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MH 106 13.07% (mh106-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 106 13.07% (mh106-il)
Reynolds number: 500,000
Max Cl/Cd: 86.64 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh106-il-500000.txt
Download as CSV file: xf-mh106-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.6915   0.07275   0.07020  -0.0142   1.0000   0.0098
 -12.250  -0.7110   0.06497   0.06231  -0.0185   1.0000   0.0097
 -12.000  -0.7332   0.05721   0.05441  -0.0226   1.0000   0.0096
 -11.750  -0.7584   0.04973   0.04679  -0.0263   1.0000   0.0096
 -11.500  -0.7784   0.04402   0.04092  -0.0287   1.0000   0.0095
 -11.250  -0.8563   0.04886   0.04539  -0.0308   1.0000   0.0098
 -11.000  -0.8766   0.04481   0.04115  -0.0296   1.0000   0.0095
 -10.750  -0.8914   0.04174   0.03790  -0.0270   1.0000   0.0092
 -10.500  -0.9395   0.03418   0.02943  -0.0194   1.0000   0.0076
 -10.250  -0.9360   0.03189   0.02690  -0.0168   1.0000   0.0075
 -10.000  -0.9281   0.02975   0.02455  -0.0146   1.0000   0.0076
  -9.750  -0.9173   0.02776   0.02235  -0.0127   1.0000   0.0076
  -9.500  -0.9044   0.02595   0.02042  -0.0109   1.0000   0.0078
  -9.250  -0.8892   0.02449   0.01883  -0.0093   1.0000   0.0079
  -9.000  -0.8729   0.02319   0.01745  -0.0078   1.0000   0.0081
  -8.750  -0.8554   0.02209   0.01626  -0.0064   1.0000   0.0084
  -8.500  -0.8374   0.02101   0.01510  -0.0050   1.0000   0.0086
  -8.250  -0.8188   0.02004   0.01405  -0.0036   1.0000   0.0089
  -8.000  -0.8007   0.01899   0.01292  -0.0020   1.0000   0.0091
  -7.750  -0.7823   0.01805   0.01189  -0.0004   1.0000   0.0093
  -7.500  -0.7632   0.01722   0.01100   0.0011   1.0000   0.0096
  -7.250  -0.7419   0.01667   0.01039   0.0022   1.0000   0.0101
  -7.000  -0.7272   0.01548   0.00915   0.0044   1.0000   0.0109
  -6.750  -0.7080   0.01481   0.00845   0.0059   1.0000   0.0116
  -6.500  -0.6882   0.01422   0.00784   0.0074   1.0000   0.0124
  -6.250  -0.6604   0.01358   0.00713   0.0072   0.9926   0.0134
  -6.000  -0.6210   0.01264   0.00612   0.0046   0.9590   0.0165
  -5.750  -0.5822   0.01173   0.00517   0.0023   0.9071   0.0320
  -5.500  -0.5647   0.01076   0.00445   0.0042   0.8566   0.1000
  -5.250  -0.5467   0.01002   0.00399   0.0059   0.8190   0.1815
  -5.000  -0.5244   0.00968   0.00372   0.0070   0.7879   0.2314
  -4.750  -0.5006   0.00946   0.00352   0.0079   0.7611   0.2650
  -4.500  -0.4759   0.00929   0.00334   0.0086   0.7366   0.2946
  -4.250  -0.4508   0.00914   0.00318   0.0092   0.7141   0.3217
  -4.000  -0.4252   0.00903   0.00302   0.0097   0.6924   0.3428
  -3.750  -0.3995   0.00891   0.00288   0.0102   0.6723   0.3665
  -3.500  -0.3736   0.00880   0.00275   0.0107   0.6532   0.3899
  -3.250  -0.3474   0.00871   0.00262   0.0111   0.6355   0.4081
  -3.000  -0.3212   0.00861   0.00248   0.0115   0.6189   0.4260
  -2.750  -0.2949   0.00852   0.00237   0.0119   0.6031   0.4450
  -2.500  -0.2685   0.00845   0.00226   0.0123   0.5879   0.4653
  -2.250  -0.2423   0.00835   0.00217   0.0127   0.5734   0.4863
  -2.000  -0.2160   0.00826   0.00208   0.0131   0.5597   0.5101
  -1.750  -0.1900   0.00815   0.00201   0.0136   0.5473   0.5356
  -1.500  -0.1640   0.00806   0.00195   0.0141   0.5359   0.5635
  -1.250  -0.1382   0.00797   0.00190   0.0146   0.5252   0.5937
  -1.000  -0.1125   0.00787   0.00187   0.0151   0.5147   0.6258
  -0.750  -0.0868   0.00778   0.00185   0.0157   0.5051   0.6593
  -0.500  -0.0614   0.00771   0.00184   0.0163   0.4966   0.6925
  -0.250  -0.0357   0.00762   0.00185   0.0170   0.4883   0.7267
   0.000  -0.0100   0.00758   0.00187   0.0176   0.4810   0.7597
   0.250   0.0161   0.00752   0.00189   0.0182   0.4734   0.7921
   0.500   0.0423   0.00751   0.00194   0.0188   0.4669   0.8231
   0.750   0.0697   0.00749   0.00200   0.0192   0.4603   0.8523
   1.000   0.0983   0.00755   0.00208   0.0193   0.4542   0.8789
   1.250   0.1296   0.00760   0.00218   0.0188   0.4482   0.9009
   1.500   0.1630   0.00771   0.00228   0.0179   0.4422   0.9188
