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MH 32 8.7% (mh32-il)

MH 32 8.7% - Martin Hepperle MH 32 for F3E and F3B


Airfoil mh32-il
Details Dat file Parser  
(mh32-il) MH 32 8.7%
Martin Hepperle MH 32 for F3E and F3B
Max thickness 8.7% at 30.2% chord.
Max camber 2.3% at 45.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 32  8.7% 
  1.00000000  0.00000000
  0.99671850  0.00034782
  0.98706463  0.00149967
  0.97145561  0.00363339
  0.95035123  0.00677805
  0.92424036  0.01086920
  0.89362390  0.01576960
  0.85900629  0.02129402
  0.82089086  0.02721967
  0.77977368  0.03329120
  0.73609426  0.03922652
  0.69023068  0.04481867
  0.64259066  0.04994067
  0.59361615  0.05451907
  0.54382705  0.05852295
  0.49381832  0.06186106
  0.44411124  0.06436644
  0.39514537  0.06595791
  0.34741929  0.06660529
  0.30140493  0.06621755
  0.25746856  0.06476927
  0.21602684  0.06232083
  0.17749047  0.05886363
  0.14216302  0.05442091
  0.11032399  0.04907369
  0.08221963  0.04292806
  0.05805331  0.03610737
  0.03796269  0.02878423
  0.02205704  0.02117736
  0.01037736  0.01359215
  0.00300681  0.00646658
  0.00184914  0.00480308
  0.00081352  0.00292741
  0.00018114  0.00121388
  0.00000483  0.00018464
  0.00008218 -0.00070798
  0.00048790 -0.00153007
  0.00120550 -0.00237236
  0.00273690 -0.00365371
  0.00476529 -0.00494109
  0.01192981 -0.00809184
  0.02604240 -0.01198316
  0.04520500 -0.01533200
  0.06925966 -0.01804904
  0.09801849 -0.02007916
  0.13124461 -0.02142047
  0.16864181 -0.02209646
  0.20985766 -0.02215984
  0.25447576 -0.02168325
  0.30202197 -0.02074377
  0.35197672 -0.01942228
  0.40378144 -0.01779533
  0.45685259 -0.01593904
  0.51058787 -0.01392702
  0.56437178 -0.01183665
  0.61758180 -0.00974179
  0.66959046 -0.00772005
  0.71977196 -0.00583616
  0.76751419 -0.00415018
  0.81222445 -0.00271210
  0.85332486 -0.00156808
  0.89026144 -0.00073182
  0.92252540 -0.00019501
  0.94965851  0.00007939
  0.97125915  0.00015184
  0.98701228  0.00012533
  0.99669738  0.00004969
  1.00000000  0.00000000
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Polars for MH 32 8.7% (mh32-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh32-il50,000935.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh32-il50,000537.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh32-il100,000953.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh32-il100,000553.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh32-il200,000972.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh32-il200,000567.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh32-il500,000994.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   mh32-il500,000584 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh32-il1,000,0009109.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh32-il1,000,000596.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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