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MUE 139 (mue139-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: MUE 139 (mue139-il)
Reynolds number: 100,000
Max Cl/Cd: 44.91 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mue139-il-100000-n5.txt
Download as CSV file: xf-mue139-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.2558   0.11612   0.11087  -0.0247   1.0000   0.0815
 -10.000  -0.2573   0.11331   0.10812  -0.0264   1.0000   0.0819
  -9.750  -0.2581   0.11033   0.10519  -0.0280   1.0000   0.0820
  -9.500  -0.2573   0.10729   0.10221  -0.0291   1.0000   0.0821
  -9.250  -0.2580   0.10426   0.09924  -0.0304   1.0000   0.0822
  -9.000  -0.2595   0.10117   0.09623  -0.0316   1.0000   0.0823
  -8.750  -0.2601   0.09813   0.09325  -0.0324   1.0000   0.0823
  -8.250  -0.2547   0.08858   0.08378  -0.0322   1.0000   0.0652
  -8.000  -0.2535   0.08619   0.08150  -0.0316   1.0000   0.0646
  -7.750  -0.2362   0.08171   0.07703  -0.0367   0.9629   0.0639
  -7.500  -0.2153   0.07628   0.07156  -0.0449   0.9246   0.0634
  -7.250  -0.1974   0.06995   0.06511  -0.0551   0.8888   0.0641
  -7.000  -0.1824   0.06378   0.05875  -0.0637   0.8574   0.0643
  -6.750  -0.1727   0.05811   0.05287  -0.0694   0.8302   0.0642
  -6.500  -0.1664   0.05243   0.04692  -0.0735   0.8079   0.0641
  -6.250  -0.1629   0.04634   0.04043  -0.0763   0.7893   0.0643
  -6.000  -0.1646   0.03914   0.03249  -0.0779   0.7738   0.0659
  -5.750  -0.1421   0.03836   0.03165  -0.0774   0.7562   0.0668
  -5.500  -0.1227   0.03668   0.02975  -0.0770   0.7400   0.0679
  -5.250  -0.1048   0.03434   0.02705  -0.0765   0.7250   0.0690
  -5.000  -0.0864   0.03199   0.02426  -0.0758   0.7107   0.0702
  -4.750  -0.0678   0.02970   0.02147  -0.0749   0.6961   0.0721
  -4.500  -0.0471   0.02806   0.01941  -0.0739   0.6810   0.0742
  -4.250  -0.0234   0.02740   0.01865  -0.0730   0.6651   0.0757
  -4.000  -0.0001   0.02651   0.01754  -0.0721   0.6495   0.0775
  -3.750   0.0233   0.02543   0.01613  -0.0711   0.6341   0.0794
  -3.500   0.0469   0.02435   0.01458  -0.0700   0.6185   0.0824
  -3.250   0.0713   0.02383   0.01403  -0.0692   0.6020   0.0844
  -3.000   0.0961   0.02329   0.01336  -0.0684   0.5862   0.0867
  -2.750   0.1212   0.02266   0.01251  -0.0675   0.5712   0.0894
  -2.500   0.1465   0.02209   0.01165  -0.0666   0.5571   0.0928
  -2.250   0.1716   0.02168   0.01120  -0.0659   0.5438   0.0956
  -2.000   0.1972   0.02128   0.01069  -0.0651   0.5304   0.0988
  -1.750   0.2230   0.02093   0.01014  -0.0643   0.5184   0.1027
  -1.250   0.2740   0.02028   0.00939  -0.0629   0.4966   0.1102
  -1.000   0.2998   0.02007   0.00901  -0.0621   0.4870   0.1149
  -0.750   0.3251   0.01980   0.00873  -0.0614   0.4769   0.1195
  -0.500   0.3504   0.01961   0.00850  -0.0606   0.4683   0.1246
  -0.250   0.3760   0.01949   0.00829  -0.0598   0.4593   0.1306
   0.000   0.4009   0.01932   0.00810  -0.0591   0.4521   0.1370
   0.250   0.4264   0.01923   0.00800  -0.0583   0.4440   0.1445
   0.500   0.4515   0.01913   0.00789  -0.0576   0.4370   0.1533
   0.750   0.4773   0.01909   0.00784  -0.0569   0.4297   0.1644
   1.250   0.5298   0.01895   0.00779  -0.0559   0.4160   0.2118
   1.500   0.5558   0.01872   0.00798  -0.0556   0.4086   0.3219
   2.000   0.6617   0.01764   0.00828  -0.0650   0.3936   1.0000
