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MH 27 11.99% (mh27-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 27 11.99% (mh27-il)
Reynolds number: 1,000,000
Max Cl/Cd: 61.25 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh27-il-1000000-n5.txt
Download as CSV file: xf-mh27-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 27  11.99%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.3501   0.06785   0.06604  -0.1102   0.9739   0.0022
 -10.750  -0.3793   0.05329   0.05133  -0.1243   0.9718   0.0022
 -10.500  -0.3949   0.04898   0.04690  -0.1247   0.9685   0.0022
 -10.250  -0.4131   0.04488   0.04266  -0.1229   0.9645   0.0022
 -10.000  -0.4375   0.04004   0.03759  -0.1193   0.9603   0.0021
  -9.750  -0.4577   0.03632   0.03365  -0.1141   0.9563   0.0021
  -9.500  -0.4903   0.03205   0.02908  -0.1055   0.9509   0.0020
  -9.250  -0.4996   0.02970   0.02650  -0.0999   0.9478   0.0020
  -9.000  -0.5126   0.02586   0.02223  -0.0936   0.9447   0.0019
  -8.750  -0.5149   0.02329   0.01934  -0.0886   0.9423   0.0019
  -8.500  -0.5109   0.02099   0.01670  -0.0845   0.9400   0.0019
  -8.250  -0.5004   0.01901   0.01441  -0.0816   0.9382   0.0018
  -8.000  -0.4844   0.01761   0.01278  -0.0796   0.9368   0.0018
  -7.750  -0.4657   0.01643   0.01140  -0.0781   0.9355   0.0018
  -7.500  -0.4465   0.01508   0.00983  -0.0766   0.9343   0.0018
  -7.250  -0.4252   0.01440   0.00905  -0.0756   0.9334   0.0018
  -7.000  -0.4049   0.01354   0.00806  -0.0743   0.9324   0.0018
  -6.750  -0.3839   0.01291   0.00732  -0.0732   0.9314   0.0018
  -6.500  -0.3648   0.01237   0.00670  -0.0716   0.9300   0.0019
  -6.250  -0.3462   0.01192   0.00619  -0.0698   0.9285   0.0019
  -6.000  -0.3269   0.01150   0.00570  -0.0682   0.9268   0.0019
  -5.750  -0.3065   0.01110   0.00524  -0.0668   0.9252   0.0020
  -5.500  -0.2845   0.01080   0.00488  -0.0658   0.9237   0.0021
  -5.250  -0.2620   0.01046   0.00448  -0.0648   0.9223   0.0022
  -5.000  -0.2378   0.01022   0.00421  -0.0642   0.9210   0.0023
  -4.750  -0.2140   0.00989   0.00383  -0.0635   0.9198   0.0031
  -4.500  -0.1890   0.00965   0.00357  -0.0631   0.9187   0.0038
  -4.250  -0.1635   0.00948   0.00337  -0.0627   0.9175   0.0044
  -4.000  -0.1448   0.00931   0.00323  -0.0609   0.9149   0.0092
  -3.750  -0.1239   0.00909   0.00306  -0.0596   0.9121   0.0207
  -3.500  -0.1017   0.00875   0.00285  -0.0586   0.9095   0.0494
  -3.250  -0.0814   0.00817   0.00261  -0.0573   0.9071   0.1336
  -3.000  -0.0585   0.00774   0.00239  -0.0565   0.9050   0.2000
  -2.750  -0.0403   0.00745   0.00228  -0.0547   0.9018   0.2531
  -2.500  -0.0232   0.00714   0.00217  -0.0526   0.8979   0.3170
  -2.250  -0.0075   0.00660   0.00200  -0.0502   0.8944   0.4257
  -2.000   0.0138   0.00625   0.00185  -0.0490   0.8917   0.4885
  -1.750   0.0264   0.00598   0.00179  -0.0458   0.8872   0.5506
  -1.500   0.0361   0.00562   0.00168  -0.0419   0.8821   0.6277
  -1.250   0.0491   0.00520   0.00152  -0.0386   0.8780   0.7084
  -1.000   0.0537   0.00492   0.00152  -0.0333   0.8709   0.7782
  -0.750   0.0768   0.00475   0.00156  -0.0321   0.8659   0.8436
  -0.500   0.1007   0.00476   0.00162  -0.0312   0.8595   0.8710
  -0.250   0.1270   0.00476   0.00161  -0.0308   0.8519   0.8872
   0.000   0.1542   0.00479   0.00164  -0.0306   0.8411   0.8954
   0.250   0.1761   0.00477   0.00156  -0.0292   0.8270   0.9025
   0.500   0.2076   0.00482   0.00154  -0.0301   0.8079   0.9057
   0.750   0.2325   0.00493   0.00154  -0.0294   0.7821   0.9098
   1.000   0.2441   0.00506   0.00153  -0.0258   0.7519   0.9163
   1.250   0.2642   0.00532   0.00166  -0.0240   0.7187   0.9202
   1.500   0.2702   0.00555   0.00177  -0.0190   0.6880   0.9284
   1.750   0.2836   0.00586   0.00197  -0.0158   0.6555   0.9336
   2.000   0.2955   0.00614   0.00214  -0.0122   0.6236   0.9387
   2.250   0.3017   0.00630   0.00220  -0.0075   0.5964   0.9440
   2.500   0.3213   0.00657   0.00234  -0.0059   0.5641   0.9457
   2.750   0.3402   0.00684   0.00247  -0.0042   0.5285   0.9476
   3.000   0.3585   0.00709   0.00260  -0.0024   0.4949   0.9498
   3.250   0.3753   0.00730   0.00270  -0.0002   0.4659   0.9527
