562   0.0112   1.0000
  19.250   1.3665   0.12349   0.11936  -0.0588   0.0111   1.0000
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