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MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: MH 94 16.03% (mh94-il)
Reynolds number: 200,000
Max Cl/Cd: 46.34 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh94-il-200000.txt
Download as CSV file: xf-mh94-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 94  16.03%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.5403   0.10419   0.10024  -0.0510   1.0000   0.0502
 -13.000  -0.8733   0.05757   0.05157  -0.0705   1.0000   0.0286
 -12.750  -0.8914   0.05508   0.04894  -0.0679   1.0000   0.0286
 -12.500  -0.9079   0.05298   0.04669  -0.0646   1.0000   0.0286
 -12.250  -0.9155   0.05089   0.04447  -0.0615   1.0000   0.0285
 -12.000  -0.9356   0.04940   0.04283  -0.0566   1.0000   0.0285
 -11.750  -0.9547   0.04809   0.04137  -0.0509   1.0000   0.0285
 -11.500  -0.9622   0.04638   0.03951  -0.0468   1.0000   0.0285
 -11.250  -0.9684   0.04441   0.03736  -0.0429   1.0000   0.0286
 -11.000  -0.9606   0.04225   0.03514  -0.0409   1.0000   0.0290
 -10.750  -0.9503   0.04072   0.03361  -0.0389   1.0000   0.0294
 -10.500  -0.9489   0.03895   0.03164  -0.0355   1.0000   0.0293
 -10.250  -0.9437   0.03732   0.02982  -0.0326   1.0000   0.0293
 -10.000  -0.9335   0.03583   0.02824  -0.0303   1.0000   0.0296
  -9.750  -0.9232   0.03438   0.02664  -0.0278   1.0000   0.0296
  -9.500  -0.9109   0.03311   0.02530  -0.0257   1.0000   0.0298
  -9.250  -0.8983   0.03194   0.02406  -0.0235   1.0000   0.0303
  -9.000  -0.8855   0.03082   0.02286  -0.0213   1.0000   0.0307
  -8.750  -0.8727   0.02976   0.02174  -0.0191   1.0000   0.0312
  -8.500  -0.8600   0.02877   0.02067  -0.0168   1.0000   0.0318
  -8.250  -0.8478   0.02787   0.01966  -0.0145   1.0000   0.0325
  -8.000  -0.8362   0.02680   0.01863  -0.0122   1.0000   0.0333
  -7.750  -0.8255   0.02593   0.01782  -0.0098   1.0000   0.0343
  -7.500  -0.8144   0.02513   0.01702  -0.0074   1.0000   0.0355
  -7.250  -0.7978   0.02439   0.01620  -0.0060   0.9992   0.0372
  -7.000  -0.7661   0.02349   0.01540  -0.0079   0.9948   0.0404
  -6.750  -0.7360   0.02259   0.01451  -0.0093   0.9899   0.0441
  -6.500  -0.7051   0.02175   0.01372  -0.0109   0.9848   0.0516
  -6.250  -0.6759   0.02080   0.01283  -0.0121   0.9797   0.0631
  -6.000  -0.6501   0.01938   0.01173  -0.0130   0.9737   0.1023
  -5.750  -0.6265   0.01754   0.01083  -0.0142   0.9686   0.2458
  -5.500  -0.6008   0.01673   0.01046  -0.0147   0.9618   0.3366
  -5.250  -0.5644   0.01642   0.01042  -0.0168   0.9578   0.4030
  -5.000  -0.5378   0.01620   0.01032  -0.0167   0.9505   0.4458
  -4.750  -0.5021   0.01615   0.01034  -0.0183   0.9455   0.4823
  -4.500  -0.4605   0.01620   0.01042  -0.0209   0.9425   0.5124
  -4.250  -0.4372   0.01611   0.01031  -0.0199   0.9333   0.5345
  -4.000  -0.3983   0.01615   0.01044  -0.0218   0.9293   0.5593
  -3.750  -0.3692   0.01619   0.01050  -0.0218   0.9222   0.5797
  -3.500  -0.3344   0.01615   0.01045  -0.0228   0.9162   0.5961
  -3.250  -0.2920   0.01606   0.01030  -0.0254   0.9129   0.6108
  -3.000  -0.2664   0.01600   0.01029  -0.0247   0.9041   0.6211
  -2.750  -0.2275   0.01583   0.01009  -0.0265   0.8993   0.6330
  -2.500  -0.1840   0.01565   0.00989  -0.0291   0.8963   0.6450
  -2.250  -0.1591   0.01556   0.00983  -0.0282   0.8866   0.6545
  -2.000  -0.1183   0.01533   0.00955  -0.0303   0.8822   0.6666
  -1.750  -0.0730   0.01505   0.00932  -0.0330   0.8797   0.6757
  -1.500  -0.0469   0.01489   0.00911  -0.0324   0.8697   0.6865
  -1.250  -0.0042   0.01455   0.00883  -0.0345   0.8657   0.6943
  -1.000   0.0439   0.01417   0.00841  -0.0379   0.8628   0.7048
  -0.750   0.0727   0.01395   0.00824  -0.0374   0.8528   0.7120
  -0.500   0.1151   0.01359   0.00788  -0.0396   0.8468   0.7210
  -0.250   0.1494   0.01331   0.00760  -0.0403   0.8373   0.7291
   0.000   0.1879   0.01305   0.00735  -0.0417   0.8283   0.7367
   0.250   0.2185   0.01285   0.00711  -0.0418   0.8154   0.7461
   0.500   0.2542   0.01266   0.00695  -0.0426   0.8036   0.7525
   0.750   0.2885   0.01251   0.00676  -0.0434   0.7898   0.7610
   1.000   0.3167   0.01242   0.00664  -0.0430   0.7728   0.7686
