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J5012 12% (j5012-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: J5012 12% (j5012-il)
Reynolds number: 500,000
Max Cl/Cd: 58.91 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-j5012-il-500000-n5.txt
Download as CSV file: xf-j5012-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: J5012   12%                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.9158   0.13871   0.13579  -0.0039   1.0000   0.0119
 -18.500  -0.9533   0.12634   0.12324  -0.0105   1.0000   0.0118
 -18.250  -0.9811   0.11650   0.11327  -0.0157   1.0000   0.0118
 -18.000  -1.0057   0.10768   0.10432  -0.0204   1.0000   0.0118
 -17.750  -1.0286   0.09942   0.09591  -0.0247   1.0000   0.0118
 -17.500  -1.0477   0.09199   0.08835  -0.0287   1.0000   0.0119
 -17.250  -1.0703   0.08430   0.08051  -0.0327   1.0000   0.0118
 -17.000  -1.0842   0.07811   0.07421  -0.0360   1.0000   0.0119
 -16.750  -1.0995   0.07197   0.06792  -0.0392   1.0000   0.0119
 -16.500  -1.1120   0.06639   0.06221  -0.0421   1.0000   0.0121
 -16.250  -1.1230   0.06131   0.05699  -0.0446   1.0000   0.0121
 -16.000  -1.1326   0.05663   0.05218  -0.0467   1.0000   0.0122
 -15.750  -1.1409   0.05235   0.04776  -0.0484   1.0000   0.0122
 -15.500  -1.1443   0.04890   0.04419  -0.0497   1.0000   0.0124
 -15.250  -1.1489   0.04548   0.04063  -0.0506   1.0000   0.0126
 -15.000  -1.1489   0.04276   0.03779  -0.0510   1.0000   0.0128
 -14.750  -1.1516   0.03994   0.03483  -0.0511   1.0000   0.0130
 -14.500  -1.1491   0.03778   0.03256  -0.0509   1.0000   0.0132
 -14.250  -1.1483   0.03561   0.03026  -0.0504   1.0000   0.0133
 -14.000  -1.1451   0.03376   0.02830  -0.0495   1.0000   0.0135
 -13.750  -1.1412   0.03211   0.02652  -0.0484   1.0000   0.0136
 -13.500  -1.1406   0.03029   0.02462  -0.0468   1.0000   0.0139
 -13.250  -1.1383   0.02874   0.02298  -0.0450   1.0000   0.0141
 -13.000  -1.1343   0.02741   0.02157  -0.0431   1.0000   0.0143
 -12.750  -1.1287   0.02626   0.02034  -0.0410   1.0000   0.0145
 -12.500  -1.1214   0.02528   0.01929  -0.0388   1.0000   0.0148
 -12.250  -1.1133   0.02441   0.01834  -0.0365   1.0000   0.0151
 -12.000  -1.1058   0.02356   0.01742  -0.0339   1.0000   0.0153
 -11.750  -1.0968   0.02285   0.01665  -0.0314   1.0000   0.0157
 -11.500  -1.0889   0.02215   0.01587  -0.0285   1.0000   0.0161
 -11.250  -1.0802   0.02157   0.01523  -0.0255   1.0000   0.0166
 -11.000  -1.0728   0.02101   0.01460  -0.0222   1.0000   0.0169
 -10.750  -1.0648   0.02050   0.01401  -0.0188   1.0000   0.0171
 -10.500  -1.0566   0.01981   0.01327  -0.0156   1.0000   0.0176
 -10.250  -1.0466   0.01919   0.01261  -0.0126   1.0000   0.0180
 -10.000  -1.0351   0.01866   0.01204  -0.0098   1.0000   0.0186
  -9.750  -1.0227   0.01818   0.01152  -0.0072   1.0000   0.0192
  -9.500  -1.0100   0.01772   0.01102  -0.0045   1.0000   0.0198
  -9.250  -0.9968   0.01729   0.01053  -0.0019   1.0000   0.0204
  -9.000  -0.9833   0.01689   0.01007   0.0006   1.0000   0.0211
  -8.750  -0.9657   0.01644   0.00958   0.0023   0.9996   0.0219
  -8.500  -0.9366   0.01589   0.00903   0.0015   0.9975   0.0234
  -8.250  -0.9066   0.01545   0.00854   0.0006   0.9951   0.0253
  -8.000  -0.8772   0.01501   0.00807  -0.0001   0.9928   0.0272
  -7.750  -0.8492   0.01454   0.00760  -0.0005   0.9898   0.0297
