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MUE 139 (mue139-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MUE 139 (mue139-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.26 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mue139-il-1000000-n5.txt
Download as CSV file: xf-mue139-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -1.1558   0.03218   0.02890  -0.0892   1.0000   0.0260
 -15.250  -1.1561   0.03009   0.02669  -0.0877   1.0000   0.0261
 -15.000  -1.1489   0.02862   0.02513  -0.0862   1.0000   0.0264
 -14.750  -1.1399   0.02728   0.02370  -0.0845   1.0000   0.0265
 -14.500  -1.1276   0.02619   0.02253  -0.0829   1.0000   0.0267
 -14.250  -1.1147   0.02515   0.02140  -0.0813   1.0000   0.0269
 -14.000  -1.1001   0.02423   0.02040  -0.0796   1.0000   0.0272
 -13.750  -1.0851   0.02333   0.01942  -0.0780   1.0000   0.0273
 -13.500  -1.0690   0.02250   0.01852  -0.0763   1.0000   0.0275
 -13.250  -1.0518   0.02177   0.01771  -0.0747   1.0000   0.0278
 -13.000  -1.0339   0.02102   0.01689  -0.0732   0.9999   0.0279
 -12.750  -1.0002   0.02031   0.01609  -0.0747   0.9979   0.0283
 -12.500  -0.9682   0.01955   0.01525  -0.0759   0.9936   0.0284
 -12.250  -0.9410   0.01887   0.01450  -0.0760   0.9864   0.0286
 -12.000  -0.9147   0.01806   0.01362  -0.0760   0.9744   0.0290
 -11.750  -0.8760   0.01727   0.01277  -0.0784   0.9578   0.0293
 -11.500  -0.8082   0.01639   0.01180  -0.0868   0.9348   0.0297
 -11.250  -0.7646   0.01596   0.01108  -0.0900   0.8571   0.0300
 -11.000  -0.7451   0.01576   0.01063  -0.0882   0.7985   0.0303
 -10.750  -0.7234   0.01548   0.01018  -0.0868   0.7674   0.0306
 -10.500  -0.7002   0.01518   0.00976  -0.0857   0.7481   0.0309
 -10.250  -0.6763   0.01487   0.00935  -0.0847   0.7322   0.0312
 -10.000  -0.6520   0.01455   0.00894  -0.0838   0.7183   0.0315
  -9.750  -0.6275   0.01425   0.00854  -0.0829   0.7060   0.0318
  -9.500  -0.6027   0.01395   0.00816  -0.0820   0.6949   0.0321
  -9.250  -0.5773   0.01366   0.00778  -0.0812   0.6859   0.0323
  -9.000  -0.5519   0.01339   0.00743  -0.0805   0.6763   0.0325
  -8.750  -0.5268   0.01303   0.00702  -0.0797   0.6675   0.0330
  -8.500  -0.5015   0.01275   0.00667  -0.0789   0.6564   0.0334
  -8.250  -0.4755   0.01249   0.00636  -0.0782   0.6469   0.0338
  -7.750  -0.4232   0.01204   0.00581  -0.0768   0.6273   0.0347
  -7.500  -0.3970   0.01185   0.00555  -0.0761   0.6161   0.0352
  -7.250  -0.3706   0.01166   0.00529  -0.0755   0.6029   0.0356
  -7.000  -0.3442   0.01149   0.00505  -0.0748   0.5872   0.0362
  -6.750  -0.3182   0.01138   0.00482  -0.0740   0.5641   0.0366
  -6.500  -0.2925   0.01125   0.00458  -0.0733   0.5376   0.0372
  -6.250  -0.2666   0.01113   0.00436  -0.0725   0.5132   0.0380
  -6.000  -0.2403   0.01102   0.00417  -0.0719   0.4944   0.0387
  -5.750  -0.2138   0.01092   0.00400  -0.0712   0.4771   0.0394
  -5.500  -0.1871   0.01083   0.00384  -0.0706   0.4618   0.0401
  -5.250  -0.1604   0.01075   0.00368  -0.0700   0.4489   0.0409
  -5.000  -0.1334   0.01067   0.00353  -0.0694   0.4382   0.0415
