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MH 200 12.97% (mh200-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 200 12.97% (mh200-il)
Reynolds number: 200,000
Max Cl/Cd: 66.65 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh200-il-200000-n5.txt
Download as CSV file: xf-mh200-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 200  12.97%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.4466   0.08557   0.08205  -0.0556   1.0000   0.0110
 -10.500  -0.4595   0.07793   0.07445  -0.0592   1.0000   0.0107
 -10.250  -0.4836   0.06803   0.06452  -0.0657   1.0000   0.0105
 -10.000  -0.5083   0.06235   0.05881  -0.0684   1.0000   0.0104
  -9.750  -0.5306   0.05754   0.05391  -0.0704   0.9974   0.0103
  -9.500  -0.5390   0.05148   0.04757  -0.0762   0.9837   0.0101
  -9.250  -0.5456   0.04678   0.04257  -0.0787   0.9669   0.0100
  -9.000  -0.5432   0.04190   0.03727  -0.0805   0.9546   0.0098
  -8.750  -0.5358   0.03747   0.03235  -0.0814   0.9440   0.0096
  -8.500  -0.5233   0.03385   0.02823  -0.0816   0.9344   0.0094
  -8.250  -0.5038   0.03060   0.02450  -0.0821   0.9280   0.0094
  -8.000  -0.4847   0.02812   0.02161  -0.0818   0.9198   0.0094
  -7.750  -0.4599   0.02596   0.01909  -0.0822   0.9145   0.0094
  -7.500  -0.4374   0.02423   0.01709  -0.0818   0.9074   0.0095
  -7.250  -0.4118   0.02270   0.01534  -0.0819   0.9019   0.0096
  -7.000  -0.3874   0.02139   0.01385  -0.0817   0.8960   0.0099
  -6.750  -0.3639   0.02027   0.01258  -0.0812   0.8898   0.0102
  -6.500  -0.3393   0.01922   0.01138  -0.0810   0.8852   0.0106
  -6.250  -0.3183   0.01837   0.01043  -0.0801   0.8789   0.0111
  -6.000  -0.2954   0.01760   0.00954  -0.0795   0.8738   0.0116
  -5.750  -0.2732   0.01675   0.00859  -0.0790   0.8692   0.0126
  -5.500  -0.2506   0.01622   0.00800  -0.0783   0.8635   0.0148
  -5.250  -0.2268   0.01564   0.00732  -0.0779   0.8590   0.0181
  -5.000  -0.2020   0.01506   0.00664  -0.0775   0.8555   0.0240
  -4.750  -0.1809   0.01432   0.00606  -0.0767   0.8504   0.0512
  -4.500  -0.1603   0.01339   0.00557  -0.0762   0.8459   0.1401
  -4.250  -0.1391   0.01245   0.00517  -0.0758   0.8423   0.2646
  -4.000  -0.1191   0.01163   0.00489  -0.0752   0.8380   0.3918
  -3.750  -0.0973   0.01108   0.00475  -0.0744   0.8337   0.4974
  -3.500  -0.0731   0.01081   0.00476  -0.0736   0.8302   0.5761
  -3.250  -0.0466   0.01078   0.00479  -0.0731   0.8273   0.6264
  -3.000  -0.0212   0.01084   0.00486  -0.0724   0.8232   0.6584
  -2.750   0.0054   0.01092   0.00489  -0.0720   0.8193   0.6826
  -2.500   0.0328   0.01099   0.00489  -0.0718   0.8159   0.7008
  -2.250   0.0610   0.01107   0.00487  -0.0718   0.8130   0.7156
  -2.000   0.0873   0.01115   0.00489  -0.0714   0.8089   0.7285
  -1.750   0.1137   0.01124   0.00494  -0.0711   0.8048   0.7389
  -1.500   0.1412   0.01131   0.00495  -0.0709   0.8013   0.7482
  -1.250   0.1697   0.01136   0.00491  -0.0710   0.7984   0.7581
  -1.000   0.1947   0.01146   0.00502  -0.0703   0.7938   0.7664
  -0.750   0.2212   0.01154   0.00507  -0.0700   0.7896   0.7750
  -0.500   0.2487   0.01159   0.00507  -0.0698   0.7860   0.7823
  -0.250   0.2763   0.01162   0.00507  -0.0697   0.7822   0.7885
   0.000   0.3016   0.01168   0.00514  -0.0692   0.7768   0.7937
   0.250   0.3296   0.01169   0.00510  -0.0693   0.7721   0.7997
   0.500   0.3567   0.01170   0.00510  -0.0691   0.7675   0.8042
   0.750   0.3821   0.01173   0.00515  -0.0686   0.7613   0.8091
   1.000   0.4107   0.01172   0.00511  -0.0687   0.7562   0.8147
   1.250   0.4358   0.01175   0.00517  -0.0681   0.7499   0.8189
   1.500   0.4623   0.01175   0.00518  -0.0678   0.7435   0.8235
   1.750   0.4894   0.01175   0.00517  -0.0677   0.7368   0.8285
   2.000   0.5155   0.01172   0.00517  -0.0673   0.7290   0.8323
   2.250   0.5409   0.01171   0.00520  -0.0668   0.7205   0.8360
   2.500   0.5682   0.01168   0.00516  -0.0666   0.7123   0.8401
   2.750   0.5940   0.01168   0.00521  -0.0663   0.7021   0.8445
   3.000   0.6191   0.01167   0.00525  -0.0657   0.6924   0.8477