   2.250   0.6856   0.01792   0.00844  -0.0640   0.3876   1.0000
   2.500   0.7095   0.01821   0.00857  -0.0631   0.3825   1.0000
   2.750   0.7334   0.01853   0.00877  -0.0621   0.3772   1.0000
   3.000   0.7570   0.01883   0.00901  -0.0612   0.3713   1.0000
   3.250   0.7808   0.01914   0.00920  -0.0603   0.3664   1.0000
   3.500   0.8052   0.01948   0.00939  -0.0594   0.3626   1.0000
   3.750   0.8285   0.01984   0.00976  -0.0585   0.3577   1.0000
   4.000   0.8520   0.02020   0.01008  -0.0576   0.3530   1.0000
   4.250   0.8758   0.02054   0.01034  -0.0567   0.3488   1.0000
   4.500   0.9001   0.02089   0.01056  -0.0559   0.3452   1.0000
   4.750   0.9226   0.02130   0.01102  -0.0549   0.3405   1.0000
   5.000   0.9456   0.02171   0.01143  -0.0540   0.3362   1.0000
   5.250   0.9690   0.02211   0.01178  -0.0532   0.3326   1.0000
   5.500   0.9930   0.02249   0.01207  -0.0524   0.3294   1.0000
   5.750   1.0157   0.02294   0.01252  -0.0515   0.3258   1.0000
   6.000   1.0373   0.02342   0.01307  -0.0504   0.3215   1.0000
   6.250   1.0595   0.02387   0.01352  -0.0495   0.3177   1.0000
   6.500   1.0824   0.02427   0.01389  -0.0486   0.3142   1.0000
   6.750   1.1063   0.02466   0.01418  -0.0479   0.3111   1.0000
   7.000   1.1253   0.02523   0.01487  -0.0466   0.3066   1.0000
   7.250   1.1454   0.02572   0.01542  -0.0454   0.3022   1.0000
   7.500   1.1668   0.02612   0.01580  -0.0444   0.2983   1.0000
   7.750   1.1897   0.02649   0.01609  -0.0436   0.2949   1.0000
   8.000   1.2075   0.02712   0.01683  -0.0422   0.2909   1.0000
   8.250   1.2252   0.02772   0.01753  -0.0408   0.2868   1.0000
   8.500   1.2445   0.02822   0.01805  -0.0396   0.2829   1.0000
   8.750   1.2656   0.02864   0.01843  -0.0386   0.2796   1.0000
   9.000   1.2842   0.02923   0.01905  -0.0374   0.2763   1.0000
   9.250   1.2973   0.03002   0.02000  -0.0355   0.2722   1.0000
   9.500   1.3126   0.03067   0.02072  -0.0339   0.2683   1.0000
   9.750   1.3303   0.03119   0.02125  -0.0326   0.2649   1.0000
  10.000   1.3514   0.03163   0.02162  -0.0317   0.2618   1.0000
  10.250   1.3573   0.03265   0.02284  -0.0291   0.2579   1.0000
  10.500   1.3640   0.03355   0.02387  -0.0266   0.2540   1.0000
  10.750   1.3736   0.03427   0.02464  -0.0244   0.2504   1.0000
  11.000   1.3883   0.03482   0.02517  -0.0229   0.2472   1.0000
  11.250   1.3963   0.03575   0.02615  -0.0208   0.2440   1.0000
  11.500   1.3904   0.03733   0.02795  -0.0178   0.2401   1.0000
  11.750   1.3912   0.03872   0.02944  -0.0157   0.2363   1.0000
  12.000   1.3995   0.03972   0.03048  -0.0143   0.2329   1.0000
  12.250   1.4163   0.04029   0.03097  -0.0134   0.2298   1.0000
  12.500   1.3946   0.04354   0.03453  -0.0115   0.2258   1.0000
  12.750   1.3821   0.04653   0.03770  -0.0105   0.2218   1.0000
  13.000   1.3829   0.04855   0.03978  -0.0100   0.2182   1.0000
  13.250   1.3982   0.04926   0.04043  -0.0093   0.2151   1.0000
  13.500   1.3541   0.05615   0.04764  -0.0102   0.2107   1.0000
  13.750   1.3031   0.06492   0.05666  -0.0127   0.2055   1.0000
  14.000   1.3114   0.06655   0.05830  -0.0126   0.2021   1.0000
  14.500   1.1443   0.09803   0.09017  -0.0256   0.1844   1.0000
  14.750   1.2022   0.09165   0.08374  -0.0219   0.1855   1.0000
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