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KC-135 BL52.44 AIRFOIL (kc135a-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: KC-135 BL52.44 AIRFOIL (kc135a-il)
Reynolds number: 100,000
Max Cl/Cd: 47.48 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-kc135a-il-100000-n5.txt
Download as CSV file: xf-kc135a-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.5556   0.09058   0.08498  -0.0468   1.0000   0.0346
 -12.250  -0.5793   0.08313   0.07746  -0.0513   1.0000   0.0343
 -12.000  -0.6067   0.07639   0.07061  -0.0550   1.0000   0.0341
 -11.750  -0.6312   0.07099   0.06508  -0.0572   1.0000   0.0339
 -11.500  -0.6543   0.06645   0.06039  -0.0582   1.0000   0.0338
 -11.250  -0.6753   0.06263   0.05641  -0.0580   1.0000   0.0337
 -11.000  -0.6944   0.05940   0.05302  -0.0565   1.0000   0.0336
 -10.750  -0.7122   0.05669   0.05014  -0.0537   1.0000   0.0337
 -10.500  -0.7287   0.05431   0.04759  -0.0499   1.0000   0.0337
 -10.250  -0.7408   0.05189   0.04496  -0.0462   1.0000   0.0339
 -10.000  -0.7486   0.04943   0.04228  -0.0427   1.0000   0.0340
  -9.750  -0.7535   0.04704   0.03964  -0.0392   1.0000   0.0341
  -9.500  -0.7551   0.04479   0.03715  -0.0358   1.0000   0.0342
  -9.250  -0.7545   0.04269   0.03479  -0.0325   1.0000   0.0344
  -9.000  -0.7530   0.04071   0.03256  -0.0290   1.0000   0.0347
  -8.750  -0.7499   0.03893   0.03054  -0.0257   0.9995   0.0350
  -8.500  -0.7196   0.03623   0.02743  -0.0274   0.9875   0.0356
  -8.250  -0.6866   0.03445   0.02559  -0.0296   0.9762   0.0368
  -8.000  -0.6531   0.03281   0.02382  -0.0316   0.9645   0.0383
  -7.750  -0.6183   0.03113   0.02188  -0.0334   0.9534   0.0403
  -7.500  -0.5803   0.02934   0.01982  -0.0355   0.9437   0.0418
  -7.250  -0.5449   0.02784   0.01835  -0.0375   0.9312   0.0433
  -7.000  -0.5102   0.02668   0.01714  -0.0392   0.9185   0.0460
  -6.750  -0.4748   0.02558   0.01586  -0.0407   0.9062   0.0491
  -6.500  -0.4424   0.02437   0.01475  -0.0420   0.8937   0.0515
  -6.250  -0.4150   0.02353   0.01386  -0.0422   0.8791   0.0551
  -6.000  -0.3911   0.02271   0.01297  -0.0417   0.8650   0.0585
  -5.750  -0.3707   0.02197   0.01222  -0.0407   0.8516   0.0621
  -5.500  -0.3495   0.02139   0.01151  -0.0397   0.8398   0.0666
  -5.250  -0.3329   0.02072   0.01080  -0.0379   0.8275   0.0711
  -5.000  -0.3137   0.02021   0.01018  -0.0365   0.8166   0.0773
  -4.750  -0.2944   0.01960   0.00952  -0.0351   0.8071   0.0858
  -4.500  -0.2759   0.01904   0.00894  -0.0336   0.7969   0.0983
  -4.250  -0.2584   0.01822   0.00824  -0.0320   0.7889   0.1360
  -4.000  -0.2658   0.01615   0.00784  -0.0267   0.7793   0.4460
  -3.750  -0.2467   0.01617   0.00799  -0.0245   0.7723   0.5314
  -3.500  -0.2256   0.01630   0.00808  -0.0228   0.7641   0.5680
  -3.250  -0.2026   0.01643   0.00813  -0.0214   0.7569   0.5955
