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NACA 25112 (naca25112-jf) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 25112 (naca25112-jf)
Reynolds number: 500,000
Max Cl/Cd: 85.91 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca25112-jf-500000-n5.txt
Download as CSV file: xf-naca25112-jf-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 25112                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -1.0996   0.04620   0.04282  -0.0387   1.0000   0.0141
 -14.000  -1.1155   0.04219   0.03861  -0.0383   1.0000   0.0142
 -13.750  -1.1236   0.03938   0.03561  -0.0367   1.0000   0.0143
 -13.500  -1.1277   0.03710   0.03316  -0.0345   1.0000   0.0144
 -13.250  -1.1283   0.03518   0.03107  -0.0319   1.0000   0.0146
 -13.000  -1.1241   0.03342   0.02914  -0.0296   1.0000   0.0148
 -12.750  -1.1158   0.03176   0.02729  -0.0278   1.0000   0.0150
 -12.500  -1.1049   0.03020   0.02555  -0.0261   1.0000   0.0152
 -12.250  -1.0921   0.02875   0.02392  -0.0245   1.0000   0.0155
 -12.000  -1.0775   0.02740   0.02238  -0.0230   1.0000   0.0157
 -11.750  -1.0611   0.02618   0.02098  -0.0217   1.0000   0.0159
 -11.500  -1.0439   0.02504   0.01969  -0.0204   1.0000   0.0162
 -11.250  -1.0252   0.02410   0.01869  -0.0193   1.0000   0.0165
 -11.000  -1.0048   0.02333   0.01785  -0.0183   1.0000   0.0169
 -10.750  -0.9835   0.02262   0.01707  -0.0174   1.0000   0.0172
 -10.500  -0.9620   0.02190   0.01627  -0.0165   1.0000   0.0176
 -10.250  -0.9404   0.02115   0.01541  -0.0156   1.0000   0.0180
 -10.000  -0.9186   0.02039   0.01455  -0.0147   1.0000   0.0184
  -9.750  -0.8964   0.01967   0.01371  -0.0138   1.0000   0.0188
  -9.500  -0.8737   0.01899   0.01292  -0.0130   1.0000   0.0192
  -9.250  -0.8516   0.01827   0.01215  -0.0120   1.0000   0.0197
  -9.000  -0.8287   0.01770   0.01155  -0.0112   1.0000   0.0201
  -8.750  -0.8052   0.01722   0.01103  -0.0104   1.0000   0.0206
  -8.500  -0.7818   0.01676   0.01053  -0.0096   1.0000   0.0213
  -8.250  -0.7520   0.01626   0.00995  -0.0101   0.9906   0.0221
  -8.000  -0.7193   0.01574   0.00935  -0.0112   0.9738   0.0228
  -7.750  -0.6874   0.01516   0.00873  -0.0122   0.9531   0.0235
  -7.500  -0.6583   0.01475   0.00826  -0.0124   0.9261   0.0243
  -7.250  -0.6334   0.01442   0.00783  -0.0115   0.8956   0.0251
  -7.000  -0.6097   0.01413   0.00741  -0.0105   0.8658   0.0260
  -6.750  -0.5855   0.01387   0.00699  -0.0095   0.8367   0.0269
  -6.500  -0.5612   0.01356   0.00658  -0.0086   0.8094   0.0280
  -6.250  -0.5360   0.01333   0.00625  -0.0079   0.7842   0.0291
  -6.000  -0.5105   0.01310   0.00590  -0.0073   0.7593   0.0303
  -5.750  -0.4847   0.01289   0.00555  -0.0067   0.7364   0.0315
  -5.500  -0.4589   0.01262   0.00521  -0.0062   0.7149   0.0329
  -5.250  -0.4326   0.01244   0.00494  -0.0058   0.6937   0.0347
  -5.000  -0.4062   0.01227   0.00466  -0.0054   0.6737   0.0365
  -4.750  -0.3799   0.01206   0.00438  -0.0050   0.6553   0.0383
  -4.500  -0.3533   0.01188   0.00414  -0.0046   0.6375   0.0405
