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J5012 12% (j5012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: J5012 12% (j5012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.71 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-j5012-il-1000000.txt
Download as CSV file: xf-j5012-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.9944   0.13179   0.12947  -0.0062   1.0000   0.0117
 -19.000  -1.0187   0.12268   0.12025  -0.0112   1.0000   0.0117
 -18.750  -1.0472   0.11302   0.11045  -0.0164   1.0000   0.0117
 -18.500  -1.0728   0.10428   0.10158  -0.0210   1.0000   0.0116
 -18.250  -1.0950   0.09633   0.09350  -0.0252   1.0000   0.0116
 -18.000  -1.1165   0.08872   0.08576  -0.0293   1.0000   0.0117
 -17.750  -1.1366   0.08157   0.07846  -0.0330   1.0000   0.0116
 -17.500  -1.1497   0.07562   0.07243  -0.0362   1.0000   0.0118
 -17.250  -1.1622   0.06998   0.06668  -0.0392   1.0000   0.0118
 -17.000  -1.1746   0.06450   0.06108  -0.0420   1.0000   0.0119
 -16.750  -1.1865   0.05937   0.05582  -0.0444   1.0000   0.0119
 -16.500  -1.1959   0.05474   0.05108  -0.0465   1.0000   0.0121
 -16.250  -1.1972   0.05136   0.04762  -0.0480   1.0000   0.0122
 -16.000  -1.2062   0.04725   0.04337  -0.0494   1.0000   0.0123
 -15.750  -1.2099   0.04395   0.03996  -0.0502   1.0000   0.0124
 -15.500  -1.2104   0.04118   0.03709  -0.0507   1.0000   0.0125
 -15.250  -1.2064   0.03903   0.03485  -0.0509   1.0000   0.0129
 -15.000  -1.2066   0.03658   0.03229  -0.0507   1.0000   0.0129
 -14.750  -1.2063   0.03434   0.02994  -0.0502   1.0000   0.0131
 -14.500  -1.2010   0.03267   0.02818  -0.0495   1.0000   0.0133
 -14.250  -1.1942   0.03122   0.02664  -0.0487   1.0000   0.0134
 -14.000  -1.1911   0.02955   0.02487  -0.0473   1.0000   0.0135
 -13.750  -1.1839   0.02830   0.02352  -0.0460   1.0000   0.0136
 -13.500  -1.1849   0.02650   0.02160  -0.0437   1.0000   0.0138
 -13.250  -1.1857   0.02485   0.01985  -0.0411   1.0000   0.0140
 -13.000  -1.1847   0.02347   0.01839  -0.0383   1.0000   0.0144
 -12.750  -1.1786   0.02248   0.01734  -0.0357   1.0000   0.0146
 -12.500  -1.1697   0.02172   0.01653  -0.0333   1.0000   0.0149
 -12.250  -1.1593   0.02111   0.01587  -0.0310   1.0000   0.0153
 -12.000  -1.1500   0.02049   0.01521  -0.0282   1.0000   0.0156
 -11.750  -1.1423   0.01990   0.01456  -0.0250   1.0000   0.0158
 -11.500  -1.1353   0.01940   0.01401  -0.0215   1.0000   0.0162
 -11.250  -1.1283   0.01894   0.01349  -0.0179   1.0000   0.0165
 -11.000  -1.1179   0.01842   0.01291  -0.0149   1.0000   0.0168
 -10.750  -1.1057   0.01798   0.01242  -0.0122   1.0000   0.0170
 -10.500  -1.0929   0.01759   0.01198  -0.0095   1.0000   0.0172
 -10.250  -1.0881   0.01678   0.01109  -0.0055   1.0000   0.0177
 -10.000  -1.0804   0.01612   0.01038  -0.0019   1.0000   0.0183
  -9.750  -1.0686   0.01567   0.00992   0.0010   1.0000   0.0189
  -9.500  -1.0550   0.01533   0.00955   0.0035   1.0000   0.0195
  -9.250  -1.0416   0.01496   0.00915   0.0062   1.0000   0.0200
  -9.000  -1.0232   0.01460   0.00874   0.0077   0.9997   0.0207
  -8.750  -0.9917   0.01421   0.00831   0.0066   0.9983   0.0213
  -8.500  -0.9613   0.01364   0.00769   0.0057   0.9966   0.0224
  -8.250  -0.9299   0.01316   0.00721   0.0045   0.9949   0.0242
  -8.000  -0.8971   0.01282   0.00684   0.0032   0.9937   0.0259
  -7.750  -0.8685   0.01238   0.00639   0.0027   0.9912   0.0282