  -7.500  -0.8193   0.01416   0.00719  -0.0013   0.9870   0.0325
  -7.250  -0.7887   0.01374   0.00678  -0.0022   0.9846   0.0363
  -7.000  -0.7567   0.01340   0.00642  -0.0034   0.9827   0.0407
  -6.750  -0.7308   0.01301   0.00606  -0.0032   0.9783   0.0458
  -6.500  -0.7011   0.01266   0.00571  -0.0038   0.9748   0.0513
  -6.250  -0.6698   0.01231   0.00539  -0.0048   0.9722   0.0583
  -6.000  -0.6374   0.01195   0.00506  -0.0060   0.9701   0.0670
  -5.750  -0.6109   0.01162   0.00477  -0.0059   0.9652   0.0770
  -5.500  -0.5815   0.01126   0.00447  -0.0065   0.9610   0.0918
  -5.250  -0.5495   0.01088   0.00418  -0.0076   0.9580   0.1112
  -5.000  -0.5164   0.01048   0.00390  -0.0090   0.9554   0.1341
  -4.750  -0.4914   0.01015   0.00366  -0.0086   0.9483   0.1570
  -4.500  -0.4607   0.00981   0.00341  -0.0093   0.9434   0.1830
  -4.250  -0.4305   0.00943   0.00317  -0.0101   0.9384   0.2156
  -4.000  -0.4038   0.00910   0.00296  -0.0100   0.9305   0.2481
  -3.750  -0.3730   0.00877   0.00275  -0.0107   0.9244   0.2818
  -3.500  -0.3474   0.00849   0.00258  -0.0103   0.9150   0.3146
  -3.250  -0.3199   0.00819   0.00241  -0.0103   0.9067   0.3524
  -3.000  -0.2941   0.00791   0.00226  -0.0099   0.8966   0.3917
  -2.750  -0.2691   0.00767   0.00213  -0.0093   0.8858   0.4288
  -2.500  -0.2435   0.00745   0.00201  -0.0088   0.8749   0.4623
  -2.250  -0.2180   0.00728   0.00190  -0.0082   0.8629   0.4927
  -2.000  -0.1937   0.00712   0.00181  -0.0074   0.8496   0.5236
  -1.750  -0.1694   0.00698   0.00174  -0.0065   0.8358   0.5536
  -1.500  -0.1450   0.00686   0.00167  -0.0057   0.8217   0.5821
  -1.250  -0.1210   0.00676   0.00162  -0.0047   0.8068   0.6090
  -1.000  -0.0967   0.00668   0.00157  -0.0038   0.7914   0.6335
  -0.750  -0.0725   0.00662   0.00154  -0.0029   0.7752   0.6573
  -0.500  -0.0482   0.00658   0.00152  -0.0020   0.7581   0.6786
  -0.250  -0.0241   0.00656   0.00150  -0.0010   0.7400   0.7001
   0.000   0.0000   0.00655   0.00150   0.0000   0.7210   0.7209
   0.250   0.0241   0.00655   0.00150   0.0010   0.7003   0.7402
   0.500   0.0482   0.00658   0.00152   0.0020   0.6789   0.7581
   0.750   0.0724   0.00662   0.00154   0.0029   0.6569   0.7752
   1.000   0.0966   0.00668   0.00157   0.0038   0.6335   0.7915
   1.250   0.1209   0.00676   0.00162   0.0048   0.6087   0.8069
   1.500   0.1450   0.00686   0.00167   0.0057   0.5820   0.8218
   1.750   0.1694   0.00698   0.00174   0.0065   0.5539   0.8359
   2.000   0.1938   0.00711   0.00181   0.0074   0.5245   0.8496
   2.500   0.2435   0.00745   0.00201   0.0088   0.4626   0.8748
   2.750   0.2689   0.00767   0.00213   0.0094   0.4279   0.8858
   3.000   0.2942   0.00790   0.00226   0.0099   0.3926   0.8965
   3.250   0.3199   0.00819   0.00241   0.0103   0.3527   0.9066
   3.500   0.3473   0.00849   0.00258   0.0103   0.3145   0.9150
   3.750   0.3730   0.00877   0.00275   0.0107   0.2819   0.9244
   4.000   0.4037   0.00911   0.00296   0.0100   0.2473   0.9305
   4.250   0.4304   0.00944   0.00317   0.0101   0.2150   0.9383
   4.500   0.4607   0.00980   0.00341   0.0093   0.1839   0.9434
   4.750   0.4914   0.01016   0.00366   0.0086   0.1566   0.9482
   5.000   0.5163   0.01048   0.00390   0.0090   0.1340   0.9554
   5.250   0.5494   0.01088   0.00418   0.0076   0.1112   0.9580