  -3.000  -0.1796   0.01660   0.00827  -0.0200   0.7499   0.6205
  -2.750  -0.1573   0.01675   0.00838  -0.0184   0.7427   0.6436
  -2.500  -0.1317   0.01686   0.00842  -0.0175   0.7372   0.6607
  -2.250  -0.1059   0.01687   0.00841  -0.0169   0.7303   0.6696
  -2.000  -0.0798   0.01680   0.00822  -0.0166   0.7238   0.6758
  -1.750  -0.0527   0.01674   0.00801  -0.0164   0.7186   0.6817
  -1.500  -0.0267   0.01672   0.00798  -0.0161   0.7115   0.6868
  -1.250  -0.0001   0.01668   0.00786  -0.0159   0.7060   0.6928
  -1.000   0.0273   0.01665   0.00771  -0.0158   0.7014   0.6992
  -0.750   0.0530   0.01667   0.00775  -0.0155   0.6946   0.7048
  -0.500   0.0794   0.01666   0.00769  -0.0153   0.6890   0.7116
  -0.250   0.1074   0.01665   0.00761  -0.0152   0.6846   0.7179
   0.000   0.1329   0.01671   0.00770  -0.0149   0.6783   0.7245
   0.250   0.1587   0.01673   0.00769  -0.0146   0.6726   0.7327
   0.500   0.1874   0.01674   0.00769  -0.0146   0.6679   0.7391
   0.750   0.2129   0.01681   0.00778  -0.0143   0.6620   0.7474
   1.000   0.2394   0.01687   0.00787  -0.0141   0.6559   0.7554
   1.250   0.2675   0.01689   0.00789  -0.0141   0.6510   0.7646
   1.500   0.2941   0.01698   0.00803  -0.0139   0.6451   0.7736
   1.750   0.3201   0.01706   0.00816  -0.0136   0.6388   0.7842
   2.000   0.3494   0.01710   0.00823  -0.0138   0.6337   0.7944
   2.250   0.3756   0.01720   0.00841  -0.0135   0.6274   0.8066
   2.500   0.4025   0.01727   0.00855  -0.0133   0.6204   0.8196
   2.750   0.4332   0.01725   0.00856  -0.0136   0.6137   0.8324
   3.000   0.4605   0.01730   0.00872  -0.0135   0.6036   0.8473
   3.250   0.4920   0.01729   0.00874  -0.0140   0.5950   0.8628
   3.500   0.5237   0.01735   0.00888  -0.0147   0.5856   0.8788
   3.750   0.5577   0.01742   0.00901  -0.0158   0.5772   0.8948
   4.000   0.5927   0.01747   0.00912  -0.0172   0.5677   0.9107
   4.250   0.6279   0.01758   0.00932  -0.0188   0.5577   0.9265
   4.500   0.6668   0.01759   0.00933  -0.0209   0.5483   0.9396
   4.750   0.7032   0.01773   0.00959  -0.0229   0.5358   0.9535
   5.000   0.7400   0.01782   0.00975  -0.0249   0.5231   0.9669
   5.250   0.7772   0.01790   0.00989  -0.0270   0.5093   0.9800
   5.500   0.8150   0.01798   0.01002  -0.0293   0.4931   0.9925
   5.750   0.8447   0.01809   0.01018  -0.0302   0.4761   1.0000
   6.000   0.8582   0.01824   0.01034  -0.0277   0.4601   1.0000
   6.250   0.8717   0.01842   0.01052  -0.0252   0.4419   1.0000
   6.500   0.8850   0.01864   0.01071  -0.0227   0.4211   1.0000
   6.750   0.8977   0.01891   0.01093  -0.0201   0.3979   1.0000
   7.000   0.9094   0.01926   0.01118  -0.0174   0.3735   1.0000
   7.250   0.9199   0.01971   0.01151  -0.0145   0.3500   1.0000
   7.500   0.9292   0.02025   0.01194  -0.0115   0.3276   1.0000
   7.750   0.9376   0.02086   0.01243  -0.0084   0.3076   1.0000
