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MUE 139 (mue139-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MUE 139 (mue139-il)
Reynolds number: 500,000
Max Cl/Cd: 90.93 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mue139-il-500000-n5.txt
Download as CSV file: xf-mue139-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MUE 139                                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.8596   0.03752   0.03410  -0.0780   1.0000   0.0320
 -12.500  -0.8783   0.03299   0.02924  -0.0773   1.0000   0.0322
 -12.250  -0.8797   0.03041   0.02641  -0.0756   1.0000   0.0323
 -12.000  -0.8744   0.02849   0.02428  -0.0738   1.0000   0.0325
 -11.750  -0.8650   0.02702   0.02270  -0.0719   1.0000   0.0327
 -11.500  -0.8478   0.02583   0.02144  -0.0710   0.9991   0.0330
 -11.250  -0.8164   0.02465   0.02017  -0.0727   0.9922   0.0332
 -10.750  -0.7573   0.02273   0.01809  -0.0746   0.9631   0.0339
 -10.500  -0.7110   0.02175   0.01700  -0.0789   0.9438   0.0344
 -10.250  -0.6545   0.02060   0.01566  -0.0852   0.9173   0.0350
 -10.000  -0.6134   0.01968   0.01447  -0.0883   0.8706   0.0355
  -9.750  -0.5900   0.01908   0.01358  -0.0875   0.8255   0.0359
  -9.500  -0.5691   0.01852   0.01278  -0.0862   0.7938   0.0363
  -8.750  -0.5031   0.01701   0.01076  -0.0826   0.7345   0.0374
  -8.500  -0.4794   0.01661   0.01027  -0.0816   0.7214   0.0378
  -8.250  -0.4551   0.01627   0.00983  -0.0807   0.7100   0.0382
  -8.000  -0.4304   0.01592   0.00940  -0.0799   0.6986   0.0386
  -7.750  -0.4056   0.01558   0.00897  -0.0791   0.6876   0.0392
  -7.500  -0.3807   0.01526   0.00855  -0.0782   0.6758   0.0398
  -7.250  -0.3552   0.01494   0.00813  -0.0775   0.6652   0.0405
  -7.000  -0.3299   0.01464   0.00770  -0.0767   0.6547   0.0412
  -6.750  -0.3044   0.01430   0.00728  -0.0759   0.6430   0.0417
  -6.500  -0.2791   0.01399   0.00691  -0.0752   0.6311   0.0424
  -6.250  -0.2536   0.01376   0.00660  -0.0744   0.6169   0.0430
  -6.000  -0.2279   0.01356   0.00631  -0.0736   0.5995   0.0437
  -5.750  -0.2023   0.01337   0.00602  -0.0728   0.5792   0.0446
  -5.500  -0.1766   0.01318   0.00572  -0.0720   0.5589   0.0454
  -5.250  -0.1508   0.01301   0.00542  -0.0713   0.5397   0.0463
  -5.000  -0.1251   0.01283   0.00514  -0.0705   0.5210   0.0472
  -4.750  -0.0992   0.01269   0.00494  -0.0698   0.5035   0.0482
  -4.500  -0.0731   0.01260   0.00476  -0.0691   0.4869   0.0494
  -4.000  -0.0205   0.01240   0.00438  -0.0678   0.4594   0.0520
  -3.750   0.0058   0.01227   0.00419  -0.0672   0.4493   0.0532
  -3.500   0.0324   0.01217   0.00406  -0.0666   0.4402   0.0545
  -3.250   0.0590   0.01209   0.00393  -0.0660   0.4325   0.0560
  -3.000   0.0860   0.01200   0.00380  -0.0654   0.4252   0.0576
  -2.750   0.1126   0.01193   0.00367  -0.0648   0.4181   0.0592
  -2.500   0.1395   0.01184   0.00359  -0.0643   0.4122   0.0611
  -2.250   0.1665   0.01179   0.00351  -0.0638   0.4054   0.0631
  -1.750   0.2202   0.01167   0.00333  -0.0626   0.3928   0.0671
  -1.500   0.2472   0.01163   0.00328  -0.0621   0.3864   0.0695
  -1.250   0.2739   0.01163   0.00323  -0.0616   0.3808   0.0720
  -1.000   0.3011   0.01158   0.00317  -0.0611   0.3757   0.0744
  -0.750   0.3280   0.01154   0.00314  -0.0606   0.3700   0.0772
  -0.500   0.3547   0.01154   0.00311  -0.0600   0.3642   0.0803
  -0.250   0.3817   0.01153   0.00307  -0.0595   0.3593   0.0830
   0.000   0.4086   0.01149   0.00306  -0.0590   0.3536   0.0865
   0.250   0.4352   0.01151   0.00305  -0.0585   0.3474   0.0902
   0.500   0.4620   0.01152   0.00304  -0.0579   0.3419   0.0935
   0.750   0.4887   0.01151   0.00304  -0.0574   0.3357   0.0978
   1.000   0.5152   0.01156   0.00305  -0.0569   0.3297   0.1023
   1.250   0.5418   0.01157   0.00307  -0.0563   0.3249   0.1072
   1.500   0.5684   0.01159   0.00310  -0.0558   0.3195   0.1129
   1.750   0.5946   0.01163   0.00314  -0.0552   0.3142   0.1198
   2.000   0.6207   0.01168   0.00319  -0.0547   0.3095   0.1290
   2.250   0.6471   0.01169   0.00324  -0.0541   0.3050   0.1422
   2.500   0.6727   0.01168   0.00331  -0.0535   0.3003   0.1724
