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MH 106 13.07% (mh106-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: MH 106 13.07% (mh106-il)
Reynolds number: 100,000
Max Cl/Cd: 44.6 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh106-il-100000-n5.txt
Download as CSV file: xf-mh106-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 106  13.07%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.6861   0.09952   0.09454  -0.0010   1.0000   0.0166
 -12.250  -0.7155   0.08817   0.08308  -0.0088   1.0000   0.0161
 -12.000  -0.7442   0.07836   0.07309  -0.0160   1.0000   0.0158
 -11.750  -0.7687   0.07059   0.06512  -0.0217   1.0000   0.0156
 -11.500  -0.7892   0.06449   0.05880  -0.0255   1.0000   0.0154
 -11.250  -0.8072   0.05952   0.05359  -0.0278   1.0000   0.0153
 -11.000  -0.8229   0.05540   0.04924  -0.0285   1.0000   0.0153
 -10.750  -0.8345   0.05209   0.04570  -0.0279   1.0000   0.0153
 -10.500  -0.8434   0.04918   0.04256  -0.0264   1.0000   0.0154
 -10.250  -0.8494   0.04651   0.03965  -0.0241   1.0000   0.0154
 -10.000  -0.8507   0.04406   0.03696  -0.0218   1.0000   0.0156
  -9.750  -0.8463   0.04164   0.03428  -0.0199   1.0000   0.0158
  -9.500  -0.8382   0.03932   0.03171  -0.0182   1.0000   0.0161
  -9.250  -0.8269   0.03717   0.02933  -0.0166   1.0000   0.0164
  -9.000  -0.8134   0.03511   0.02705  -0.0151   1.0000   0.0169
  -8.750  -0.7981   0.03331   0.02504  -0.0137   1.0000   0.0177
  -8.500  -0.7813   0.03181   0.02330  -0.0123   1.0000   0.0189
  -8.250  -0.7673   0.03010   0.02158  -0.0109   1.0000   0.0200
  -8.000  -0.7515   0.02879   0.02023  -0.0095   1.0000   0.0215
  -7.750  -0.7354   0.02744   0.01879  -0.0079   1.0000   0.0230
  -7.500  -0.7196   0.02615   0.01738  -0.0061   1.0000   0.0244
  -7.250  -0.7053   0.02482   0.01596  -0.0042   1.0000   0.0261
  -7.000  -0.6896   0.02368   0.01479  -0.0026   1.0000   0.0298
  -6.750  -0.6732   0.02259   0.01360  -0.0008   1.0000   0.0345
  -6.500  -0.6568   0.02144   0.01236   0.0009   1.0000   0.0417
  -6.250  -0.6413   0.02017   0.01119   0.0027   1.0000   0.0571
  -6.000  -0.6282   0.01863   0.01006   0.0047   1.0000   0.1055
  -5.750  -0.6151   0.01736   0.00941   0.0066   1.0000   0.1977
  -5.500  -0.5980   0.01678   0.00907   0.0082   1.0000   0.2567
  -5.250  -0.5655   0.01635   0.00874   0.0068   0.9737   0.3060
  -5.000  -0.5280   0.01604   0.00845   0.0047   0.9339   0.3501
  -4.750  -0.4898   0.01577   0.00811   0.0027   0.8977   0.3806
  -4.500  -0.4567   0.01553   0.00775   0.0020   0.8630   0.4019
  -4.250  -0.4284   0.01534   0.00740   0.0023   0.8309   0.4208
  -4.000  -0.4027   0.01517   0.00708   0.0031   0.8019   0.4384
  -3.750  -0.3778   0.01500   0.00681   0.0040   0.7761   0.4563
  -3.500  -0.3531   0.01485   0.00655   0.0050   0.7524   0.4754
  -3.250  -0.3281   0.01471   0.00630   0.0058   0.7308   0.4957
  -3.000  -0.3032   0.01455   0.00608   0.0067   0.7106   0.5166
  -2.750  -0.2780   0.01442   0.00588   0.0075   0.6922   0.5397
  -2.500  -0.2527   0.01429   0.00572   0.0083   0.6752   0.5640
  -2.250  -0.2271   0.01417   0.00557   0.0091   0.6588   0.5901
  -2.000  -0.2012   0.01407   0.00546   0.0098   0.6436   0.6185
  -1.750  -0.1749   0.01399   0.00537   0.0105   0.6295   0.6481
  -1.500  -0.1481   0.01393   0.00532   0.0111   0.6162   0.6792
  -1.250  -0.1205   0.01390   0.00528   0.0115   0.6032   0.7109
  -1.000  -0.0920   0.01389   0.00528   0.0118   0.5909   0.7428
  -0.750  -0.0623   0.01393   0.00531   0.0119   0.5797   0.7740
  -0.500  -0.0310   0.01401   0.00535   0.0117   0.5697   0.8034
  -0.250   0.0024   0.01412   0.00543   0.0111   0.5590   0.8302
   0.000   0.0367   0.01426   0.00552   0.0102   0.5488   0.8544
   0.250   0.0725   0.01443   0.00560   0.0090   0.5401   0.8752
   0.500   0.1072   0.01459   0.00571   0.0079   0.5310   0.8950
   0.750   0.1437   0.01478   0.00582   0.0064   0.5227   0.9118
   1.000   0.1807   0.01496   0.00593   0.0048   0.5144   0.9266
   1.250   0.2184   0.01514   0.00606   0.0029   0.5066   0.9401
   1.500   0.2586   0.01531   0.00616   0.0005   0.4991   0.9513
   1.750   0.2981   0.01547   0.00629  -0.0019   0.4914   0.9624
