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J5012 12% (j5012-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: J5012 12% (j5012-il)
Reynolds number: 500,000
Max Cl/Cd: 59.94 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-j5012-il-500000.txt
Download as CSV file: xf-j5012-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.9440   0.09733   0.09422  -0.0294   1.0000   0.0178
 -16.500  -0.9784   0.08662   0.08331  -0.0361   1.0000   0.0178
 -16.250  -1.0017   0.07858   0.07506  -0.0411   1.0000   0.0176
 -16.000  -1.0233   0.07146   0.06776  -0.0452   1.0000   0.0176
 -15.750  -1.0382   0.06582   0.06193  -0.0483   1.0000   0.0175
 -15.500  -1.0542   0.06043   0.05640  -0.0507   1.0000   0.0177
 -15.250  -1.0657   0.05598   0.05183  -0.0523   1.0000   0.0179
 -15.000  -1.0749   0.05202   0.04771  -0.0535   1.0000   0.0180
 -14.750  -1.0818   0.04856   0.04413  -0.0541   1.0000   0.0181
 -14.500  -1.0845   0.04580   0.04127  -0.0543   1.0000   0.0183
 -14.250  -1.0859   0.04337   0.03876  -0.0542   1.0000   0.0186
 -14.000  -1.0885   0.04085   0.03610  -0.0536   1.0000   0.0187
 -13.750  -1.0894   0.03866   0.03379  -0.0527   1.0000   0.0190
 -13.500  -1.0887   0.03678   0.03179  -0.0515   1.0000   0.0193
 -13.250  -1.0861   0.03516   0.03005  -0.0501   1.0000   0.0196
 -13.000  -1.0830   0.03370   0.02847  -0.0484   1.0000   0.0201
 -12.750  -1.0798   0.03209   0.02673  -0.0464   1.0000   0.0203
 -12.500  -1.0749   0.03079   0.02530  -0.0443   1.0000   0.0207
 -12.250  -1.0692   0.02956   0.02393  -0.0420   1.0000   0.0210
 -12.000  -1.0624   0.02840   0.02265  -0.0396   1.0000   0.0212
 -11.750  -1.0547   0.02749   0.02162  -0.0371   1.0000   0.0215
 -11.500  -1.0512   0.02548   0.01949  -0.0342   1.0000   0.0220
 -11.250  -1.0455   0.02431   0.01826  -0.0312   1.0000   0.0226
 -11.000  -1.0384   0.02351   0.01742  -0.0281   1.0000   0.0231
 -10.750  -1.0310   0.02289   0.01676  -0.0249   1.0000   0.0236
 -10.500  -1.0235   0.02230   0.01613  -0.0215   1.0000   0.0243
 -10.250  -1.0137   0.02162   0.01538  -0.0186   1.0000   0.0249
 -10.000  -1.0026   0.02098   0.01467  -0.0158   1.0000   0.0256
  -9.750  -0.9910   0.02037   0.01399  -0.0130   1.0000   0.0262
  -9.500  -0.9789   0.01983   0.01337  -0.0102   1.0000   0.0266
  -9.250  -0.9742   0.01876   0.01223  -0.0063   1.0000   0.0275
  -9.000  -0.9660   0.01802   0.01148  -0.0029   1.0000   0.0285
  -8.750  -0.9543   0.01751   0.01095  -0.0001   1.0000   0.0294
  -8.500  -0.9421   0.01704   0.01044   0.0027   1.0000   0.0305
  -8.250  -0.9284   0.01666   0.01001   0.0053   1.0000   0.0320
  -8.000  -0.9153   0.01622   0.00951   0.0080   1.0000   0.0333
  -7.750  -0.9057   0.01554   0.00882   0.0112   1.0000   0.0356
  -7.500  -0.8914   0.01517   0.00843   0.0136   1.0000   0.0379
  -7.250  -0.8756   0.01488   0.00810   0.0158   1.0000   0.0403
  -7.000  -0.8548   0.01427   0.00750   0.0168   0.9990   0.0451
  -6.750  -0.8209   0.01386   0.00707   0.0152   0.9964   0.0509
  -6.500  -0.7866   0.01345   0.00669   0.0135   0.9941   0.0588
