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MUE 139 (mue139-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MUE 139 (mue139-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.53 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mue139-il-1000000.txt
Download as CSV file: xf-mue139-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.3746   0.15382   0.15200  -0.0046   1.0000   0.0263
 -14.000  -0.2602   0.14156   0.13988  -0.0177   1.0000   0.0290
 -13.750  -0.9532   0.03517   0.03238  -0.0842   1.0000   0.0318
 -13.500  -0.9623   0.03247   0.02950  -0.0826   1.0000   0.0320
 -13.250  -0.9574   0.03086   0.02777  -0.0810   1.0000   0.0322
 -13.000  -0.9541   0.02905   0.02581  -0.0790   1.0000   0.0323
 -12.750  -0.9383   0.02839   0.02507  -0.0776   1.0000   0.0325
 -12.500  -0.9419   0.02570   0.02214  -0.0749   1.0000   0.0328
 -12.250  -0.9332   0.02425   0.02060  -0.0727   1.0000   0.0333
 -12.000  -0.9189   0.02335   0.01964  -0.0708   1.0000   0.0335
 -11.750  -0.9026   0.02265   0.01892  -0.0690   1.0000   0.0337
 -11.500  -0.8824   0.02191   0.01813  -0.0679   0.9996   0.0340
 -11.250  -0.8455   0.02107   0.01722  -0.0701   0.9971   0.0343
 -11.000  -0.8088   0.02024   0.01631  -0.0723   0.9933   0.0347
 -10.750  -0.7775   0.01941   0.01540  -0.0732   0.9874   0.0350
 -10.500  -0.7446   0.01863   0.01453  -0.0745   0.9801   0.0354
 -10.000  -0.6730   0.01705   0.01275  -0.0779   0.9535   0.0362
  -9.750  -0.6134   0.01622   0.01177  -0.0845   0.9343   0.0366
  -9.500  -0.5694   0.01574   0.01106  -0.0877   0.8875   0.0369
  -9.250  -0.5507   0.01485   0.00990  -0.0861   0.8369   0.0375
  -9.000  -0.5294   0.01452   0.00940  -0.0845   0.8002   0.0380
  -8.750  -0.5064   0.01428   0.00903  -0.0833   0.7740   0.0384
  -8.500  -0.4826   0.01402   0.00866  -0.0822   0.7536   0.0388
  -8.250  -0.4580   0.01375   0.00830  -0.0813   0.7383   0.0392
  -8.000  -0.4330   0.01347   0.00793  -0.0804   0.7256   0.0397
  -7.750  -0.4079   0.01320   0.00756  -0.0796   0.7134   0.0402
  -7.500  -0.3823   0.01291   0.00719  -0.0788   0.7024   0.0407
  -7.250  -0.3566   0.01267   0.00685  -0.0780   0.6911   0.0412
  -7.000  -0.3304   0.01246   0.00656  -0.0773   0.6789   0.0415
  -6.750  -0.3064   0.01193   0.00595  -0.0763   0.6657   0.0424
  -6.500  -0.2809   0.01166   0.00563  -0.0755   0.6523   0.0430
  -6.250  -0.2545   0.01149   0.00540  -0.0748   0.6397   0.0437
  -6.000  -0.2277   0.01133   0.00520  -0.0742   0.6283   0.0446
  -5.750  -0.2012   0.01119   0.00499  -0.0735   0.6151   0.0454
  -5.500  -0.1746   0.01105   0.00476  -0.0729   0.5997   0.0462
  -5.250  -0.1478   0.01095   0.00457  -0.0722   0.5828   0.0467
  -5.000  -0.1228   0.01059   0.00416  -0.0714   0.5652   0.0481
  -4.750  -0.0965   0.01049   0.00398  -0.0707   0.5459   0.0491
  -4.500  -0.0700   0.01043   0.00384  -0.0700   0.5256   0.0502
  -4.250  -0.0434   0.01038   0.00370  -0.0694   0.5058   0.0514
  -4.000  -0.0167   0.01036   0.00358  -0.0687   0.4881   0.0523