  -7.500  -0.8379   0.01199   0.00603   0.0018   0.9888   0.0317
  -7.250  -0.8062   0.01159   0.00564   0.0008   0.9868   0.0364
  -7.000  -0.7729   0.01131   0.00536  -0.0006   0.9852   0.0405
  -6.750  -0.7396   0.01091   0.00502  -0.0021   0.9839   0.0475
  -6.500  -0.7053   0.01058   0.00471  -0.0037   0.9828   0.0547
  -6.250  -0.6788   0.01029   0.00444  -0.0035   0.9785   0.0618
  -6.000  -0.6475   0.00996   0.00417  -0.0044   0.9758   0.0720
  -5.750  -0.6149   0.00960   0.00389  -0.0057   0.9737   0.0870
  -5.500  -0.5814   0.00923   0.00362  -0.0071   0.9721   0.1052
  -5.250  -0.5466   0.00887   0.00336  -0.0088   0.9708   0.1265
  -5.000  -0.5142   0.00851   0.00311  -0.0100   0.9685   0.1528
  -4.750  -0.4880   0.00812   0.00288  -0.0098   0.9628   0.1856
  -4.500  -0.4572   0.00771   0.00264  -0.0107   0.9589   0.2251
  -4.250  -0.4243   0.00734   0.00242  -0.0119   0.9558   0.2623
  -4.000  -0.4001   0.00705   0.00226  -0.0112   0.9478   0.2963
  -3.750  -0.3706   0.00674   0.00208  -0.0116   0.9419   0.3351
  -3.500  -0.3460   0.00647   0.00194  -0.0110   0.9334   0.3726
  -3.250  -0.3181   0.00622   0.00180  -0.0110   0.9258   0.4078
  -3.000  -0.2939   0.00602   0.00169  -0.0102   0.9157   0.4396
  -2.750  -0.2682   0.00583   0.00158  -0.0097   0.9062   0.4740
  -2.500  -0.2438   0.00563   0.00148  -0.0089   0.8954   0.5102
  -2.250  -0.2196   0.00548   0.00141  -0.0080   0.8839   0.5414
  -2.000  -0.1950   0.00535   0.00134  -0.0072   0.8723   0.5709
  -1.750  -0.1701   0.00525   0.00128  -0.0064   0.8604   0.5979
  -1.500  -0.1458   0.00515   0.00123  -0.0055   0.8475   0.6236
  -1.250  -0.1216   0.00507   0.00119  -0.0046   0.8337   0.6486
  -1.000  -0.0973   0.00500   0.00116  -0.0037   0.8194   0.6726
  -0.750  -0.0729   0.00495   0.00113  -0.0028   0.8043   0.6944
  -0.500  -0.0488   0.00492   0.00111  -0.0018   0.7881   0.7157
  -0.250  -0.0244   0.00490   0.00110  -0.0009   0.7712   0.7353
   0.000   0.0000   0.00491   0.00110   0.0000   0.7536   0.7537
   0.250   0.0244   0.00491   0.00110   0.0009   0.7351   0.7709
   0.500   0.0487   0.00492   0.00111   0.0018   0.7154   0.7879
   0.750   0.0729   0.00495   0.00113   0.0028   0.6944   0.8042
   1.000   0.0972   0.00500   0.00116   0.0037   0.6721   0.8194
   1.250   0.1216   0.00507   0.00119   0.0046   0.6488   0.8336
   1.500   0.1458   0.00515   0.00123   0.0055   0.6236   0.8476
   1.750   0.1701   0.00524   0.00128   0.0064   0.5981   0.8604
   2.000   0.1948   0.00535   0.00134   0.0072   0.5701   0.8724
   2.250   0.2194   0.00548   0.00141   0.0080   0.5407   0.8840
   2.500   0.2437   0.00563   0.00148   0.0089   0.5103   0.8954
   2.750   0.2682   0.00583   0.00158   0.0097   0.4742   0.9062
   3.000   0.2938   0.00603   0.00169   0.0102   0.4391   0.9158
   3.250   0.3181   0.00622   0.00179   0.0110   0.4078   0.9258
   3.500   0.3460   0.00647   0.00194   0.0110   0.3726   0.9334
   3.750   0.3706   0.00674   0.00208   0.0116   0.3354   0.9419
   4.000   0.4001   0.00705   0.00226   0.0112   0.2967   0.9478
   4.250   0.4242   0.00733   0.00242   0.0120   0.2631   0.9557
   4.500   0.4571   0.00772   0.00264   0.0107   0.2239   0.9589
   4.750   0.4882   0.00810   0.00287   0.0098   0.1876   0.9628
   5.250   0.5467   0.00887   0.00336   0.0088   0.1264   0.9708
   5.500   0.5814   0.00923   0.00362   0.0071   0.1053   0.9721
   5.750   0.6149   0.00960   0.00389   0.0057   0.0870   0.9737