  -6.250  -0.7554   0.01298   0.00627   0.0124   0.9909   0.0688
  -6.000  -0.7226   0.01256   0.00590   0.0110   0.9876   0.0810
  -5.750  -0.6881   0.01216   0.00557   0.0093   0.9850   0.0975
  -5.500  -0.6528   0.01172   0.00526   0.0074   0.9830   0.1221
  -5.250  -0.6247   0.01127   0.00494   0.0070   0.9782   0.1510
  -5.000  -0.5930   0.01077   0.00465   0.0058   0.9745   0.1903
  -4.750  -0.5589   0.01029   0.00438   0.0041   0.9719   0.2357
  -4.500  -0.5232   0.00984   0.00413   0.0021   0.9700   0.2844
  -4.250  -0.4977   0.00944   0.00390   0.0025   0.9637   0.3263
  -4.000  -0.4648   0.00902   0.00368   0.0012   0.9601   0.3745
  -3.750  -0.4293   0.00862   0.00346  -0.0006   0.9577   0.4236
  -3.500  -0.3920   0.00826   0.00327  -0.0027   0.9559   0.4672
  -3.250  -0.3654   0.00798   0.00312  -0.0024   0.9494   0.5052
  -3.000  -0.3335   0.00766   0.00295  -0.0033   0.9449   0.5461
  -2.750  -0.2989   0.00737   0.00279  -0.0046   0.9415   0.5844
  -2.500  -0.2733   0.00716   0.00268  -0.0040   0.9337   0.6155
  -2.250  -0.2424   0.00694   0.00254  -0.0044   0.9277   0.6451
  -2.000  -0.2151   0.00677   0.00245  -0.0041   0.9197   0.6715
  -1.750  -0.1865   0.00660   0.00235  -0.0040   0.9116   0.6970
  -1.500  -0.1605   0.00648   0.00229  -0.0033   0.9016   0.7205
  -1.250  -0.1317   0.00637   0.00222  -0.0032   0.8927   0.7420
  -1.000  -0.1060   0.00628   0.00218  -0.0024   0.8811   0.7619
  -0.750  -0.0800   0.00622   0.00214  -0.0017   0.8691   0.7806
  -0.500  -0.0533   0.00618   0.00212  -0.0012   0.8568   0.7977
  -0.250  -0.0266   0.00615   0.00209  -0.0006   0.8437   0.8141
   0.000   0.0000   0.00614   0.00209   0.0000   0.8296   0.8296
   0.250   0.0265   0.00615   0.00209   0.0006   0.8141   0.8438
   0.500   0.0533   0.00618   0.00212   0.0012   0.7979   0.8568
   0.750   0.0800   0.00622   0.00214   0.0017   0.7804   0.8691
   1.000   0.1060   0.00628   0.00218   0.0024   0.7619   0.8811
   1.250   0.1316   0.00637   0.00222   0.0032   0.7419   0.8928
   1.500   0.1605   0.00648   0.00229   0.0033   0.7205   0.9017
   1.750   0.1865   0.00660   0.00235   0.0040   0.6970   0.9116
   2.000   0.2152   0.00677   0.00245   0.0041   0.6721   0.9196
   2.250   0.2424   0.00694   0.00254   0.0044   0.6454   0.9276
   2.500   0.2733   0.00716   0.00268   0.0040   0.6154   0.9337
   2.750   0.2989   0.00737   0.00279   0.0046   0.5843   0.9415
   3.000   0.3335   0.00766   0.00294   0.0033   0.5461   0.9449
   3.250   0.3653   0.00798   0.00311   0.0024   0.5051   0.9493
   3.500   0.3919   0.00826   0.00327   0.0027   0.4672   0.9559
   3.750   0.4292   0.00862   0.00346   0.0006   0.4228   0.9577
   4.000   0.4648   0.00902   0.00368  -0.0012   0.3747   0.9601
   4.250   0.4976   0.00944   0.00390  -0.0024   0.3260   0.9637
   4.500   0.5231   0.00984   0.00413  -0.0021   0.2837   0.9700
   4.750   0.5588   0.01030   0.00438  -0.0041   0.2348   0.9718
   5.000   0.5929   0.01077   0.00465  -0.0058   0.1903   0.9745