   2.750   0.6965   0.01153   0.00345  -0.0526   0.2955   0.2896
   3.000   0.7217   0.01151   0.00354  -0.0519   0.2915   0.3440
   3.250   0.7427   0.01112   0.00368  -0.0506   0.2878   0.5315
   3.750   0.8700   0.01065   0.00414  -0.0656   0.2777   1.0000
   4.000   0.8947   0.01079   0.00426  -0.0647   0.2751   1.0000
   4.250   0.9191   0.01094   0.00439  -0.0639   0.2720   1.0000
   4.500   0.9432   0.01111   0.00452  -0.0629   0.2688   1.0000
   4.750   0.9670   0.01130   0.00467  -0.0620   0.2656   1.0000
   5.000   0.9902   0.01154   0.00485  -0.0609   0.2615   1.0000
   5.250   1.0148   0.01168   0.00498  -0.0601   0.2581   1.0000
   5.500   1.0389   0.01185   0.00514  -0.0593   0.2542   1.0000
   5.750   1.0626   0.01205   0.00532  -0.0583   0.2513   1.0000
   6.000   1.0858   0.01227   0.00551  -0.0573   0.2482   1.0000
   6.250   1.1087   0.01252   0.00572  -0.0563   0.2456   1.0000
   6.500   1.1328   0.01269   0.00591  -0.0555   0.2438   1.0000
   6.750   1.1568   0.01287   0.00610  -0.0546   0.2413   1.0000
   7.000   1.1802   0.01307   0.00630  -0.0537   0.2386   1.0000
   7.250   1.2032   0.01329   0.00652  -0.0528   0.2359   1.0000
   7.500   1.2257   0.01354   0.00675  -0.0517   0.2333   1.0000
   7.750   1.2476   0.01381   0.00701  -0.0506   0.2308   1.0000
   8.000   1.2703   0.01404   0.00725  -0.0497   0.2287   1.0000
   8.250   1.2933   0.01424   0.00749  -0.0487   0.2262   1.0000
   8.500   1.3157   0.01447   0.00774  -0.0477   0.2232   1.0000
   8.750   1.3373   0.01473   0.00800  -0.0466   0.2201   1.0000
   9.000   1.3579   0.01502   0.00829  -0.0454   0.2172   1.0000
   9.250   1.3779   0.01534   0.00861  -0.0441   0.2144   1.0000
   9.500   1.3997   0.01557   0.00888  -0.0431   0.2119   1.0000
   9.750   1.4204   0.01583   0.00917  -0.0419   0.2085   1.0000
  10.000   1.4397   0.01615   0.00950  -0.0405   0.2045   1.0000
  10.250   1.4564   0.01652   0.00986  -0.0387   0.2007   1.0000
  10.500   1.4735   0.01683   0.01020  -0.0369   0.1976   1.0000
  10.750   1.4901   0.01716   0.01056  -0.0351   0.1934   1.0000
  11.000   1.5047   0.01758   0.01099  -0.0332   0.1888   1.0000
  11.250   1.5188   0.01805   0.01146  -0.0312   0.1841   1.0000
  11.500   1.5340   0.01851   0.01194  -0.0295   0.1787   1.0000
  11.750   1.5464   0.01912   0.01255  -0.0276   0.1734   1.0000
  12.000   1.5594   0.01975   0.01320  -0.0258   0.1683   1.0000
  12.250   1.5708   0.02051   0.01396  -0.0241   0.1624   1.0000
  12.500   1.5804   0.02142   0.01488  -0.0224   0.1576   1.0000
  12.750   1.5915   0.02231   0.01581  -0.0210   0.1532   1.0000
  13.000   1.6001   0.02344   0.01696  -0.0196   0.1488   1.0000
  13.250   1.6071   0.02477   0.01831  -0.0184   0.1450   1.0000
  13.500   1.6162   0.02603   0.01963  -0.0175   0.1417   1.0000
  13.750   1.6233   0.02753   0.02118  -0.0167   0.1385   1.0000
  14.000   1.6274   0.02937   0.02306  -0.0160   0.1354   1.0000
  14.250   1.6306   0.03139   0.02513  -0.0155   0.1326   1.0000
  14.500   1.6361   0.03324   0.02706  -0.0151   0.1302   1.0000
  14.750   1.6389   0.03541   0.02929  -0.0148   0.1275   1.0000
  15.000   1.6389   0.03791   0.03185  -0.0146   0.1252   1.0000
  15.250   1.6343   0.04094   0.03494  -0.0146   0.1227   1.0000
  15.500   1.6299   0.04402   0.03809  -0.0147   0.1208   1.0000
  15.750   1.6295   0.04672   0.04089  -0.0148   0.1193   1.0000
  16.000   1.6264   0.04978   0.04404  -0.0151   0.1177   1.0000
  16.250   1.6208   0.05322   0.04757  -0.0155   0.1159   1.0000
  16.500   1.6131   0.05700   0.05142  -0.0162   0.1142   1.0000
  16.750   1.6009   0.06143   0.05592  -0.0171   0.1121   1.0000
  17.000   1.5894   0.06586   0.06044  -0.0181   0.1108   1.0000
  17.250   1.5792   0.07017   0.06483  -0.0191   0.1088   1.0000
  17.500   1.5733   0.07395   0.06870  -0.0200   0.1074   1.0000
  17.750   1.5659   0.07798   0.07282  -0.0209   0.1061   1.0000
  18.000   1.5541   0.08262   0.07754  -0.0222   0.1037   1.0000
  18.250   1.5428   0.08726   0.08224  -0.0235   0.1021   1.0000
  18.500   1.5316   0.09191   0.08695  -0.0249   0.1006   1.0000
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