   6.000   0.6475   0.00996   0.00417   0.0044   0.0717   0.9758
   6.250   0.6788   0.01029   0.00444   0.0035   0.0618   0.9785
   6.500   0.7053   0.01058   0.00471   0.0037   0.0547   0.9828
   6.750   0.7396   0.01091   0.00501   0.0021   0.0474   0.9838
   7.000   0.7730   0.01130   0.00535   0.0006   0.0404   0.9852
   7.250   0.8062   0.01160   0.00564  -0.0008   0.0362   0.9868
   7.500   0.8379   0.01199   0.00602  -0.0019   0.0317   0.9888
   7.750   0.8685   0.01238   0.00639  -0.0027   0.0282   0.9912
   8.000   0.8972   0.01281   0.00683  -0.0032   0.0257   0.9937
   8.250   0.9299   0.01315   0.00720  -0.0045   0.0241   0.9949
   8.500   0.9614   0.01362   0.00767  -0.0057   0.0226   0.9965
   8.750   0.9917   0.01421   0.00831  -0.0066   0.0213   0.9983
   9.000   1.0232   0.01461   0.00874  -0.0078   0.0206   0.9997
   9.250   1.0414   0.01498   0.00916  -0.0061   0.0199   1.0000
   9.500   1.0550   0.01533   0.00954  -0.0035   0.0193   1.0000
   9.750   1.0684   0.01569   0.00992  -0.0009   0.0187   1.0000
  10.000   1.0798   0.01615   0.01041   0.0020   0.0182   1.0000
  10.250   1.0878   0.01679   0.01110   0.0055   0.0176   1.0000
  10.500   1.0935   0.01755   0.01194   0.0094   0.0172   1.0000
  10.750   1.1049   0.01802   0.01247   0.0123   0.0170   1.0000
  11.000   1.1166   0.01849   0.01299   0.0151   0.0168   1.0000
  11.250   1.1275   0.01897   0.01353   0.0180   0.0165   1.0000
  11.500   1.1336   0.01947   0.01409   0.0218   0.0163   1.0000
  11.750   1.1410   0.01997   0.01463   0.0252   0.0160   1.0000
  12.000   1.1488   0.02057   0.01529   0.0284   0.0157   1.0000
  12.250   1.1588   0.02115   0.01592   0.0310   0.0153   1.0000
  12.500   1.1688   0.02179   0.01661   0.0335   0.0150   1.0000
  12.750   1.1769   0.02261   0.01748   0.0360   0.0147   1.0000
  13.000   1.1855   0.02344   0.01837   0.0382   0.0145   1.0000
  13.250   1.1898   0.02461   0.01961   0.0407   0.0142   1.0000
  13.500   1.1832   0.02666   0.02177   0.0438   0.0138   1.0000
  13.750   1.1803   0.02864   0.02388   0.0462   0.0137   1.0000
  14.000   1.1899   0.02970   0.02502   0.0473   0.0136   1.0000
  14.250   1.1968   0.03105   0.02647   0.0484   0.0134   1.0000
  14.500   1.2004   0.03279   0.02830   0.0495   0.0133   1.0000
  14.750   1.2048   0.03455   0.03016   0.0502   0.0132   1.0000
  15.000   1.2077   0.03656   0.03227   0.0506   0.0130   1.0000
  15.250   1.2095   0.03881   0.03462   0.0507   0.0128   1.0000
  15.500   1.2137   0.04092   0.03682   0.0505   0.0125   1.0000
  15.750   1.2103   0.04402   0.04004   0.0501   0.0125   1.0000
  16.000   1.2096   0.04697   0.04308   0.0492   0.0123   1.0000
  16.250   1.2060   0.05045   0.04666   0.0480   0.0121   1.0000
  16.500   1.1991   0.05450   0.05083   0.0464   0.0120   1.0000
  16.750   1.1894   0.05915   0.05560   0.0443   0.0119   1.0000
  17.000   1.1787   0.06413   0.06071   0.0419   0.0119   1.0000
  17.250   1.1650   0.06980   0.06650   0.0390   0.0118   1.0000
  17.500   1.1578   0.07468   0.07145   0.0363   0.0116   1.0000
  17.750   1.1383   0.08156   0.07847   0.0327   0.0117   1.0000
  18.000   1.1205   0.08839   0.08542   0.0291   0.0117   1.0000
  18.250   1.0991   0.09597   0.09312   0.0251   0.0116   1.0000
  18.500   1.0744   0.10439   0.10169   0.0206   0.0117   1.0000
  18.750   1.0513   0.11268   0.11010   0.0162   0.0116   1.0000
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