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MH 84 13.69% (mh84-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 84 13.69% (mh84-il)
Reynolds number: 500,000
Max Cl/Cd: 91.98 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh84-il-500000-n5.txt
Download as CSV file: xf-mh84-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 84  13.69%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.5628   0.06319   0.05997  -0.0319   0.8111   0.0099
 -10.500  -0.6134   0.05259   0.04918  -0.0392   0.7927   0.0098
 -10.250  -0.6470   0.04171   0.03806  -0.0507   0.7762   0.0097
  -9.750  -0.6294   0.02957   0.02510  -0.0661   0.7481   0.0098
  -9.500  -0.6098   0.02741   0.02267  -0.0675   0.7359   0.0098
  -9.250  -0.5878   0.02567   0.02068  -0.0684   0.7232   0.0099
  -9.000  -0.5643   0.02417   0.01896  -0.0691   0.7116   0.0099
  -8.750  -0.5401   0.02281   0.01738  -0.0695   0.6998   0.0100
  -8.500  -0.5153   0.02144   0.01584  -0.0700   0.6882   0.0101
  -8.250  -0.4894   0.02043   0.01467  -0.0703   0.6772   0.0103
  -8.000  -0.4627   0.01959   0.01372  -0.0704   0.6654   0.0104
  -7.750  -0.4355   0.01885   0.01286  -0.0705   0.6546   0.0106
  -7.500  -0.4081   0.01818   0.01205  -0.0706   0.6431   0.0108
  -7.250  -0.3804   0.01752   0.01127  -0.0706   0.6327   0.0110
  -7.000  -0.3526   0.01689   0.01051  -0.0706   0.6215   0.0112
  -6.750  -0.3245   0.01628   0.00978  -0.0707   0.6110   0.0113
  -6.250  -0.2678   0.01516   0.00843  -0.0706   0.5898   0.0117
  -6.000  -0.2393   0.01468   0.00782  -0.0706   0.5795   0.0119
  -5.750  -0.2105   0.01423   0.00727  -0.0706   0.5689   0.0121
  -5.500  -0.1816   0.01384   0.00677  -0.0705   0.5589   0.0124
  -5.250  -0.1528   0.01338   0.00623  -0.0705   0.5486   0.0127
  -5.000  -0.1238   0.01303   0.00580  -0.0705   0.5388   0.0131
  -4.750  -0.0948   0.01273   0.00543  -0.0704   0.5284   0.0136
  -4.500  -0.0656   0.01246   0.00507  -0.0703   0.5188   0.0142
  -4.250  -0.0364   0.01222   0.00474  -0.0702   0.5085   0.0149
  -4.000  -0.0071   0.01196   0.00442  -0.0702   0.4993   0.0159
  -3.750   0.0221   0.01176   0.00415  -0.0701   0.4891   0.0171
  -3.500   0.0514   0.01156   0.00390  -0.0701   0.4799   0.0188
  -3.250   0.0807   0.01139   0.00367  -0.0700   0.4700   0.0214
  -3.000   0.1100   0.01122   0.00346  -0.0699   0.4609   0.0254
  -2.750   0.1393   0.01105   0.00327  -0.0699   0.4513   0.0328
  -2.500   0.1686   0.01086   0.00311  -0.0699   0.4425   0.0458
  -2.250   0.1978   0.01069   0.00297  -0.0698   0.4330   0.0636
  -2.000   0.2270   0.01056   0.00287  -0.0698   0.4247   0.0831
  -1.750   0.2563   0.01045   0.00278  -0.0698   0.4154   0.1030
  -1.500   0.2855   0.01036   0.00273  -0.0698   0.4070   0.1241
  -1.250   0.3147   0.01029   0.00269  -0.0698   0.3982   0.1466
  -1.000   0.3439   0.01025   0.00267  -0.0697   0.3901   0.1678
  -0.750   0.3731   0.01022   0.00266  -0.0697   0.3814   0.1885
  -0.500   0.4022   0.01023   0.00265  -0.0696   0.3737   0.2052
  -0.250   0.4314   0.01023   0.00265  -0.0696   0.3660   0.2202
   0.000   0.4605   0.01028   0.00267  -0.0695   0.3577   0.2349
   0.250   0.4896   0.01029   0.00268  -0.0694   0.3502   0.2509
   0.500   0.5186   0.01032   0.00271  -0.0694   0.3427   0.2677
   0.750   0.5477   0.01036   0.00276  -0.0693   0.3362   0.2864
   1.000   0.5766   0.01039   0.00280  -0.0693   0.3286   0.3075
   1.250   0.6054   0.01045   0.00287  -0.0692   0.3214   0.3322
   1.500   0.6343   0.01046   0.00294  -0.0692   0.3148   0.3623
   1.750   0.6630   0.01050   0.00303  -0.0692   0.3081   0.3991
   2.000   0.6917   0.01051   0.00313  -0.0692   0.3021   0.4433
   2.250   0.7202   0.01052   0.00324  -0.0691   0.2953   0.4967
   2.750   0.7765   0.01050   0.00352  -0.0689   0.2835   0.6326
   3.000   0.8037   0.01046   0.00367  -0.0685   0.2775   0.7147
   3.250   0.8261   0.01023   0.00380  -0.0671   0.2720   0.8555
   3.500   0.8575   0.01023   0.00387  -0.0674   0.2663   1.0000
   3.750   0.8858   0.01044   0.00401  -0.0674   0.2607   1.0000
