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KC-135 BL52.44 AIRFOIL (kc135a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: KC-135 BL52.44 AIRFOIL (kc135a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 82.52 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-kc135a-il-1000000-n5.txt
Download as CSV file: xf-kc135a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: KC-135 BL52.44 AIRFOIL                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -1.0177   0.09739   0.09455  -0.0347   1.0000   0.0100
 -18.750  -1.0437   0.08883   0.08582  -0.0395   1.0000   0.0100
 -18.500  -1.0694   0.08084   0.07767  -0.0438   1.0000   0.0100
 -18.250  -1.0761   0.07616   0.07288  -0.0461   1.0000   0.0100
 -18.000  -1.0948   0.06992   0.06649  -0.0491   1.0000   0.0100
 -17.750  -1.1101   0.06451   0.06094  -0.0515   1.0000   0.0101
 -17.500  -1.1210   0.05991   0.05622  -0.0532   1.0000   0.0102
 -17.250  -1.1259   0.05626   0.05246  -0.0545   1.0000   0.0102
 -17.000  -1.1322   0.05263   0.04872  -0.0555   1.0000   0.0102
 -16.750  -1.1380   0.04917   0.04515  -0.0564   1.0000   0.0103
 -16.500  -1.1386   0.04642   0.04231  -0.0568   1.0000   0.0103
 -16.250  -1.1385   0.04383   0.03964  -0.0572   1.0000   0.0104
 -16.000  -1.1371   0.04142   0.03713  -0.0573   1.0000   0.0104
 -15.750  -1.1349   0.03914   0.03478  -0.0573   1.0000   0.0105
 -15.500  -1.1305   0.03713   0.03270  -0.0573   1.0000   0.0106
 -15.250  -1.1232   0.03544   0.03095  -0.0571   1.0000   0.0107
 -15.000  -1.1190   0.03349   0.02890  -0.0567   1.0000   0.0107
 -14.750  -1.1118   0.03187   0.02721  -0.0563   1.0000   0.0108
 -14.500  -1.1036   0.03037   0.02564  -0.0558   1.0000   0.0108
 -14.250  -1.0950   0.02897   0.02417  -0.0551   1.0000   0.0109
 -14.000  -1.0837   0.02783   0.02299  -0.0544   1.0000   0.0111
 -13.750  -1.0753   0.02651   0.02159  -0.0535   1.0000   0.0112
 -13.500  -1.0650   0.02539   0.02042  -0.0524   1.0000   0.0112
 -13.250  -1.0535   0.02443   0.01941  -0.0514   1.0000   0.0114
 -13.000  -1.0434   0.02342   0.01833  -0.0500   1.0000   0.0114
 -12.750  -1.0327   0.02251   0.01737  -0.0485   1.0000   0.0116
 -12.500  -1.0231   0.02160   0.01639  -0.0467   1.0000   0.0116
 -12.250  -1.0123   0.02084   0.01558  -0.0449   1.0000   0.0117
 -12.000  -1.0022   0.02012   0.01481  -0.0427   1.0000   0.0118
 -11.750  -0.9924   0.01947   0.01411  -0.0403   1.0000   0.0119
 -11.500  -0.9819   0.01884   0.01343  -0.0379   0.9917   0.0120
 -11.250  -0.9446   0.01803   0.01257  -0.0409   0.9726   0.0121
 -11.000  -0.8876   0.01709   0.01155  -0.0481   0.9519   0.0123
 -10.750  -0.8318   0.01633   0.01063  -0.0549   0.9077   0.0124
 -10.500  -0.8206   0.01590   0.00997  -0.0522   0.8499   0.0126
 -10.250  -0.8112   0.01557   0.00947  -0.0490   0.8118   0.0128
 -10.000  -0.7999   0.01525   0.00903  -0.0461   0.7872   0.0130
  -9.750  -0.7869   0.01496   0.00865  -0.0435   0.7695   0.0132
  -9.500  -0.7704   0.01465   0.00826  -0.0416   0.7556   0.0134
  -9.250  -0.7524   0.01433   0.00788  -0.0399   0.7436   0.0136
  -9.000  -0.7335   0.01402   0.00751  -0.0384   0.7333   0.0140
  -8.750  -0.7136   0.01373   0.00716  -0.0371   0.7238   0.0142
  -8.500  -0.6933   0.01344   0.00681  -0.0358   0.7160   0.0145
  -8.250  -0.6721   0.01316   0.00648  -0.0347   0.7084   0.0149
  -8.000  -0.6508   0.01289   0.00615  -0.0335   0.7014   0.0152