  -4.750  -0.1064   0.01054   0.00338  -0.0689   0.4304   0.0425
  -4.500  -0.0793   0.01044   0.00325  -0.0683   0.4228   0.0436
  -4.250  -0.0521   0.01036   0.00314  -0.0678   0.4159   0.0446
  -4.000  -0.0246   0.01028   0.00302  -0.0673   0.4103   0.0458
  -3.750   0.0028   0.01021   0.00292  -0.0668   0.4041   0.0467
  -3.500   0.0299   0.01013   0.00282  -0.0663   0.3980   0.0482
  -3.250   0.0574   0.01005   0.00273  -0.0659   0.3928   0.0497
  -3.000   0.0848   0.00999   0.00264  -0.0654   0.3863   0.0510
  -2.750   0.1121   0.00997   0.00257  -0.0649   0.3801   0.0522
  -2.500   0.1397   0.00989   0.00249  -0.0644   0.3755   0.0537
  -2.250   0.1671   0.00983   0.00243  -0.0640   0.3702   0.0554
  -2.000   0.1945   0.00981   0.00238  -0.0635   0.3644   0.0571
  -1.750   0.2221   0.00978   0.00233  -0.0630   0.3599   0.0587
  -1.500   0.2495   0.00973   0.00228  -0.0626   0.3547   0.0611
  -1.250   0.2769   0.00971   0.00225  -0.0621   0.3489   0.0632
  -1.000   0.3043   0.00971   0.00222  -0.0617   0.3437   0.0652
  -0.750   0.3317   0.00969   0.00220  -0.0612   0.3381   0.0678
  -0.500   0.3590   0.00969   0.00219  -0.0608   0.3316   0.0707
  -0.250   0.3862   0.00971   0.00218  -0.0603   0.3254   0.0731
   0.000   0.4135   0.00970   0.00218  -0.0599   0.3196   0.0761
   0.250   0.4406   0.00973   0.00219  -0.0594   0.3135   0.0793
   0.500   0.4679   0.00976   0.00220  -0.0590   0.3084   0.0819
   0.750   0.4951   0.00977   0.00221  -0.0585   0.3033   0.0857
   1.000   0.5220   0.00981   0.00224  -0.0580   0.2976   0.0894
   1.250   0.5491   0.00986   0.00227  -0.0576   0.2929   0.0922
   1.500   0.5761   0.00987   0.00230  -0.0571   0.2887   0.0972
   1.750   0.6030   0.00992   0.00234  -0.0566   0.2841   0.1020
   2.000   0.6296   0.00999   0.00239  -0.0561   0.2789   0.1069
   2.250   0.6565   0.01002   0.00245  -0.0557   0.2753   0.1137
   2.500   0.6833   0.01005   0.00250  -0.0552   0.2718   0.1227
   2.750   0.7099   0.01010   0.00256  -0.0547   0.2685   0.1335
   3.000   0.7360   0.01013   0.00264  -0.0542   0.2651   0.1567
   3.250   0.7604   0.01000   0.00276  -0.0534   0.2618   0.2614
   3.500   0.7864   0.00997   0.00286  -0.0528   0.2599   0.3169
   3.750   0.8123   0.00996   0.00295  -0.0522   0.2575   0.3570
   4.000   0.8197   0.00889   0.00312  -0.0481   0.2553   0.8268
   4.500   0.9665   0.00916   0.00354  -0.0675   0.2436   1.0000
   4.750   0.9913   0.00928   0.00365  -0.0667   0.2406   1.0000
   5.000   1.0160   0.00942   0.00376  -0.0658   0.2382   1.0000
   5.250   1.0405   0.00956   0.00389  -0.0650   0.2360   1.0000
   5.500   1.0648   0.00973   0.00402  -0.0641   0.2332   1.0000
   5.750   1.0888   0.00991   0.00417  -0.0632   0.2301   1.0000
   6.000   1.1135   0.01004   0.00430  -0.0624   0.2286   1.0000
   6.250   1.1382   0.01017   0.00444  -0.0617   0.2269   1.0000
   6.500   1.1627   0.01031   0.00458  -0.0609   0.2250   1.0000
   6.750   1.1870   0.01047   0.00473  -0.0601   0.2228   1.0000
   7.000   1.2110   0.01064   0.00489  -0.0592   0.2202   1.0000
   7.250   1.2346   0.01084   0.00507  -0.0583   0.2171   1.0000