   3.250   0.6450   0.01165   0.00526  -0.0653   0.6819   0.8513
   3.500   0.6704   0.01165   0.00530  -0.0648   0.6695   0.8555
   3.750   0.6957   0.01165   0.00534  -0.0644   0.6551   0.8595
   4.000   0.7193   0.01166   0.00541  -0.0634   0.6378   0.8629
   4.250   0.7431   0.01168   0.00544  -0.0626   0.6163   0.8670
   4.500   0.7672   0.01174   0.00546  -0.0618   0.5889   0.8715
   4.750   0.7890   0.01188   0.00551  -0.0606   0.5569   0.8754
   5.000   0.8085   0.01213   0.00563  -0.0590   0.5208   0.8799
   5.250   0.8270   0.01249   0.00583  -0.0573   0.4822   0.8852
   5.500   0.8435   0.01289   0.00609  -0.0553   0.4435   0.8901
   5.750   0.8588   0.01334   0.00641  -0.0531   0.4060   0.8959
   6.000   0.8742   0.01382   0.00679  -0.0511   0.3706   0.9025
   6.250   0.8879   0.01430   0.00716  -0.0487   0.3375   0.9094
   6.500   0.9024   0.01480   0.00756  -0.0466   0.3058   0.9172
   6.750   0.9158   0.01529   0.00797  -0.0442   0.2773   0.9270
   7.000   0.9290   0.01577   0.00840  -0.0419   0.2511   0.9395
   7.500   0.9662   0.01689   0.00943  -0.0400   0.2005   1.0000
   7.750   0.9835   0.01756   0.01002  -0.0389   0.1793   1.0000
   8.000   1.0007   0.01824   0.01065  -0.0379   0.1592   1.0000
   8.500   1.0332   0.01972   0.01201  -0.0356   0.1227   1.0000
   8.750   1.0486   0.02052   0.01279  -0.0343   0.1060   1.0000
   9.000   1.0633   0.02137   0.01360  -0.0330   0.0912   1.0000
   9.250   1.0777   0.02224   0.01446  -0.0317   0.0788   1.0000
   9.500   1.0916   0.02317   0.01539  -0.0304   0.0682   1.0000
   9.750   1.1047   0.02416   0.01639  -0.0291   0.0591   1.0000
  10.250   1.1295   0.02629   0.01859  -0.0263   0.0460   1.0000
  10.500   1.1390   0.02759   0.01993  -0.0248   0.0409   1.0000
  10.750   1.1511   0.02872   0.02117  -0.0236   0.0371   1.0000
  11.000   1.1613   0.03000   0.02251  -0.0223   0.0334   1.0000
  11.250   1.1682   0.03158   0.02414  -0.0208   0.0305   1.0000
  11.500   1.1792   0.03286   0.02555  -0.0198   0.0278   1.0000
  11.750   1.1880   0.03434   0.02713  -0.0186   0.0254   1.0000
  12.000   1.1927   0.03619   0.02904  -0.0174   0.0234   1.0000
  12.250   1.1990   0.03797   0.03095  -0.0162   0.0216   1.0000
  12.500   1.2068   0.03964   0.03276  -0.0154   0.0197   1.0000
  12.750   1.2130   0.04148   0.03470  -0.0146   0.0180   1.0000
  13.000   1.2130   0.04395   0.03727  -0.0137   0.0166   1.0000
  13.250   1.2171   0.04614   0.03962  -0.0130   0.0154   1.0000
  13.500   1.2215   0.04834   0.04197  -0.0125   0.0139   1.0000
  13.750   1.2232   0.05087   0.04463  -0.0122   0.0129   1.0000
  14.000   1.2219   0.05382   0.04767  -0.0121   0.0119   1.0000
  14.250   1.2192   0.05709   0.05109  -0.0120   0.0111   1.0000
  14.500   1.2190   0.06020   0.05439  -0.0123   0.0102   1.0000
  14.750   1.2162   0.06377   0.05812  -0.0128   0.0096   1.0000
  15.000   1.2140   0.06741   0.06190  -0.0137   0.0088   1.0000
  15.250   1.2087   0.07166   0.06629  -0.0150   0.0085   1.0000
  15.500   1.2002   0.07660   0.07138  -0.0167   0.0082   1.0000
  15.750   1.1884   0.08233   0.07726  -0.0190   0.0079   1.0000
  16.000   1.1793   0.08785   0.08297  -0.0213   0.0077   1.0000
  16.250   1.1691   0.09384   0.08916  -0.0241   0.0075   1.0000
  16.500   1.1578   0.10023   0.09574  -0.0272   0.0074   1.0000
  16.750   1.1454   0.10706   0.10275  -0.0308   0.0072   1.0000
  17.000   1.1330   0.11412   0.11000  -0.0347   0.0070   1.0000
  17.250   1.1194   0.12161   0.11765  -0.0389   0.0070   1.0000
  17.500   1.1054   0.12949   0.12570  -0.0435   0.0069   1.0000
  17.750   1.0913   0.13757   0.13394  -0.0483   0.0069   1.0000
  18.000   1.0768   0.14599   0.14250  -0.0534   0.0069   1.0000
  18.250   1.0619   0.15481   0.15147  -0.0587   0.0069   1.0000
  18.500   1.0454   0.16441   0.16120  -0.0646   0.0070   1.0000
  18.750   1.0269   0.17507   0.17198  -0.0709   0.0071   1.0000
  19.000   1.0027   0.18819   0.18521  -0.0784   0.0074   1.0000
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