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MH 64 8.59% (mh64-il)

MH 64 8.59% - Martin Hepperle MH 64 for flying wings


Airfoil mh64-il
Details Dat file Parser  
(mh64-il) MH 64 8.59%
Martin Hepperle MH 64 for flying wings
Max thickness 8.6% at 26.9% chord.
Max camber 1.4% at 41.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 64  8.59% 
  1.00000000  0.00000000
  0.99677882 -0.00001741
  0.98710222  0.00007686
  0.97112117  0.00061269
  0.94919338  0.00180715
  0.92172048  0.00378243
  0.88920839  0.00666283
  0.85230568  0.01046738
  0.81167214  0.01507212
  0.76794901  0.02030702
  0.72177737  0.02595115
  0.67378586  0.03173522
  0.62451989  0.03733285
  0.57443366  0.04248661
  0.52396327  0.04699723
  0.47352260  0.05074736
  0.42356875  0.05368619
  0.37459982  0.05577096
  0.32710703  0.05694621
  0.28156946  0.05716210
  0.23841873  0.05635245
  0.19802650  0.05449350
  0.16073193  0.05158876
  0.12682611  0.04768368
  0.09657874  0.04285847
  0.07022520  0.03720997
  0.04794175  0.03084017
  0.02980596  0.02392029
  0.01588864  0.01672252
  0.00622672  0.00960304
  0.00199243  0.00486572
  0.00090014  0.00302044
  0.00022004  0.00132032
  0.00001234  0.00029269
  0.00006096 -0.00060685
  0.00044110 -0.00144891
  0.00113432 -0.00232546
  0.00262979 -0.00368490
  0.00461687 -0.00509428
  0.00694442 -0.00648334
  0.01833919 -0.01125146
  0.03466796 -0.01579724
  0.05569927 -0.01992063
  0.08123487 -0.02343413
  0.11108087 -0.02618117
  0.14506914 -0.02807622
  0.18296176 -0.02912012
  0.22447823 -0.02935635
  0.26924359 -0.02889666
  0.31680488 -0.02783543
  0.36666707 -0.02627939
  0.41830185 -0.02433568
  0.47112929 -0.02214198
  0.52452660 -0.01980453
  0.57785027 -0.01743256
  0.63044378 -0.01509558
  0.68166011 -0.01286103
  0.73086778 -0.01076257
  0.77746469 -0.00883812
  0.82088254 -0.00710380
  0.86058195 -0.00558859
  0.89605977 -0.00428517
  0.92686848 -0.00318669
  0.95261991 -0.00225972
  0.97298999 -0.00147270
  0.98776650 -0.00075632
  0.99686985 -0.00020132
  1.00000000  0.00000000
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Polars for MH 64 8.59% (mh64-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh64-il50,000929.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh64-il50,000533.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh64-il100,000944.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh64-il100,000545.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh64-il200,000959.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh64-il200,000557 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh64-il500,000978 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh64-il500,000572.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh64-il1,000,000990.8 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh64-il1,000,000584 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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