   2.000   0.3370   0.01561   0.00638  -0.0042   0.4844   0.9733
   2.250   0.3765   0.01574   0.00651  -0.0068   0.4772   0.9838
   2.500   0.4175   0.01584   0.00658  -0.0097   0.4701   0.9933
   2.750   0.4549   0.01593   0.00669  -0.0120   0.4632   1.0000
   3.000   0.4768   0.01606   0.00682  -0.0111   0.4570   1.0000
   3.250   0.4989   0.01621   0.00695  -0.0102   0.4516   1.0000
   3.500   0.5211   0.01638   0.00719  -0.0094   0.4447   1.0000
   3.750   0.5434   0.01656   0.00733  -0.0085   0.4393   1.0000
   4.000   0.5658   0.01676   0.00762  -0.0077   0.4323   1.0000
   4.250   0.5883   0.01695   0.00781  -0.0068   0.4260   1.0000
   4.500   0.6108   0.01717   0.00811  -0.0059   0.4192   1.0000
   4.750   0.6333   0.01737   0.00834  -0.0050   0.4121   1.0000
   5.000   0.6558   0.01760   0.00863  -0.0041   0.4048   1.0000
   5.250   0.6783   0.01780   0.00888  -0.0032   0.3971   1.0000
   5.500   0.7006   0.01804   0.00922  -0.0023   0.3889   1.0000
   5.750   0.7232   0.01823   0.00944  -0.0013   0.3809   1.0000
   6.000   0.7452   0.01847   0.00982  -0.0004   0.3713   1.0000
   6.250   0.7675   0.01869   0.01009   0.0006   0.3626   1.0000
   6.500   0.7895   0.01890   0.01040   0.0016   0.3525   1.0000
   6.750   0.8112   0.01914   0.01079   0.0026   0.3413   1.0000
   7.000   0.8328   0.01938   0.01114   0.0037   0.3297   1.0000
   7.250   0.8541   0.01962   0.01148   0.0047   0.3170   1.0000
   7.500   0.8750   0.01988   0.01187   0.0058   0.3028   1.0000
   7.750   0.8955   0.02018   0.01227   0.0070   0.2869   1.0000
   8.000   0.9151   0.02052   0.01268   0.0082   0.2694   1.0000
   8.250   0.9336   0.02095   0.01312   0.0096   0.2507   1.0000
   8.500   0.9512   0.02151   0.01371   0.0109   0.2304   1.0000
   8.750   0.9667   0.02222   0.01438   0.0125   0.2106   1.0000
   9.000   0.9812   0.02305   0.01524   0.0141   0.1922   1.0000
   9.250   0.9942   0.02398   0.01617   0.0157   0.1744   1.0000
   9.500   1.0057   0.02500   0.01720   0.0175   0.1589   1.0000
   9.750   1.0157   0.02610   0.01832   0.0194   0.1451   1.0000
  10.000   1.0238   0.02727   0.01952   0.0213   0.1328   1.0000
  10.250   1.0297   0.02853   0.02081   0.0234   0.1224   1.0000
  10.500   1.0316   0.02993   0.02221   0.0257   0.1138   1.0000
  10.750   1.0318   0.03130   0.02368   0.0282   0.1055   1.0000
  11.000   1.0272   0.03312   0.02547   0.0302   0.0997   1.0000
  11.250   1.0269   0.03503   0.02756   0.0313   0.0927   1.0000
  11.500   1.0222   0.03753   0.03006   0.0317   0.0876   1.0000
  11.750   1.0221   0.03991   0.03257   0.0319   0.0818   1.0000
  12.000   1.0185   0.04277   0.03548   0.0316   0.0769   1.0000
  12.250   1.0157   0.04565   0.03840   0.0312   0.0727   1.0000
  12.500   1.0136   0.04862   0.04151   0.0306   0.0676   1.0000
  12.750   1.0083   0.05199   0.04489   0.0297   0.0640   1.0000
  13.000   1.0052   0.05520   0.04820   0.0291   0.0599   1.0000
  13.250   1.0023   0.05849   0.05160   0.0282   0.0563   1.0000
  13.500   0.9965   0.06220   0.05536   0.0269   0.0533   1.0000
  13.750   0.9913   0.06583   0.05901   0.0258   0.0503   1.0000
  14.000   0.9876   0.06947   0.06282   0.0247   0.0473   1.0000
  14.250   0.9826   0.07332   0.06677   0.0233   0.0448   1.0000
  14.500   0.9752   0.07772   0.07121   0.0214   0.0424   1.0000
  14.750   0.9712   0.08155   0.07506   0.0201   0.0405   1.0000
  15.000   0.9650   0.08617   0.07988   0.0183   0.0383   1.0000
  15.250   0.9590   0.09078   0.08463   0.0163   0.0365   1.0000
  15.500   0.9522   0.09563   0.08958   0.0141   0.0348   1.0000
  15.750   0.9450   0.10067   0.09466   0.0117   0.0333   1.0000
  16.000   0.9398   0.10520   0.09918   0.0097   0.0317   1.0000
  16.250   0.9304   0.11106   0.10524   0.0069   0.0309   1.0000
  16.500   0.9162   0.11819   0.11256   0.0032   0.0299   1.0000
  16.750   0.9026   0.12534   0.11989  -0.0004   0.0294   1.0000
  17.000   0.8834   0.13418   0.12888  -0.0051   0.0287   1.0000
  17.250   0.8575   0.14524   0.14011  -0.0109   0.0290   1.0000
  17.500   0.8075   0.16451   0.15943  -0.0205   0.0297   1.0000
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