   8.000   0.9459   0.02151   0.01300  -0.0054   0.2900   1.0000
   8.250   0.9538   0.02218   0.01361  -0.0025   0.2741   1.0000
   8.500   0.9612   0.02289   0.01426   0.0005   0.2598   1.0000
   8.750   0.9674   0.02358   0.01493   0.0037   0.2468   1.0000
   9.000   0.9733   0.02432   0.01566   0.0067   0.2349   1.0000
   9.250   0.9790   0.02514   0.01644   0.0096   0.2235   1.0000
   9.500   0.9839   0.02606   0.01730   0.0123   0.2121   1.0000
   9.750   0.9902   0.02699   0.01826   0.0146   0.1997   1.0000
  10.000   0.9963   0.02801   0.01929   0.0167   0.1879   1.0000
  10.250   1.0019   0.02913   0.02040   0.0187   0.1771   1.0000
  10.500   1.0068   0.03036   0.02163   0.0204   0.1670   1.0000
  10.750   1.0139   0.03157   0.02291   0.0219   0.1565   1.0000
  11.000   1.0196   0.03292   0.02428   0.0232   0.1471   1.0000
  11.250   1.0239   0.03443   0.02579   0.0245   0.1383   1.0000
  11.500   1.0301   0.03590   0.02735   0.0255   0.1287   1.0000
  11.750   1.0343   0.03757   0.02904   0.0264   0.1205   1.0000
  12.000   1.0370   0.03942   0.03091   0.0273   0.1119   1.0000
  12.250   1.0411   0.04125   0.03282   0.0280   0.1034   1.0000
  12.500   1.0424   0.04335   0.03492   0.0286   0.0966   1.0000
  12.750   1.0441   0.04552   0.03715   0.0291   0.0893   1.0000
  13.000   1.0451   0.04780   0.03949   0.0295   0.0832   1.0000
  13.250   1.0443   0.05032   0.04204   0.0298   0.0777   1.0000
  13.500   1.0445   0.05282   0.04460   0.0300   0.0730   1.0000
  13.750   1.0434   0.05553   0.04737   0.0300   0.0687   1.0000
  14.000   1.0412   0.05843   0.05029   0.0299   0.0654   1.0000
  14.250   1.0416   0.06115   0.05314   0.0298   0.0621   1.0000
  14.500   1.0395   0.06424   0.05629   0.0294   0.0593   1.0000
  14.750   1.0371   0.06742   0.05949   0.0289   0.0570   1.0000
  15.000   1.0369   0.07048   0.06271   0.0284   0.0546   1.0000
  15.250   1.0356   0.07373   0.06605   0.0277   0.0526   1.0000
  15.500   1.0338   0.07708   0.06946   0.0269   0.0510   1.0000
  15.750   1.0328   0.08033   0.07273   0.0261   0.0497   1.0000
  16.000   1.0305   0.08404   0.07663   0.0251   0.0480   1.0000
  16.250   1.0270   0.08796   0.08069   0.0238   0.0464   1.0000
  16.500   1.0248   0.09170   0.08453   0.0225   0.0453   1.0000
  16.750   1.0224   0.09551   0.08842   0.0211   0.0441   1.0000
  17.000   1.0234   0.09872   0.09164   0.0201   0.0431   1.0000
  17.250   1.0166   0.10356   0.09667   0.0181   0.0422   1.0000
  17.500   1.0068   0.10908   0.10240   0.0156   0.0413   1.0000
  17.750   0.9961   0.11494   0.10845   0.0127   0.0407   1.0000
  18.000   0.9833   0.12138   0.11507   0.0094   0.0400   1.0000
  18.250   0.9675   0.12867   0.12254   0.0054   0.0395   1.0000
  18.500   0.9445   0.13784   0.13190   0.0002   0.0391   1.0000
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