  -4.250  -0.3264   0.01174   0.00391  -0.0043   0.6204   0.0429
  -4.000  -0.2997   0.01156   0.00369  -0.0040   0.6049   0.0457
  -3.750  -0.2727   0.01143   0.00349  -0.0037   0.5901   0.0488
  -3.500  -0.2457   0.01129   0.00330  -0.0034   0.5760   0.0521
  -3.250  -0.2187   0.01116   0.00313  -0.0032   0.5630   0.0564
  -2.750  -0.1643   0.01092   0.00283  -0.0027   0.5386   0.0663
  -2.500  -0.1370   0.01081   0.00269  -0.0025   0.5280   0.0724
  -2.250  -0.1096   0.01072   0.00257  -0.0023   0.5177   0.0794
  -2.000  -0.0823   0.01061   0.00247  -0.0021   0.5080   0.0886
  -1.750  -0.0549   0.01052   0.00237  -0.0019   0.4987   0.0988
  -1.500  -0.0275   0.01042   0.00228  -0.0018   0.4901   0.1116
  -1.250  -0.0001   0.01033   0.00221  -0.0016   0.4818   0.1275
  -1.000   0.0272   0.01021   0.00214  -0.0014   0.4736   0.1486
  -0.750   0.0543   0.01010   0.00208  -0.0012   0.4661   0.1773
  -0.500   0.0811   0.00989   0.00202  -0.0010   0.4588   0.2244
  -0.250   0.1042   0.00929   0.00190  -0.0004   0.4516   0.3792
   0.000   0.1167   0.00795   0.00180   0.0025   0.4460   0.7231
   0.250   0.1396   0.00768   0.00187   0.0040   0.4393   0.8217
   0.500   0.1663   0.00768   0.00197   0.0047   0.4326   0.8718
   0.750   0.1952   0.00774   0.00207   0.0049   0.4259   0.9011
   1.000   0.2245   0.00785   0.00216   0.0049   0.4191   0.9209
   1.250   0.2550   0.00797   0.00225   0.0046   0.4127   0.9351
   1.500   0.2860   0.00810   0.00234   0.0042   0.4057   0.9464
   1.750   0.3160   0.00826   0.00245   0.0040   0.3995   0.9576
   2.000   0.3543   0.00844   0.00260   0.0020   0.3922   0.9659
   2.250   0.3856   0.00858   0.00268   0.0014   0.3855   0.9713
   2.500   0.4200   0.00866   0.00274   0.0000   0.3790   0.9726
   2.750   0.4538   0.00877   0.00280  -0.0013   0.3719   0.9741
   3.000   0.4869   0.00887   0.00286  -0.0025   0.3656   0.9759
   3.250   0.5190   0.00897   0.00294  -0.0034   0.3585   0.9781
   3.500   0.5495   0.00909   0.00302  -0.0040   0.3519   0.9809
   3.750   0.5798   0.00919   0.00310  -0.0046   0.3453   0.9834
   4.000   0.6132   0.00931   0.00319  -0.0059   0.3379   0.9846
   4.250   0.6462   0.00942   0.00329  -0.0070   0.3311   0.9860
   4.500   0.6785   0.00955   0.00339  -0.0081   0.3235   0.9876
   4.750   0.7103   0.00967   0.00351  -0.0091   0.3165   0.9894
   5.000   0.7413   0.00982   0.00363  -0.0099   0.3086   0.9913
   5.250   0.7719   0.00996   0.00378  -0.0106   0.3012   0.9932
   5.500   0.8034   0.01012   0.00392  -0.0115   0.2925   0.9945
   5.750   0.8354   0.01028   0.00406  -0.0126   0.2841   0.9958
   6.000   0.8668   0.01048   0.00423  -0.0136   0.2745   0.9972
   6.250   0.8980   0.01065   0.00441  -0.0145   0.2642   0.9986
   6.500   0.9289   0.01087   0.00460  -0.0154   0.2532   0.9998
   6.750   0.9532   0.01111   0.00481  -0.0149   0.2423   1.0000
   7.000   0.9758   0.01137   0.00503  -0.0141   0.2306   1.0000
   7.250   0.9983   0.01162   0.00527  -0.0132   0.2187   1.0000