   7.500   1.2582   0.01104   0.00525  -0.0574   0.2142   1.0000
   7.750   1.2825   0.01119   0.00542  -0.0567   0.2124   1.0000
   8.000   1.3065   0.01136   0.00559  -0.0559   0.2101   1.0000
   8.250   1.3301   0.01154   0.00578  -0.0550   0.2073   1.0000
   8.500   1.3531   0.01176   0.00598  -0.0541   0.2039   1.0000
   8.750   1.3755   0.01201   0.00621  -0.0531   0.1998   1.0000
   9.000   1.3989   0.01220   0.00641  -0.0523   0.1970   1.0000
   9.250   1.4215   0.01242   0.00663  -0.0513   0.1930   1.0000
   9.500   1.4432   0.01270   0.00688  -0.0503   0.1884   1.0000
   9.750   1.4646   0.01297   0.00715  -0.0492   0.1840   1.0000
  10.000   1.4857   0.01325   0.00742  -0.0481   0.1781   1.0000
  10.250   1.5048   0.01364   0.00776  -0.0467   0.1714   1.0000
  10.500   1.5243   0.01398   0.00809  -0.0453   0.1648   1.0000
  10.750   1.5414   0.01443   0.00850  -0.0436   0.1577   1.0000
  11.000   1.5590   0.01483   0.00889  -0.0420   0.1519   1.0000
  11.250   1.5721   0.01530   0.00933  -0.0397   0.1464   1.0000
  11.500   1.5868   0.01569   0.00974  -0.0376   0.1425   1.0000
  11.750   1.6007   0.01614   0.01019  -0.0355   0.1384   1.0000
  12.000   1.6135   0.01668   0.01072  -0.0333   0.1345   1.0000
  12.250   1.6280   0.01718   0.01124  -0.0315   0.1316   1.0000
  12.500   1.6422   0.01771   0.01179  -0.0298   0.1286   1.0000
  12.750   1.6546   0.01836   0.01246  -0.0280   0.1254   1.0000
  13.000   1.6657   0.01914   0.01325  -0.0263   0.1222   1.0000
  13.250   1.6783   0.01986   0.01401  -0.0248   0.1200   1.0000
  13.500   1.6910   0.02064   0.01482  -0.0235   0.1181   1.0000
  13.750   1.7024   0.02154   0.01577  -0.0223   0.1160   1.0000
  14.000   1.7115   0.02267   0.01693  -0.0211   0.1134   1.0000
  14.250   1.7190   0.02400   0.01829  -0.0200   0.1109   1.0000
  14.500   1.7274   0.02535   0.01968  -0.0191   0.1083   1.0000
  14.750   1.7360   0.02677   0.02115  -0.0185   0.1063   1.0000
  15.000   1.7436   0.02832   0.02276  -0.0179   0.1048   1.0000
  15.250   1.7474   0.03028   0.02476  -0.0175   0.1024   1.0000
  15.500   1.7471   0.03269   0.02721  -0.0171   0.0994   1.0000
  15.750   1.7509   0.03477   0.02935  -0.0168   0.0982   1.0000
  16.000   1.7530   0.03706   0.03171  -0.0166   0.0962   1.0000
  16.250   1.7514   0.03975   0.03446  -0.0166   0.0942   1.0000
  16.500   1.7496   0.04253   0.03732  -0.0166   0.0932   1.0000
  16.750   1.7409   0.04611   0.04096  -0.0168   0.0909   1.0000
  17.000   1.7301   0.05007   0.04500  -0.0173   0.0892   1.0000
  17.250   1.7239   0.05361   0.04863  -0.0178   0.0883   1.0000
  17.500   1.7155   0.05750   0.05260  -0.0185   0.0867   1.0000
  17.750   1.7054   0.06169   0.05689  -0.0193   0.0859   1.0000
  18.000   1.6916   0.06640   0.06168  -0.0204   0.0842   1.0000
  18.250   1.6772   0.07124   0.06661  -0.0215   0.0831   1.0000
  18.500   1.6569   0.07691   0.07235  -0.0230   0.0812   1.0000
  18.750   1.6376   0.08250   0.07803  -0.0245   0.0797   1.0000
  19.000   1.6232   0.08751   0.08313  -0.0259   0.0786   1.0000
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