  -3.750   0.0091   0.01016   0.00332  -0.0680   0.4732   0.0540
  -3.500   0.0361   0.01010   0.00323  -0.0674   0.4611   0.0556
  -3.250   0.0631   0.01008   0.00316  -0.0669   0.4500   0.0572
  -3.000   0.0903   0.01006   0.00308  -0.0664   0.4402   0.0584
  -2.750   0.1168   0.00991   0.00290  -0.0657   0.4320   0.0605
  -2.500   0.1441   0.00986   0.00284  -0.0652   0.4248   0.0623
  -2.250   0.1711   0.00985   0.00279  -0.0647   0.4171   0.0642
  -2.000   0.1989   0.00982   0.00273  -0.0643   0.4117   0.0656
  -1.750   0.2257   0.00970   0.00261  -0.0637   0.4055   0.0683
  -1.500   0.2528   0.00972   0.00260  -0.0632   0.3987   0.0707
  -1.250   0.2807   0.00969   0.00256  -0.0628   0.3940   0.0728
  -1.000   0.3078   0.00961   0.00248  -0.0623   0.3883   0.0756
  -0.750   0.3347   0.00962   0.00246  -0.0618   0.3815   0.0785
  -0.500   0.3624   0.00961   0.00245  -0.0614   0.3765   0.0813
  -0.250   0.3896   0.00956   0.00239  -0.0609   0.3704   0.0844
   0.000   0.4164   0.00957   0.00239  -0.0604   0.3638   0.0881
   0.250   0.4441   0.00957   0.00238  -0.0600   0.3588   0.0914
   0.500   0.4712   0.00954   0.00235  -0.0595   0.3529   0.0956
   0.750   0.4979   0.00957   0.00236  -0.0590   0.3461   0.1001
   1.000   0.5255   0.00959   0.00237  -0.0586   0.3409   0.1036
   1.250   0.5523   0.00957   0.00236  -0.0581   0.3347   0.1100
   1.500   0.5788   0.00964   0.00240  -0.0575   0.3276   0.1154
   1.750   0.6059   0.00962   0.00241  -0.0571   0.3226   0.1238
   2.000   0.6325   0.00965   0.00244  -0.0566   0.3161   0.1334
   2.250   0.6584   0.00966   0.00249  -0.0559   0.3098   0.1555
   2.500   0.6827   0.00941   0.00258  -0.0551   0.3054   0.2861
   2.750   0.7081   0.00937   0.00266  -0.0544   0.3003   0.3483
   3.000   0.7284   0.00901   0.00280  -0.0529   0.2950   0.5513
   3.250   0.8468   0.00830   0.00308  -0.0723   0.2879   1.0000
   3.500   0.8712   0.00844   0.00317  -0.0714   0.2839   1.0000
   3.750   0.8949   0.00862   0.00329  -0.0703   0.2792   1.0000
   4.000   0.9197   0.00874   0.00339  -0.0695   0.2761   1.0000
   4.250   0.9447   0.00884   0.00347  -0.0687   0.2727   1.0000
   4.500   0.9692   0.00899   0.00358  -0.0678   0.2686   1.0000
   4.750   0.9931   0.00917   0.00371  -0.0668   0.2647   1.0000
   5.000   1.0168   0.00937   0.00387  -0.0658   0.2613   1.0000
   5.250   1.0420   0.00947   0.00398  -0.0651   0.2597   1.0000
   5.500   1.0670   0.00959   0.00410  -0.0643   0.2576   1.0000
   5.750   1.0916   0.00973   0.00423  -0.0635   0.2551   1.0000
   6.000   1.1158   0.00989   0.00437  -0.0627   0.2525   1.0000
   6.250   1.1396   0.01008   0.00454  -0.0618   0.2497   1.0000
   6.500   1.1625   0.01032   0.00475  -0.0607   0.2465   1.0000
   6.750   1.1868   0.01048   0.00491  -0.0599   0.2448   1.0000
   7.000   1.2117   0.01060   0.00505  -0.0592   0.2432   1.0000
   7.250   1.2364   0.01074   0.00519  -0.0585   0.2410   1.0000
   7.500   1.2605   0.01090   0.00535  -0.0577   0.2385   1.0000
   7.750   1.2842   0.01109   0.00553  -0.0568   0.2360   1.0000