   1.250   0.3449   0.01238   0.00659  -0.0424   0.7549   0.7759
   1.500   0.3733   0.01234   0.00646  -0.0422   0.7356   0.7851
   1.750   0.3994   0.01236   0.00644  -0.0412   0.7145   0.7913
   2.000   0.4227   0.01240   0.00642  -0.0399   0.6904   0.8000
   2.250   0.4459   0.01244   0.00638  -0.0386   0.6645   0.8075
   2.500   0.4680   0.01255   0.00638  -0.0370   0.6381   0.8151
   2.750   0.4890   0.01264   0.00637  -0.0354   0.6102   0.8242
   3.000   0.5087   0.01279   0.00643  -0.0333   0.5835   0.8312
   3.250   0.5284   0.01292   0.00646  -0.0316   0.5551   0.8411
   3.500   0.5457   0.01310   0.00654  -0.0291   0.5279   0.8483
   3.750   0.5635   0.01327   0.00661  -0.0270   0.4993   0.8582
   4.000   0.5791   0.01347   0.00670  -0.0243   0.4723   0.8664
   4.250   0.5956   0.01367   0.00681  -0.0221   0.4445   0.8770
   4.500   0.6093   0.01388   0.00693  -0.0190   0.4188   0.8861
   4.750   0.6240   0.01409   0.00705  -0.0164   0.3933   0.8972
   5.000   0.6371   0.01430   0.00718  -0.0134   0.3691   0.9086
   5.250   0.6496   0.01453   0.00731  -0.0104   0.3459   0.9206
   5.500   0.6632   0.01476   0.00746  -0.0076   0.3242   0.9339
   5.750   0.6818   0.01505   0.00768  -0.0060   0.3013   0.9475
   6.000   0.7074   0.01550   0.00802  -0.0060   0.2769   0.9602
   6.250   0.7387   0.01609   0.00848  -0.0073   0.2519   0.9716
   6.500   0.7744   0.01674   0.00900  -0.0096   0.2268   0.9814
   6.750   0.8118   0.01752   0.00961  -0.0125   0.2050   0.9898
   7.000   0.8426   0.01819   0.01016  -0.0141   0.1887   1.0000
   7.250   0.8393   0.01826   0.01023  -0.0092   0.1816   1.0000
   7.500   0.8529   0.01881   0.01064  -0.0074   0.1728   1.0000
   7.750   0.8722   0.01931   0.01114  -0.0065   0.1646   1.0000
   8.000   0.8905   0.01999   0.01170  -0.0054   0.1580   1.0000
   8.250   0.9113   0.02059   0.01231  -0.0047   0.1524   1.0000
   8.500   0.9311   0.02117   0.01287  -0.0038   0.1472   1.0000
   8.750   0.9526   0.02207   0.01361  -0.0033   0.1423   1.0000
   9.000   0.9727   0.02260   0.01424  -0.0024   0.1387   1.0000
   9.250   0.9930   0.02323   0.01488  -0.0016   0.1350   1.0000
   9.500   1.0140   0.02394   0.01556  -0.0010   0.1318   1.0000
   9.750   1.0419   0.02501   0.01652  -0.0015   0.1286   1.0000
  10.000   1.0605   0.02566   0.01730  -0.0004   0.1262   1.0000
  10.250   1.0802   0.02638   0.01809   0.0004   0.1237   1.0000
  10.500   1.1002   0.02712   0.01885   0.0012   0.1211   1.0000
  10.750   1.1226   0.02794   0.01964   0.0015   0.1188   1.0000
  11.000   1.1569   0.02940   0.02102  -0.0002   0.1162   1.0000
  11.250   1.1724   0.03021   0.02198   0.0013   0.1149   1.0000
  11.500   1.1888   0.03111   0.02303   0.0025   0.1132   1.0000
  11.750   1.2047   0.03205   0.02408   0.0037   0.1115   1.0000
  12.000   1.2208   0.03300   0.02511   0.0048   0.1097   1.0000
  12.250   1.2390   0.03400   0.02615   0.0056   0.1081   1.0000
  12.500   1.2604   0.03511   0.02727   0.0059   0.1066   1.0000
  12.750   1.2916   0.03690   0.02904   0.0045   0.1049   1.0000
  13.000   1.3020   0.03843   0.03075   0.0061   0.1038   1.0000
  13.250   1.3056   0.03968   0.03221   0.0086   0.1029   1.0000
  13.500   1.3093   0.04112   0.03384   0.0108   0.1018   1.0000
  13.750   1.3129   0.04263   0.03553   0.0128   0.1007   1.0000
  14.000   1.3170   0.04429   0.03735   0.0146   0.0996   1.0000
  14.250   1.3213   0.04604   0.03925   0.0162   0.0987   1.0000
  14.500   1.3244   0.04785   0.04120   0.0177   0.0977   1.0000
  14.750   1.3270   0.04967   0.04314   0.0191   0.0968   1.0000
  15.000   1.3309   0.05155   0.04511   0.0201   0.0959   1.0000
  15.250   1.3436   0.05329   0.04686   0.0205   0.0947   1.0000
  15.500   1.3510   0.05668   0.05033   0.0207   0.0936   1.0000
  15.750   1.3294   0.05986   0.05378   0.0225   0.0933   1.0000
  16.000   1.3033   0.06381   0.05799   0.0236   0.0931   1.0000
  16.250   1.2723   0.06871   0.06317   0.0237   0.0929   1.0000
  16.500   1.2338   0.07503   0.06977   0.0225   0.0928   1.0000
  16.750   1.1805   0.08404   0.07908   0.0191   0.0928   1.0000
  17.000   1.0868   0.10099   0.09640   0.0099   0.0933   1.0000
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