   1.750   0.1980   0.00786   0.00240   0.0166   0.4365   0.9326
   2.000   0.2332   0.00798   0.00252   0.0152   0.4307   0.9437
   2.250   0.2655   0.00815   0.00263   0.0144   0.4253   0.9545
   2.500   0.3061   0.00829   0.00278   0.0119   0.4194   0.9589
   2.750   0.3432   0.00843   0.00290   0.0100   0.4139   0.9650
   3.000   0.3795   0.00862   0.00303   0.0083   0.4085   0.9704
   3.250   0.4197   0.00870   0.00314   0.0058   0.4026   0.9742
   3.500   0.4560   0.00884   0.00325   0.0040   0.3969   0.9797
   3.750   0.4941   0.00895   0.00337   0.0019   0.3908   0.9836
   4.000   0.5341   0.00901   0.00344  -0.0007   0.3842   0.9870
   4.250   0.5722   0.00913   0.00353  -0.0029   0.3780   0.9911
   4.500   0.6110   0.00917   0.00362  -0.0053   0.3712   0.9946
   4.750   0.6510   0.00925   0.00368  -0.0080   0.3642   0.9980
   5.000   0.6854   0.00926   0.00374  -0.0095   0.3571   1.0000
   5.250   0.7084   0.00937   0.00383  -0.0086   0.3507   1.0000
   5.500   0.7322   0.00938   0.00392  -0.0079   0.3437   1.0000
   5.750   0.7553   0.00950   0.00401  -0.0070   0.3362   1.0000
   6.000   0.7791   0.00954   0.00412  -0.0063   0.3275   1.0000
   6.250   0.8025   0.00965   0.00425  -0.0055   0.3180   1.0000
   6.500   0.8258   0.00979   0.00438  -0.0047   0.3077   1.0000
   6.750   0.8493   0.00991   0.00453  -0.0039   0.2949   1.0000
   7.000   0.8723   0.01010   0.00470  -0.0031   0.2794   1.0000
   7.250   0.8950   0.01033   0.00492  -0.0022   0.2604   1.0000
   7.500   0.9165   0.01068   0.00520  -0.0012   0.2380   1.0000
   7.750   0.9375   0.01110   0.00554  -0.0002   0.2146   1.0000
   8.000   0.9576   0.01161   0.00595   0.0010   0.1910   1.0000
   8.250   0.9773   0.01214   0.00640   0.0022   0.1695   1.0000
   8.500   0.9969   0.01267   0.00687   0.0034   0.1510   1.0000
   8.750   1.0163   0.01322   0.00738   0.0046   0.1337   1.0000
   9.000   1.0350   0.01379   0.00790   0.0059   0.1179   1.0000
   9.250   1.0534   0.01439   0.00845   0.0072   0.1039   1.0000
   9.500   1.0716   0.01497   0.00901   0.0086   0.0918   1.0000
   9.750   1.0895   0.01556   0.00959   0.0100   0.0813   1.0000
  10.000   1.1065   0.01620   0.01021   0.0114   0.0716   1.0000
  10.250   1.1220   0.01692   0.01091   0.0131   0.0623   1.0000
  10.500   1.1382   0.01755   0.01155   0.0146   0.0550   1.0000
  10.750   1.1530   0.01825   0.01227   0.0163   0.0480   1.0000
  11.000   1.1637   0.01916   0.01315   0.0184   0.0410   1.0000
  11.250   1.1776   0.01982   0.01385   0.0201   0.0362   1.0000
  11.500   1.1850   0.02081   0.01484   0.0225   0.0313   1.0000
  11.750   1.1924   0.02161   0.01570   0.0251   0.0279   1.0000
  12.000   1.1881   0.02288   0.01698   0.0287   0.0245   1.0000
  12.250   1.1925   0.02399   0.01817   0.0307   0.0222   1.0000
  12.500   1.1929   0.02566   0.01990   0.0321   0.0199   1.0000
  12.750   1.1882   0.02817   0.02248   0.0326   0.0178   1.0000
  13.000   1.1901   0.03043   0.02486   0.0326   0.0165   1.0000
  13.250   1.1892   0.03317   0.02766   0.0321   0.0148   1.0000
  13.500   1.1820   0.03678   0.03135   0.0312   0.0137   1.0000
  13.750   1.1776   0.04017   0.03485   0.0303   0.0126   1.0000
  14.000   1.1736   0.04355   0.03834   0.0293   0.0120   1.0000
  14.250   1.1700   0.04690   0.04178   0.0283   0.0113   1.0000
  14.500   1.1619   0.05086   0.04583   0.0271   0.0107   1.0000
  14.750   1.1518   0.05508   0.05012   0.0257   0.0101   1.0000
  15.000   1.1356   0.06015   0.05529   0.0240   0.0097   1.0000
  15.250   1.1249   0.06465   0.05989   0.0224   0.0093   1.0000
  15.500   1.1188   0.06872   0.06407   0.0209   0.0090   1.0000
  15.750   1.1111   0.07311   0.06855   0.0193   0.0086   1.0000
  16.000   1.1036   0.07759   0.07313   0.0175   0.0083   1.0000
  16.250   1.0993   0.08167   0.07729   0.0159   0.0080   1.0000
  16.500   1.0876   0.08695   0.08265   0.0137   0.0077   1.0000
  16.750   1.0768   0.09224   0.08802   0.0115   0.0073   1.0000
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