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MH 62 9.3% (mh62-il)

MH 62 9.3% - Martin Hepperle MH 62 for flying wings


Airfoil mh62-il
Details Dat file Parser  
(mh62-il) MH 62 9.3%
Martin Hepperle MH 62 for flying wings
Max thickness 9.3% at 26.9% chord.
Max camber 1.6% at 36.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 62  9.3% 
  1.00000000  0.00000000
  0.99672320 -0.00005436
  0.98685283 -0.00004227
  0.97053131  0.00044022
  0.94815429  0.00166033
  0.92015682  0.00376111
  0.88708273  0.00688970
  0.84963205  0.01106850
  0.80850880  0.01615624
  0.76438713  0.02195639
  0.71793385  0.02821659
  0.66979461  0.03462645
  0.62051197  0.04081389
  0.57051869  0.04648866
  0.52022803  0.05143382
  0.47002954  0.05552368
  0.42036402  0.05871060
  0.37172105  0.06095135
  0.32458149  0.06218839
  0.27941266  0.06237129
  0.23663376  0.06143558
  0.19660300  0.05936305
  0.15965048  0.05616726
  0.12606278  0.05190115
  0.09610193  0.04664817
  0.06999052  0.04051440
  0.04789620  0.03361471
  0.02988773  0.02613699
  0.01603412  0.01837117
  0.00637213  0.01069211
  0.00178293  0.00505036
  0.00077015  0.00307015
  0.00016380  0.00124513
  0.00000237  0.00014025
  0.00009452 -0.00083055
  0.00051805 -0.00173743
  0.00125746 -0.00267469
  0.00282697 -0.00412213
  0.00489391 -0.00561505
  0.00662611 -0.00668823
  0.01795493 -0.01168918
  0.03425341 -0.01646465
  0.05527811 -0.02080445
  0.08082177 -0.02452171
  0.11068708 -0.02745559
  0.14470193 -0.02952059
  0.18262595 -0.03071456
  0.22417611 -0.03108025
  0.26897575 -0.03072687
  0.31657049 -0.02974802
  0.36646434 -0.02824858
  0.41812828 -0.02633552
  0.47098183 -0.02414541
  0.52440200 -0.02178507
  0.57774515 -0.01936355
  0.63035485 -0.01695180
  0.68158415 -0.01461807
  0.73080181 -0.01239832
  0.77740590 -0.01033227
  0.82082839 -0.00843907
  0.86053021 -0.00675058
  0.89600848 -0.00526331
  0.92681587 -0.00397449
  0.95256426 -0.00285512
  0.97292940 -0.00187770
  0.98770717 -0.00097268
  0.99684228 -0.00026167
  1.00000000  0.00000000
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Polars for MH 62 9.3% (mh62-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh62-il50,000928.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh62-il50,000533.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh62-il100,000945 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh62-il100,000546 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh62-il200,000960.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh62-il200,000558.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh62-il500,000980.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh62-il500,000575 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh62-il1,000,000994.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh62-il1,000,000587.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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