   8.000   1.3071   0.01132   0.00574  -0.0558   0.2331   1.0000
   8.250   1.3289   0.01160   0.00601  -0.0547   0.2298   1.0000
   8.500   1.3536   0.01172   0.00616  -0.0540   0.2284   1.0000
   8.750   1.3780   0.01186   0.00632  -0.0533   0.2262   1.0000
   9.000   1.4018   0.01203   0.00650  -0.0525   0.2235   1.0000
   9.250   1.4246   0.01224   0.00671  -0.0516   0.2205   1.0000
   9.500   1.4463   0.01250   0.00696  -0.0506   0.2171   1.0000
   9.750   1.4681   0.01276   0.00722  -0.0495   0.2139   1.0000
  10.000   1.4918   0.01290   0.00740  -0.0488   0.2113   1.0000
  10.250   1.5143   0.01310   0.00761  -0.0479   0.2075   1.0000
  10.500   1.5350   0.01339   0.00787  -0.0467   0.2031   1.0000
  10.750   1.5554   0.01368   0.00816  -0.0455   0.1989   1.0000
  11.000   1.5770   0.01390   0.00840  -0.0445   0.1949   1.0000
  11.250   1.5963   0.01422   0.00871  -0.0431   0.1899   1.0000
  11.500   1.6130   0.01459   0.00907  -0.0413   0.1849   1.0000
  11.750   1.6298   0.01488   0.00938  -0.0396   0.1801   1.0000
  12.000   1.6434   0.01533   0.00980  -0.0373   0.1741   1.0000
  12.250   1.6582   0.01575   0.01023  -0.0354   0.1688   1.0000
  12.500   1.6714   0.01628   0.01074  -0.0333   0.1626   1.0000
  12.750   1.6837   0.01688   0.01134  -0.0313   0.1569   1.0000
  13.000   1.6965   0.01749   0.01195  -0.0295   0.1518   1.0000
  13.250   1.7056   0.01832   0.01277  -0.0274   0.1464   1.0000
  13.500   1.7183   0.01902   0.01350  -0.0258   0.1430   1.0000
  13.750   1.7289   0.01988   0.01438  -0.0243   0.1394   1.0000
  14.000   1.7358   0.02103   0.01554  -0.0226   0.1353   1.0000
  14.250   1.7450   0.02213   0.01668  -0.0213   0.1321   1.0000
  14.500   1.7548   0.02326   0.01785  -0.0203   0.1291   1.0000
  14.750   1.7613   0.02471   0.01933  -0.0193   0.1261   1.0000
  15.000   1.7658   0.02644   0.02110  -0.0184   0.1236   1.0000
  15.250   1.7690   0.02836   0.02306  -0.0177   0.1207   1.0000
  15.500   1.7774   0.02989   0.02466  -0.0173   0.1186   1.0000
  15.750   1.7822   0.03180   0.02663  -0.0169   0.1168   1.0000
  16.000   1.7824   0.03417   0.02905  -0.0166   0.1143   1.0000
  16.250   1.7780   0.03709   0.03201  -0.0164   0.1117   1.0000
  16.500   1.7720   0.04021   0.03521  -0.0163   0.1101   1.0000
  16.750   1.7727   0.04271   0.03779  -0.0163   0.1086   1.0000
  17.000   1.7713   0.04547   0.04063  -0.0164   0.1071   1.0000
  17.250   1.7666   0.04865   0.04390  -0.0167   0.1059   1.0000
  17.500   1.7570   0.05254   0.04785  -0.0172   0.1039   1.0000
  17.750   1.7445   0.05685   0.05225  -0.0179   0.1025   1.0000
  18.000   1.7259   0.06205   0.05752  -0.0190   0.1005   1.0000
  18.250   1.7064   0.06744   0.06300  -0.0203   0.0989   1.0000
  18.500   1.7002   0.07119   0.06684  -0.0211   0.0979   1.0000
  18.750   1.6906   0.07541   0.07115  -0.0221   0.0966   1.0000
  19.000   1.6779   0.08007   0.07589  -0.0233   0.0952   1.0000
  19.250   1.6648   0.08480   0.08070  -0.0246   0.0940   1.0000
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