   3.500   0.3849   0.00743   0.00274   0.0036   0.4404   0.9569
   3.750   0.4080   0.00771   0.00288   0.0042   0.4035   0.9580
   4.000   0.4330   0.00796   0.00303   0.0044   0.3754   0.9591
   4.250   0.4572   0.00825   0.00320   0.0048   0.3413   0.9603
   4.500   0.4810   0.00853   0.00336   0.0052   0.3109   0.9616
   4.750   0.5041   0.00880   0.00352   0.0058   0.2822   0.9631
   5.000   0.5257   0.00907   0.00368   0.0068   0.2547   0.9649
   5.250   0.5447   0.00931   0.00385   0.0083   0.2302   0.9674
   5.500   0.5595   0.00953   0.00399   0.0108   0.2084   0.9705
   5.750   0.5850   0.00992   0.00423   0.0107   0.1741   0.9713
   6.000   0.6111   0.01027   0.00447   0.0105   0.1475   0.9720
   6.250   0.6363   0.01067   0.00475   0.0104   0.1187   0.9727
   6.500   0.6627   0.01099   0.00502   0.0102   0.1008   0.9734
   6.750   0.6885   0.01136   0.00531   0.0100   0.0816   0.9741
   7.000   0.7140   0.01172   0.00560   0.0099   0.0662   0.9749
   7.250   0.7388   0.01207   0.00591   0.0099   0.0538   0.9758
   7.500   0.7625   0.01245   0.00623   0.0102   0.0416   0.9768
   7.750   0.7854   0.01283   0.00658   0.0106   0.0318   0.9781
   8.000   0.8072   0.01320   0.00695   0.0113   0.0249   0.9797
   8.250   0.8255   0.01352   0.00727   0.0128   0.0207   0.9819
   8.500   0.8457   0.01391   0.00765   0.0138   0.0162   0.9832
   8.750   0.8708   0.01430   0.00805   0.0136   0.0127   0.9837
   9.000   0.8949   0.01476   0.00850   0.0136   0.0099   0.9842
   9.250   0.9192   0.01517   0.00893   0.0136   0.0084   0.9848
   9.500   0.9429   0.01560   0.00938   0.0136   0.0064   0.9855
   9.750   0.9653   0.01610   0.00989   0.0139   0.0047   0.9862
  10.000   0.9877   0.01657   0.01041   0.0142   0.0038   0.9870
  10.250   1.0088   0.01712   0.01098   0.0147   0.0026   0.9879
  10.500   1.0295   0.01768   0.01159   0.0152   0.0020   0.9889
  10.750   1.0478   0.01838   0.01234   0.0161   0.0013   0.9901
  11.000   1.0669   0.01893   0.01294   0.0169   0.0013   0.9912
  11.250   1.0849   0.01951   0.01359   0.0179   0.0012   0.9923
  11.500   1.1006   0.02019   0.01435   0.0193   0.0010   0.9935
  11.750   1.1182   0.02085   0.01508   0.0202   0.0010   0.9944
  12.000   1.1355   0.02166   0.01597   0.0209   0.0010   0.9952
  12.250   1.1522   0.02249   0.01689   0.0217   0.0008   0.9961
  12.500   1.1680   0.02339   0.01790   0.0226   0.0008   0.9970
  12.750   1.1833   0.02427   0.01885   0.0236   0.0007   0.9979
  13.000   1.1954   0.02541   0.02009   0.0248   0.0006   0.9987
  13.250   1.2088   0.02643   0.02120   0.0259   0.0006   0.9993
  13.500   1.2153   0.02803   0.02296   0.0276   0.0005   0.9999
  13.750   1.2186   0.02905   0.02406   0.0304   0.0005   1.0000
  14.000   1.2171   0.03034   0.02545   0.0338   0.0005   1.0000
  14.250   1.2187   0.03146   0.02666   0.0366   0.0004   1.0000
  14.500   1.2111   0.03334   0.02868   0.0402   0.0005   1.0000
  14.750   1.2127   0.03463   0.03006   0.0425   0.0005   1.0000
  15.000   1.2182   0.03569   0.03117   0.0444   0.0004   1.0000
  15.250   1.2087   0.03814   0.03379   0.0470   0.0004   1.0000
  15.500   1.2081   0.03997   0.03572   0.0487   0.0004   1.0000
  15.750   1.1958   0.04314   0.03905   0.0504   0.0004   1.0000
  16.000   1.1930   0.04557   0.04158   0.0513   0.0004   1.0000
  16.250   1.1946   0.04769   0.04378   0.0519   0.0004   1.0000
  16.500   1.1741   0.05264   0.04893   0.0520   0.0004   1.0000
  16.750   1.1762   0.05507   0.05142   0.0518   0.0004   1.0000
  17.000   1.1510   0.06141   0.05798   0.0503   0.0004   1.0000
  17.250   1.1484   0.06488   0.06153   0.0493   0.0004   1.0000
  17.500   1.1322   0.07066   0.06745   0.0471   0.0004   1.0000
  17.750   1.1117   0.07747   0.07442   0.0442   0.0004   1.0000
  18.000   1.0994   0.08314   0.08019   0.0416   0.0003   1.0000
  18.250   1.0659   0.09296   0.09019   0.0369   0.0004   1.0000
  18.500   1.0193   0.10567   0.10311   0.0309   0.0004   1.0000
  18.750   0.9943   0.11447   0.11201   0.0268   0.0004   1.0000
  19.000   0.9603   0.12529   0.12296   0.0218   0.0004   1.0000
  19.250   0.9272   0.13633   0.13410   0.0168   0.0004   1.0000
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