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KC-135 BL52.44 AIRFOIL (kc135a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: KC-135 BL52.44 AIRFOIL (kc135a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.79 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-kc135a-il-1000000.txt
Download as CSV file: xf-kc135a-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.8239   0.08024   0.07796  -0.0455   1.0000   0.0145
 -15.500  -0.8770   0.06810   0.06554  -0.0525   1.0000   0.0144
 -15.250  -0.8979   0.06208   0.05934  -0.0555   1.0000   0.0145
 -15.000  -0.9356   0.05438   0.05138  -0.0584   1.0000   0.0143
 -14.750  -0.9631   0.04845   0.04519  -0.0598   1.0000   0.0143
 -14.500  -0.9756   0.04454   0.04109  -0.0603   1.0000   0.0143
 -14.250  -0.9866   0.04096   0.03731  -0.0603   1.0000   0.0144
 -14.000  -0.9926   0.03805   0.03421  -0.0598   1.0000   0.0145
 -13.750  -0.9973   0.03532   0.03129  -0.0589   1.0000   0.0146
 -13.500  -0.9955   0.03334   0.02918  -0.0579   1.0000   0.0146
 -13.250  -0.9924   0.03160   0.02730  -0.0566   1.0000   0.0147
 -13.000  -0.9882   0.02990   0.02548  -0.0551   1.0000   0.0147
 -12.750  -0.9818   0.02859   0.02405  -0.0536   1.0000   0.0149
 -12.500  -0.9751   0.02715   0.02248  -0.0518   1.0000   0.0149
 -12.250  -0.9664   0.02617   0.02141  -0.0500   1.0000   0.0150
 -12.000  -0.9573   0.02531   0.02045  -0.0479   1.0000   0.0151
 -11.750  -0.9515   0.02333   0.01833  -0.0456   1.0000   0.0154
 -11.500  -0.9426   0.02232   0.01727  -0.0433   1.0000   0.0156
 -11.250  -0.9335   0.02147   0.01638  -0.0408   1.0000   0.0157
 -11.000  -0.9253   0.02079   0.01566  -0.0379   1.0000   0.0158
 -10.750  -0.9193   0.02027   0.01511  -0.0344   1.0000   0.0160
 -10.500  -0.9165   0.01976   0.01456  -0.0301   1.0000   0.0161
 -10.250  -0.8831   0.01900   0.01377  -0.0320   0.9954   0.0164
 -10.000  -0.8538   0.01820   0.01292  -0.0331   0.9852   0.0167
  -9.750  -0.8198   0.01737   0.01205  -0.0351   0.9745   0.0170
  -9.500  -0.7769   0.01653   0.01114  -0.0390   0.9634   0.0173
  -9.250  -0.7269   0.01560   0.01013  -0.0444   0.9449   0.0176
  -9.000  -0.6881   0.01498   0.00936  -0.0472   0.9045   0.0180
  -8.750  -0.6702   0.01472   0.00890  -0.0454   0.8600   0.0182
  -8.500  -0.6599   0.01415   0.00817  -0.0424   0.8269   0.0185
  -8.250  -0.6456   0.01373   0.00764  -0.0400   0.8034   0.0191
  -8.000  -0.6276   0.01341   0.00723  -0.0382   0.7856   0.0194
  -7.750  -0.6078   0.01315   0.00689  -0.0368   0.7711   0.0199
  -7.500  -0.5869   0.01288   0.00657  -0.0356   0.7591   0.0205
  -7.250  -0.5650   0.01265   0.00626  -0.0345   0.7489   0.0213
  -7.000  -0.5454   0.01228   0.00582  -0.0330   0.7391   0.0221
  -6.750  -0.5241   0.01196   0.00548  -0.0319   0.7311   0.0232
  -6.500  -0.5011   0.01174   0.00522  -0.0310   0.7232   0.0242
  -6.250  -0.4769   0.01157   0.00499  -0.0303   0.7164   0.0255
  -6.000  -0.4552   0.01121   0.00462  -0.0292   0.7096   0.0273
  -5.750  -0.4311   0.01104   0.00442  -0.0285   0.7030   0.0291
  -5.500  -0.4063   0.01085   0.00419  -0.0279   0.6972   0.0305
  -5.250  -0.3829   0.01058   0.00392  -0.0271   0.6911   0.0328