   5.250   0.6246   0.01126   0.00494  -0.0070   0.1513   0.9782
   5.500   0.6528   0.01172   0.00526  -0.0074   0.1223   0.9829
   5.750   0.6881   0.01216   0.00556  -0.0093   0.0978   0.9850
   6.000   0.7227   0.01256   0.00590  -0.0111   0.0812   0.9876
   6.250   0.7554   0.01298   0.00627  -0.0124   0.0688   0.9909
   6.500   0.7867   0.01345   0.00669  -0.0135   0.0588   0.9941
   6.750   0.8209   0.01387   0.00707  -0.0152   0.0506   0.9964
   7.000   0.8548   0.01426   0.00749  -0.0168   0.0449   0.9990
   7.250   0.8757   0.01487   0.00809  -0.0159   0.0402   1.0000
   7.500   0.8914   0.01517   0.00843  -0.0136   0.0379   1.0000
   7.750   0.9057   0.01554   0.00883  -0.0112   0.0356   1.0000
   8.000   0.9136   0.01634   0.00962  -0.0077   0.0330   1.0000
   8.250   0.9284   0.01666   0.01001  -0.0053   0.0319   1.0000
   8.500   0.9418   0.01706   0.01046  -0.0027   0.0306   1.0000
   8.750   0.9543   0.01751   0.01095   0.0001   0.0294   1.0000
   9.000   0.9657   0.01803   0.01149   0.0030   0.0284   1.0000
   9.250   0.9736   0.01880   0.01228   0.0064   0.0274   1.0000
   9.500   0.9789   0.01983   0.01337   0.0103   0.0265   1.0000
   9.750   0.9912   0.02036   0.01398   0.0130   0.0261   1.0000
  10.000   1.0025   0.02099   0.01468   0.0158   0.0255   1.0000
  10.250   1.0137   0.02162   0.01538   0.0186   0.0248   1.0000
  10.500   1.0242   0.02221   0.01603   0.0214   0.0241   1.0000
  10.750   1.0309   0.02292   0.01679   0.0249   0.0236   1.0000
  11.000   1.0381   0.02359   0.01750   0.0282   0.0231   1.0000
  11.250   1.0455   0.02435   0.01830   0.0312   0.0226   1.0000
  11.500   1.0519   0.02545   0.01947   0.0341   0.0222   1.0000
  11.750   1.0555   0.02746   0.02159   0.0370   0.0215   1.0000
  12.000   1.0627   0.02853   0.02277   0.0395   0.0213   1.0000
  12.250   1.0695   0.02961   0.02399   0.0419   0.0211   1.0000
  12.500   1.0753   0.03081   0.02532   0.0442   0.0207   1.0000
  12.750   1.0798   0.03224   0.02689   0.0464   0.0204   1.0000
  13.000   1.0836   0.03370   0.02848   0.0483   0.0201   1.0000
  13.250   1.0868   0.03519   0.03009   0.0500   0.0197   1.0000
  13.500   1.0879   0.03704   0.03207   0.0515   0.0194   1.0000
  13.750   1.0874   0.03913   0.03430   0.0527   0.0192   1.0000
  14.000   1.0873   0.04117   0.03646   0.0536   0.0189   1.0000
  14.250   1.0870   0.04334   0.03872   0.0540   0.0186   1.0000
  14.500   1.0840   0.04602   0.04152   0.0542   0.0184   1.0000
  14.750   1.0805   0.04889   0.04450   0.0539   0.0182   1.0000
  15.000   1.0729   0.05247   0.04822   0.0532   0.0181   1.0000
  15.250   1.0670   0.05599   0.05184   0.0521   0.0179   1.0000
  15.500   1.0551   0.06054   0.05654   0.0504   0.0178   1.0000
  15.750   1.0411   0.06566   0.06179   0.0481   0.0176   1.0000
  16.000   1.0252   0.07147   0.06778   0.0449   0.0177   1.0000
  16.250   1.0037   0.07854   0.07502   0.0409   0.0176   1.0000
  16.500   0.9794   0.08674   0.08343   0.0357   0.0177   1.0000
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