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MH 23 8% (mh23-il)

MH 23 8% - Martin Hepperle MH 23 for F3D Pylon Racing (extended laminar flow)


Airfoil mh23-il
Details Dat file Parser  
(mh23-il) MH 23 8%
Martin Hepperle MH 23 for F3D Pylon Racing (extended laminar flow)
Max thickness 8% at 37.5% chord.
Max camber 1.2% at 42.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 23  8% 
  1.00000000  0.00000000
  0.99654891  0.00021002
  0.98638164  0.00106437
  0.96998124  0.00296595
  0.94800139  0.00610570
  0.92118921  0.01045067
  0.89031194  0.01575297
  0.85609439  0.02147937
  0.81881667  0.02686673
  0.77833061  0.03162776
  0.73482769  0.03593914
  0.68882550  0.03985290
  0.64081070  0.04331623
  0.59131663  0.04632354
  0.54090044  0.04880706
  0.49010217  0.05072471
  0.43946837  0.05202613
  0.38954323  0.05268363
  0.34085802  0.05265035
  0.29391873  0.05190854
  0.24921148  0.05043165
  0.20718720  0.04821694
  0.16825913  0.04525334
  0.13278111  0.04156398
  0.10107217  0.03718625
  0.07339004  0.03218696
  0.04995254  0.02665608
  0.03090007  0.02072236
  0.01634588  0.01457859
  0.00633460  0.00848345
  0.00187296  0.00419942
  0.00083390  0.00259110
  0.00019669  0.00110607
  0.00000845  0.00021283
  0.00006741 -0.00055535
  0.00045537 -0.00125931
  0.00116150 -0.00198573
  0.00268384 -0.00310871
  0.00470453 -0.00428571
  0.00674568 -0.00531418
  0.01818877 -0.00930151
  0.03475010 -0.01303636
  0.05627852 -0.01634982
  0.08264936 -0.01916279
  0.11366235 -0.02149126
  0.14901824 -0.02339855
  0.18829159 -0.02493191
  0.23103070 -0.02608303
  0.27674146 -0.02685342
  0.32493807 -0.02720281
  0.37513360 -0.02716554
  0.42678480 -0.02678840
  0.47929590 -0.02613063
  0.53206388 -0.02520550
  0.58448190 -0.02405271
  0.63594771 -0.02267570
  0.68586872 -0.02110271
  0.73368042 -0.01931914
  0.77884998 -0.01735713
  0.82085481 -0.01517772
  0.85934130 -0.01277321
  0.89392583 -0.01030911
  0.92410094 -0.00780159
  0.94970175 -0.00516897
  0.97065426 -0.00275126
  0.98651517 -0.00101933
  0.99654701 -0.00019154
  1.00000000  0.00000000
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Polars for MH 23 8% (mh23-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh23-il50,000934.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh23-il50,000533.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh23-il100,000950 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh23-il100,000545.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh23-il200,000966.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh23-il200,000557.4 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh23-il500,000983.8 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh23-il500,000566.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   mh23-il1,000,000983.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh23-il1,000,000572.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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