  -5.000  -0.3579   0.01046   0.00375  -0.0266   0.6849   0.0347
  -4.750  -0.3331   0.01023   0.00351  -0.0260   0.6794   0.0369
  -4.500  -0.3079   0.01005   0.00333  -0.0255   0.6737   0.0394
  -4.250  -0.2822   0.00995   0.00317  -0.0250   0.6681   0.0416
  -4.000  -0.2571   0.00973   0.00297  -0.0245   0.6632   0.0459
  -3.750  -0.2312   0.00958   0.00282  -0.0241   0.6579   0.0505
  -3.500  -0.2059   0.00941   0.00265  -0.0236   0.6526   0.0580
  -3.250  -0.1819   0.00913   0.00247  -0.0229   0.6475   0.0822
  -3.000  -0.1742   0.00753   0.00187  -0.0197   0.6427   0.3417
  -2.750  -0.1554   0.00690   0.00169  -0.0182   0.6373   0.4655
  -2.500  -0.1300   0.00680   0.00165  -0.0177   0.6318   0.5023
  -2.250  -0.1028   0.00672   0.00163  -0.0175   0.6272   0.5248
  -2.000  -0.0752   0.00669   0.00160  -0.0173   0.6221   0.5398
  -1.750  -0.0482   0.00668   0.00159  -0.0171   0.6168   0.5516
  -1.500  -0.0207   0.00667   0.00158  -0.0170   0.6118   0.5634
  -1.250   0.0074   0.00668   0.00157  -0.0170   0.6061   0.5731
  -1.000   0.0347   0.00667   0.00155  -0.0168   0.6003   0.5799
  -0.750   0.0625   0.00669   0.00156  -0.0167   0.5952   0.5886
  -0.500   0.0902   0.00667   0.00155  -0.0167   0.5899   0.5968
  -0.250   0.1178   0.00669   0.00155  -0.0166   0.5847   0.6028
   0.000   0.1458   0.00672   0.00155  -0.0166   0.5798   0.6071
   0.250   0.1740   0.00671   0.00153  -0.0166   0.5736   0.6109
   0.750   0.2289   0.00672   0.00152  -0.0164   0.5584   0.6201
   1.000   0.2567   0.00675   0.00153  -0.0164   0.5524   0.6245
   1.250   0.2843   0.00678   0.00154  -0.0163   0.5469   0.6287
   1.500   0.3121   0.00676   0.00156  -0.0163   0.5417   0.6337
   1.750   0.3397   0.00679   0.00158  -0.0162   0.5364   0.6389
   2.000   0.3671   0.00685   0.00162  -0.0161   0.5310   0.6439
   2.250   0.3949   0.00683   0.00165  -0.0161   0.5257   0.6496
   2.500   0.4222   0.00685   0.00168  -0.0160   0.5200   0.6556
   2.750   0.4494   0.00691   0.00173  -0.0159   0.5140   0.6615
   3.000   0.4768   0.00690   0.00177  -0.0158   0.5080   0.6686
   3.250   0.5036   0.00694   0.00182  -0.0156   0.5010   0.6766
   3.500   0.5306   0.00696   0.00188  -0.0155   0.4944   0.6849
   3.750   0.5572   0.00699   0.00194  -0.0152   0.4862   0.6947
   4.000   0.5835   0.00702   0.00200  -0.0150   0.4781   0.7057
   4.250   0.6093   0.00707   0.00208  -0.0146   0.4676   0.7188
   4.500   0.6351   0.00709   0.00215  -0.0142   0.4565   0.7350
   4.750   0.6599   0.00713   0.00225  -0.0136   0.4445   0.7543
   5.000   0.6838   0.00719   0.00235  -0.0129   0.4281   0.7776
   5.250   0.7061   0.00729   0.00248  -0.0118   0.4049   0.8064
   5.500   0.7266   0.00743   0.00264  -0.0104   0.3776   0.8415
   5.750   0.7468   0.00764   0.00287  -0.0089   0.3502   0.8819
   6.000   0.7713   0.00793   0.00315  -0.0085   0.3203   0.9206
   6.250   0.8053   0.00838   0.00350  -0.0102   0.2856   0.9468
   6.500   0.8427   0.00896   0.00390  -0.0129   0.2471   0.9620
   6.750   0.8781   0.00944   0.00424  -0.0150   0.2202   0.9724
   7.000   0.9132   0.00985   0.00457  -0.0171   0.2014   0.9788
   7.250   0.9447   0.01020   0.00486  -0.0182   0.1877   0.9855