   4.000   0.9140   0.01065   0.00417  -0.0673   0.2557   1.0000
   4.250   0.9423   0.01083   0.00431  -0.0672   0.2506   1.0000
   4.500   0.9703   0.01106   0.00448  -0.0671   0.2451   1.0000
   4.750   0.9981   0.01130   0.00466  -0.0670   0.2406   1.0000
   5.000   1.0261   0.01149   0.00483  -0.0669   0.2364   1.0000
   5.250   1.0538   0.01172   0.00503  -0.0668   0.2314   1.0000
   5.500   1.0810   0.01200   0.00525  -0.0667   0.2267   1.0000
   5.750   1.1087   0.01221   0.00545  -0.0666   0.2232   1.0000
   6.000   1.1361   0.01244   0.00566  -0.0665   0.2193   1.0000
   6.250   1.1631   0.01271   0.00591  -0.0663   0.2153   1.0000
   6.500   1.1898   0.01302   0.00617  -0.0662   0.2113   1.0000
   6.750   1.2169   0.01325   0.00641  -0.0660   0.2079   1.0000
   7.000   1.2436   0.01352   0.00667  -0.0658   0.2043   1.0000
   7.250   1.2699   0.01382   0.00695  -0.0656   0.2008   1.0000
   7.500   1.2956   0.01418   0.00727  -0.0654   0.1974   1.0000
   7.750   1.3220   0.01443   0.00755  -0.0652   0.1948   1.0000
   8.000   1.3480   0.01472   0.00785  -0.0650   0.1915   1.0000
   8.250   1.3733   0.01506   0.00818  -0.0647   0.1880   1.0000
   8.500   1.3980   0.01545   0.00856  -0.0644   0.1849   1.0000
   8.750   1.4229   0.01579   0.00891  -0.0641   0.1825   1.0000
   9.000   1.4479   0.01611   0.00926  -0.0637   0.1800   1.0000
   9.250   1.4722   0.01647   0.00963  -0.0634   0.1773   1.0000
   9.500   1.4957   0.01688   0.01005  -0.0629   0.1743   1.0000
   9.750   1.5181   0.01736   0.01052  -0.0624   0.1713   1.0000
  10.000   1.5412   0.01775   0.01095  -0.0619   0.1691   1.0000
  10.250   1.5639   0.01815   0.01138  -0.0614   0.1669   1.0000
  10.500   1.5857   0.01859   0.01186  -0.0608   0.1645   1.0000
  10.750   1.6061   0.01909   0.01238  -0.0600   0.1622   1.0000
  11.000   1.6249   0.01967   0.01297  -0.0591   0.1599   1.0000
  11.250   1.6423   0.02028   0.01360  -0.0581   0.1577   1.0000
  11.500   1.6600   0.02079   0.01418  -0.0570   0.1558   1.0000
  11.750   1.6732   0.02139   0.01484  -0.0554   0.1537   1.0000
  12.000   1.6841   0.02215   0.01564  -0.0538   0.1519   1.0000
  12.250   1.6939   0.02307   0.01660  -0.0523   0.1500   1.0000
  12.500   1.7026   0.02416   0.01774  -0.0510   0.1483   1.0000
  12.750   1.7100   0.02546   0.01907  -0.0499   0.1465   1.0000
  13.000   1.7208   0.02661   0.02029  -0.0491   0.1451   1.0000
  13.250   1.7313   0.02784   0.02160  -0.0484   0.1435   1.0000
  13.500   1.7404   0.02924   0.02308  -0.0478   0.1417   1.0000
  13.750   1.7478   0.03085   0.02474  -0.0473   0.1399   1.0000
  14.000   1.7535   0.03267   0.02663  -0.0469   0.1383   1.0000
  14.250   1.7574   0.03473   0.02874  -0.0466   0.1368   1.0000
  14.500   1.7592   0.03705   0.03111  -0.0464   0.1353   1.0000
  14.750   1.7640   0.03916   0.03330  -0.0463   0.1341   1.0000
  15.000   1.7693   0.04127   0.03550  -0.0463   0.1328   1.0000
  15.250   1.7729   0.04357   0.03790  -0.0463   0.1313   1.0000
  15.500   1.7746   0.04615   0.04056  -0.0466   0.1298   1.0000
  15.750   1.7744   0.04898   0.04346  -0.0469   0.1283   1.0000
  16.000   1.7723   0.05210   0.04666  -0.0474   0.1269   1.0000
  16.250   1.7688   0.05548   0.05011  -0.0481   0.1256   1.0000
  16.500   1.7639   0.05916   0.05384  -0.0490   0.1242   1.0000
  16.750   1.7643   0.06222   0.05702  -0.0497   0.1231   1.0000
  17.000   1.7639   0.06545   0.06035  -0.0505   0.1219   1.0000
  17.250   1.7624   0.06889   0.06388  -0.0515   0.1205   1.0000
  17.500   1.7591   0.07264   0.06772  -0.0527   0.1190   1.0000
  17.750   1.7539   0.07673   0.07190  -0.0541   0.1176   1.0000
  18.000   1.7475   0.08107   0.07630  -0.0556   0.1162   1.0000
  18.250   1.7404   0.08552   0.08082  -0.0572   0.1148   1.0000
  18.500   1.7354   0.08978   0.08516  -0.0589   0.1134   1.0000
  18.750   1.7319   0.09386   0.08936  -0.0605   0.1122   1.0000
  19.000   1.7282   0.09802   0.09362  -0.0621   0.1108   1.0000
  19.250   1.7216   0.10267   0.09837  -0.0641   0.1093   1.0000
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