   5.500   0.5816   0.01125   0.00447   0.0065   0.0923   0.9610
   5.750   0.6110   0.01161   0.00476   0.0059   0.0777   0.9651
   6.000   0.6375   0.01195   0.00506   0.0060   0.0672   0.9702
   6.250   0.6698   0.01231   0.00539   0.0048   0.0584   0.9722
   6.500   0.7011   0.01267   0.00572   0.0038   0.0513   0.9749
   6.750   0.7307   0.01301   0.00606   0.0032   0.0454   0.9783
   7.000   0.7567   0.01339   0.00642   0.0034   0.0403   0.9827
   7.250   0.7887   0.01374   0.00678   0.0022   0.0361   0.9846
   7.500   0.8194   0.01416   0.00720   0.0012   0.0324   0.9870
   7.750   0.8492   0.01454   0.00760   0.0005   0.0296   0.9898
   8.000   0.8771   0.01503   0.00808   0.0001   0.0268   0.9928
   8.250   0.9067   0.01544   0.00854  -0.0007   0.0252   0.9952
   8.500   0.9366   0.01590   0.00903  -0.0015   0.0236   0.9975
   8.750   0.9657   0.01645   0.00959  -0.0023   0.0219   0.9996
   9.000   0.9832   0.01690   0.01008  -0.0006   0.0210   1.0000
   9.250   0.9967   0.01730   0.01054   0.0020   0.0203   1.0000
   9.500   1.0097   0.01774   0.01103   0.0046   0.0197   1.0000
   9.750   1.0226   0.01818   0.01152   0.0072   0.0191   1.0000
  10.000   1.0349   0.01867   0.01205   0.0099   0.0186   1.0000
  10.250   1.0465   0.01920   0.01261   0.0126   0.0180   1.0000
  10.500   1.0565   0.01982   0.01327   0.0156   0.0176   1.0000
  10.750   1.0644   0.02052   0.01403   0.0189   0.0171   1.0000
  11.000   1.0721   0.02105   0.01464   0.0223   0.0169   1.0000
  11.250   1.0799   0.02159   0.01525   0.0256   0.0165   1.0000
  11.500   1.0879   0.02221   0.01594   0.0286   0.0162   1.0000
  11.750   1.0971   0.02284   0.01664   0.0313   0.0157   1.0000
  12.000   1.1053   0.02360   0.01747   0.0340   0.0154   1.0000
  12.250   1.1135   0.02441   0.01835   0.0365   0.0151   1.0000
  12.500   1.1217   0.02528   0.01929   0.0387   0.0148   1.0000
  12.750   1.1287   0.02628   0.02037   0.0409   0.0145   1.0000
  13.000   1.1349   0.02740   0.02157   0.0430   0.0144   1.0000
  13.250   1.1394   0.02870   0.02295   0.0449   0.0142   1.0000
  13.500   1.1405   0.03035   0.02467   0.0468   0.0138   1.0000
  13.750   1.1404   0.03222   0.02663   0.0484   0.0136   1.0000
  14.000   1.1452   0.03381   0.02834   0.0494   0.0135   1.0000
  14.250   1.1482   0.03568   0.03033   0.0503   0.0134   1.0000
  14.500   1.1497   0.03780   0.03257   0.0508   0.0132   1.0000
  14.750   1.1507   0.04011   0.03500   0.0510   0.0131   1.0000
  15.000   1.1500   0.04275   0.03777   0.0509   0.0129   1.0000
  15.250   1.1489   0.04559   0.04074   0.0504   0.0127   1.0000
  15.500   1.1438   0.04906   0.04436   0.0495   0.0126   1.0000
  15.750   1.1413   0.05244   0.04785   0.0483   0.0124   1.0000
  16.000   1.1333   0.05668   0.05223   0.0465   0.0123   1.0000
  16.250   1.1242   0.06131   0.05700   0.0444   0.0122   1.0000
  16.500   1.1129   0.06645   0.06228   0.0419   0.0121   1.0000
  16.750   1.0993   0.07219   0.06815   0.0389   0.0120   1.0000
  17.000   1.0858   0.07810   0.07419   0.0358   0.0120   1.0000
  17.250   1.0668   0.08510   0.08134   0.0321   0.0119   1.0000
  17.500   1.0524   0.09155   0.08791   0.0286   0.0118   1.0000
  17.750   1.0301   0.09947   0.09597   0.0244   0.0118   1.0000
  18.000   1.0076   0.10771   0.10434   0.0200   0.0118   1.0000
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