   7.500   0.9786   0.01056   0.00517  -0.0200   0.1743   0.9901
   7.750   1.0110   0.01094   0.00550  -0.0214   0.1614   0.9946
   8.000   1.0461   0.01133   0.00583  -0.0235   0.1482   0.9980
   8.250   1.0782   0.01173   0.00617  -0.0250   0.1360   1.0000
   8.500   1.0919   0.01203   0.00644  -0.0225   0.1273   1.0000
   8.750   1.1057   0.01234   0.00673  -0.0201   0.1190   1.0000
   9.000   1.1180   0.01271   0.00705  -0.0174   0.1101   1.0000
   9.250   1.1309   0.01307   0.00738  -0.0148   0.1020   1.0000
   9.500   1.1431   0.01345   0.00774  -0.0121   0.0940   1.0000
   9.750   1.1510   0.01389   0.00813  -0.0087   0.0853   1.0000
  10.000   1.1558   0.01435   0.00855  -0.0047   0.0767   1.0000
  10.250   1.1635   0.01484   0.00901  -0.0015   0.0686   1.0000
  10.500   1.1689   0.01552   0.00963   0.0019   0.0580   1.0000
  10.750   1.1750   0.01628   0.01033   0.0048   0.0482   1.0000
  11.000   1.1817   0.01711   0.01113   0.0075   0.0407   1.0000
  11.250   1.1898   0.01798   0.01198   0.0097   0.0361   1.0000
  11.500   1.1997   0.01883   0.01285   0.0115   0.0333   1.0000
  11.750   1.2089   0.01980   0.01384   0.0131   0.0310   1.0000
  12.000   1.2200   0.02073   0.01481   0.0144   0.0292   1.0000
  12.250   1.2293   0.02184   0.01594   0.0157   0.0279   1.0000
  12.500   1.2370   0.02314   0.01728   0.0169   0.0266   1.0000
  12.750   1.2493   0.02416   0.01835   0.0177   0.0258   1.0000
  13.000   1.2602   0.02533   0.01957   0.0185   0.0251   1.0000
  13.250   1.2696   0.02665   0.02093   0.0192   0.0242   1.0000
  13.500   1.2768   0.02817   0.02250   0.0200   0.0234   1.0000
  13.750   1.2799   0.03010   0.02447   0.0208   0.0225   1.0000
  14.000   1.2887   0.03158   0.02602   0.0213   0.0222   1.0000
  14.250   1.2974   0.03307   0.02757   0.0217   0.0218   1.0000
  14.500   1.3055   0.03465   0.02920   0.0221   0.0211   1.0000
  14.750   1.3121   0.03639   0.03100   0.0224   0.0205   1.0000
  15.000   1.3163   0.03837   0.03303   0.0227   0.0200   1.0000
  15.250   1.3171   0.04073   0.03545   0.0230   0.0195   1.0000
  15.500   1.3136   0.04361   0.03840   0.0231   0.0189   1.0000
  15.750   1.3180   0.04576   0.04063   0.0231   0.0186   1.0000
  16.000   1.3207   0.04814   0.04309   0.0230   0.0184   1.0000
  16.250   1.3246   0.05045   0.04546   0.0228   0.0179   1.0000
  16.500   1.3261   0.05308   0.04817   0.0225   0.0176   1.0000
  16.750   1.3277   0.05575   0.05091   0.0221   0.0172   1.0000
  17.000   1.3279   0.05861   0.05384   0.0216   0.0169   1.0000
  17.250   1.3254   0.06189   0.05719   0.0210   0.0165   1.0000
  17.500   1.3194   0.06567   0.06104   0.0201   0.0162   1.0000
  17.750   1.3083   0.07015   0.06561   0.0190   0.0159   1.0000
  18.000   1.2966   0.07485   0.07040   0.0177   0.0157   1.0000
  18.250   1.2970   0.07804   0.07368   0.0167   0.0155   1.0000
  18.500   1.2914   0.08206   0.07779   0.0154   0.0153   1.0000
  18.750   1.2849   0.08629   0.08212   0.0140   0.0151   1.0000
  19.000   1.2778   0.09069   0.08661   0.0125   0.0149   1.0000
  19.250   1.2701   0.09526   0.09128   0.0108   0.0146   1.0000
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