  -7.750  -0.6290   0.01260   0.00585  -0.0325   0.6951   0.0159
  -7.500  -0.6066   0.01235   0.00557  -0.0316   0.6884   0.0165
  -7.250  -0.5837   0.01212   0.00530  -0.0307   0.6825   0.0172
  -7.000  -0.5603   0.01189   0.00504  -0.0299   0.6765   0.0179
  -6.750  -0.5369   0.01167   0.00478  -0.0291   0.6707   0.0188
  -6.500  -0.5130   0.01147   0.00456  -0.0284   0.6657   0.0197
  -6.250  -0.4884   0.01127   0.00435  -0.0278   0.6610   0.0209
  -6.000  -0.4638   0.01108   0.00414  -0.0273   0.6559   0.0221
  -5.750  -0.4393   0.01090   0.00394  -0.0267   0.6509   0.0235
  -5.500  -0.4141   0.01073   0.00375  -0.0262   0.6466   0.0247
  -5.250  -0.3886   0.01057   0.00357  -0.0257   0.6418   0.0260
  -5.000  -0.3635   0.01040   0.00340  -0.0252   0.6365   0.0277
  -4.750  -0.3380   0.01027   0.00323  -0.0248   0.6312   0.0292
  -4.500  -0.3120   0.01012   0.00307  -0.0244   0.6265   0.0308
  -4.250  -0.2862   0.00997   0.00292  -0.0240   0.6214   0.0330
  -4.000  -0.2603   0.00985   0.00278  -0.0237   0.6164   0.0353
  -3.750  -0.2343   0.00970   0.00265  -0.0233   0.6120   0.0392
  -3.500  -0.2080   0.00957   0.00253  -0.0230   0.6071   0.0438
  -3.000  -0.1559   0.00931   0.00228  -0.0223   0.5972   0.0573
  -2.750  -0.1301   0.00913   0.00216  -0.0219   0.5921   0.0728
  -2.500  -0.1059   0.00884   0.00201  -0.0213   0.5868   0.1182
  -2.250  -0.0974   0.00733   0.00149  -0.0182   0.5822   0.3921
  -2.000  -0.0733   0.00704   0.00141  -0.0176   0.5782   0.4516
  -1.750  -0.0471   0.00692   0.00137  -0.0172   0.5735   0.4821
  -1.500  -0.0204   0.00685   0.00135  -0.0170   0.5684   0.5073
  -1.250   0.0066   0.00682   0.00133  -0.0168   0.5632   0.5240
  -1.000   0.0342   0.00680   0.00132  -0.0167   0.5576   0.5342
  -0.750   0.0615   0.00679   0.00132  -0.0165   0.5520   0.5463
  -0.250   0.1169   0.00679   0.00132  -0.0164   0.5427   0.5641
   0.000   0.1448   0.00680   0.00132  -0.0164   0.5377   0.5687
   0.250   0.1725   0.00685   0.00132  -0.0163   0.5310   0.5722
   0.500   0.2003   0.00687   0.00132  -0.0163   0.5213   0.5757
   0.750   0.2274   0.00691   0.00133  -0.0161   0.5121   0.5797
   1.000   0.2552   0.00693   0.00135  -0.0161   0.5052   0.5836
   1.500   0.3108   0.00701   0.00140  -0.0161   0.4932   0.5907
   1.750   0.3383   0.00704   0.00143  -0.0160   0.4871   0.5947
   2.000   0.3655   0.00708   0.00147  -0.0159   0.4810   0.5991
   2.250   0.3932   0.00711   0.00150  -0.0159   0.4739   0.6033
   2.500   0.4204   0.00718   0.00155  -0.0158   0.4666   0.6072
   2.750   0.4479   0.00723   0.00160  -0.0157   0.4583   0.6110
   3.000   0.4745   0.00729   0.00166  -0.0155   0.4487   0.6159
   3.250   0.5013   0.00736   0.00172  -0.0153   0.4366   0.6211
   3.500   0.5278   0.00747   0.00180  -0.0151   0.4216   0.6257
   3.750   0.5529   0.00762   0.00189  -0.0147   0.4000   0.6306
   4.000   0.5770   0.00784   0.00202  -0.0140   0.3727   0.6363
   4.250   0.6005   0.00810   0.00218  -0.0133   0.3442   0.6423
   4.500   0.6235   0.00837   0.00236  -0.0126   0.3166   0.6487
   4.750   0.6468   0.00862   0.00254  -0.0118   0.2932   0.6562
   5.250   0.6929   0.00910   0.00292  -0.0103   0.2516   0.6724
   5.500   0.7161   0.00932   0.00310  -0.0096   0.2360   0.6822
   5.750   0.7393   0.00950   0.00329  -0.0088   0.2237   0.6944
   6.000   0.7619   0.00970   0.00349  -0.0079   0.2115   0.7075
   6.250   0.7844   0.00988   0.00369  -0.0071   0.1998   0.7224