   7.500   1.0204   0.01191   0.00553  -0.0123   0.2066   1.0000
   7.750   1.0420   0.01224   0.00582  -0.0114   0.1938   1.0000
   8.000   1.0631   0.01259   0.00613  -0.0103   0.1807   1.0000
   8.250   1.0837   0.01298   0.00648  -0.0093   0.1670   1.0000
   8.500   1.1038   0.01340   0.00685  -0.0081   0.1530   1.0000
   8.750   1.1233   0.01387   0.00726  -0.0069   0.1386   1.0000
   9.000   1.1422   0.01437   0.00771  -0.0056   0.1246   1.0000
   9.250   1.1606   0.01490   0.00819  -0.0042   0.1110   1.0000
   9.500   1.1785   0.01547   0.00870  -0.0028   0.0984   1.0000
   9.750   1.1958   0.01605   0.00925  -0.0013   0.0870   1.0000
  10.000   1.2127   0.01665   0.00982   0.0002   0.0771   1.0000
  10.250   1.2294   0.01727   0.01041   0.0016   0.0684   1.0000
  10.500   1.2456   0.01793   0.01105   0.0031   0.0610   1.0000
  10.750   1.2617   0.01858   0.01170   0.0046   0.0546   1.0000
  11.000   1.2778   0.01923   0.01237   0.0060   0.0496   1.0000
  11.250   1.2922   0.01998   0.01312   0.0075   0.0451   1.0000
  11.500   1.3069   0.02068   0.01386   0.0090   0.0415   1.0000
  11.750   1.3178   0.02150   0.01470   0.0109   0.0385   1.0000
  12.000   1.3276   0.02230   0.01556   0.0130   0.0361   1.0000
  12.250   1.3354   0.02333   0.01662   0.0148   0.0337   1.0000
  12.500   1.3439   0.02445   0.01781   0.0163   0.0318   1.0000
  12.750   1.3519   0.02575   0.01918   0.0173   0.0301   1.0000
  13.000   1.3580   0.02737   0.02085   0.0181   0.0286   1.0000
  13.250   1.3636   0.02920   0.02276   0.0184   0.0274   1.0000
  13.500   1.3696   0.03117   0.02483   0.0184   0.0262   1.0000
  13.750   1.3734   0.03350   0.02724   0.0182   0.0251   1.0000
  14.000   1.3750   0.03621   0.03003   0.0176   0.0241   1.0000
  14.250   1.3742   0.03928   0.03319   0.0169   0.0233   1.0000
  14.500   1.3748   0.04227   0.03628   0.0161   0.0226   1.0000
  14.750   1.3731   0.04555   0.03967   0.0152   0.0219   1.0000
  15.000   1.3693   0.04912   0.04334   0.0142   0.0213   1.0000
  15.250   1.3635   0.05295   0.04727   0.0131   0.0208   1.0000
  15.500   1.3559   0.05701   0.05142   0.0119   0.0204   1.0000
  15.750   1.3466   0.06134   0.05585   0.0106   0.0200   1.0000
  16.000   1.3357   0.06591   0.06051   0.0093   0.0197   1.0000
  16.250   1.3270   0.07036   0.06506   0.0078   0.0193   1.0000
  16.500   1.3191   0.07477   0.06957   0.0063   0.0190   1.0000
  16.750   1.3107   0.07932   0.07422   0.0048   0.0187   1.0000
  17.000   1.3023   0.08397   0.07897   0.0031   0.0183   1.0000
  17.250   1.2936   0.08871   0.08381   0.0014   0.0180   1.0000
  17.500   1.2846   0.09354   0.08873  -0.0004   0.0176   1.0000
  17.750   1.2756   0.09848   0.09375  -0.0023   0.0173   1.0000
  18.000   1.2663   0.10349   0.09885  -0.0043   0.0170   1.0000
  18.250   1.2569   0.10856   0.10400  -0.0063   0.0167   1.0000
  18.500   1.2469   0.11382   0.10933  -0.0085   0.0164   1.0000
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