   6.500   0.8055   0.01009   0.00391  -0.0059   0.1856   0.7414
   6.750   0.8246   0.01035   0.00416  -0.0045   0.1684   0.7655
   7.000   0.8432   0.01057   0.00441  -0.0029   0.1539   0.7945
   7.250   0.8612   0.01074   0.00466  -0.0011   0.1422   0.8307
   7.500   0.8794   0.01088   0.00492   0.0007   0.1338   0.8743
   7.750   0.9051   0.01111   0.00525   0.0008   0.1234   0.9248
   8.000   0.9541   0.01160   0.00572  -0.0045   0.1094   0.9563
   8.250   0.9985   0.01210   0.00617  -0.0087   0.0972   0.9704
   8.500   1.0340   0.01257   0.00659  -0.0111   0.0868   0.9800
   8.750   1.0631   0.01301   0.00700  -0.0120   0.0779   0.9887
   9.000   1.0866   0.01348   0.00743  -0.0118   0.0694   0.9985
   9.250   1.1061   0.01397   0.00787  -0.0108   0.0610   1.0000
   9.500   1.1124   0.01438   0.00825  -0.0070   0.0544   1.0000
   9.750   1.1179   0.01484   0.00869  -0.0032   0.0474   1.0000
  10.000   1.1254   0.01537   0.00918   0.0000   0.0411   1.0000
  10.250   1.1347   0.01592   0.00973   0.0027   0.0366   1.0000
  10.500   1.1452   0.01651   0.01031   0.0051   0.0329   1.0000
  10.750   1.1562   0.01714   0.01095   0.0072   0.0298   1.0000
  11.000   1.1674   0.01782   0.01164   0.0091   0.0276   1.0000
  11.250   1.1792   0.01854   0.01238   0.0107   0.0257   1.0000
  11.500   1.1916   0.01928   0.01315   0.0121   0.0244   1.0000
  11.750   1.2031   0.02014   0.01403   0.0135   0.0232   1.0000
  12.000   1.2149   0.02104   0.01496   0.0147   0.0219   1.0000
  12.250   1.2275   0.02194   0.01590   0.0157   0.0213   1.0000
  12.500   1.2395   0.02293   0.01692   0.0166   0.0206   1.0000
  12.750   1.2498   0.02408   0.01810   0.0175   0.0196   1.0000
  13.000   1.2604   0.02526   0.01932   0.0183   0.0190   1.0000
  13.250   1.2713   0.02646   0.02056   0.0190   0.0185   1.0000
  13.500   1.2822   0.02768   0.02183   0.0196   0.0180   1.0000
  13.750   1.2921   0.02900   0.02321   0.0201   0.0175   1.0000
  14.000   1.3011   0.03044   0.02469   0.0207   0.0171   1.0000
  14.250   1.3095   0.03194   0.02624   0.0211   0.0168   1.0000
  14.500   1.3162   0.03361   0.02795   0.0216   0.0161   1.0000
  14.750   1.3217   0.03542   0.02981   0.0220   0.0156   1.0000
  15.000   1.3294   0.03707   0.03152   0.0223   0.0154   1.0000
  15.250   1.3356   0.03886   0.03338   0.0226   0.0151   1.0000
  15.500   1.3413   0.04075   0.03534   0.0228   0.0147   1.0000
  15.750   1.3465   0.04275   0.03739   0.0228   0.0144   1.0000
  16.000   1.3504   0.04492   0.03962   0.0229   0.0141   1.0000
  16.250   1.3533   0.04721   0.04198   0.0228   0.0137   1.0000
  16.500   1.3558   0.04964   0.04446   0.0227   0.0135   1.0000
  16.750   1.3568   0.05230   0.04718   0.0224   0.0132   1.0000
  17.000   1.3559   0.05520   0.05016   0.0220   0.0129   1.0000
  17.250   1.3573   0.05791   0.05294   0.0215   0.0127   1.0000
  17.500   1.3579   0.06076   0.05588   0.0210   0.0125   1.0000
  17.750   1.3583   0.06369   0.05888   0.0204   0.0122   1.0000
  18.000   1.3563   0.06695   0.06223   0.0196   0.0121   1.0000
  18.250   1.3542   0.07027   0.06562   0.0188   0.0118   1.0000
  18.500   1.3496   0.07399   0.06943   0.0177   0.0116   1.0000
  18.750   1.3441   0.07791   0.07344   0.0165   0.0114   1.0000
  19.000   1.3378   0.08199   0.07760   0.0153   0.0113   1.0000
  19.250   1.3300   0.08634   0.08203   0.0138   0.0111   1.0000
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