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MH 70 11.08% (mh70-il)

MH 70 11.08% - Martin Hepperle MH 70 for fying wing (full size)


Airfoil mh70-il
Details Dat file Parser  
(mh70-il) MH 70 11.08%
Martin Hepperle MH 70 for fying wing (full size)
Max thickness 11.1% at 29.4% chord.
Max camber 3% at 39.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 70  11.08% 
  1.00000000  0.00000000
  0.99663874  0.00038973
  0.98681861  0.00160039
  0.97091284  0.00366465
  0.94918585  0.00661587
  0.92201087  0.01055332
  0.88990605  0.01555023
  0.85351341  0.02156423
  0.81348356  0.02843088
  0.77045027  0.03593166
  0.72505209  0.04381288
  0.67791513  0.05175439
  0.62958956  0.05939579
  0.58054074  0.06640360
  0.53117433  0.07249554
  0.48183152  0.07749388
  0.43291812  0.08134625
  0.38490056  0.08398008
  0.33821526  0.08532374
  0.29327034  0.08533399
  0.25046211  0.08401195
  0.21017875  0.08136709
  0.17277302  0.07742995
  0.13857039  0.07223969
  0.10783154  0.06584860
  0.08075868  0.05834736
  0.05748979  0.04986763
  0.03810212  0.04060855
  0.02264005  0.03085990
  0.01116110  0.02097603
  0.00368716  0.01137304
  0.00049015  0.00381228
  0.00007503  0.00139590
  0.00002872 -0.00081542
  0.00021629 -0.00214578
  0.00062912 -0.00330577
  0.00136089 -0.00434878
  0.00241995 -0.00537081
  0.00449418 -0.00687682
  0.00709496 -0.00835404
  0.00853955 -0.00906297
  0.02171085 -0.01371562
  0.04014361 -0.01784573
  0.06353610 -0.02131274
  0.09165680 -0.02399974
  0.12427053 -0.02584970
  0.16111728 -0.02684532
  0.20189931 -0.02703766
  0.24623689 -0.02652725
  0.29366811 -0.02542450
  0.34368819 -0.02383141
  0.39575196 -0.02187620
  0.44925704 -0.01969020
  0.50355203 -0.01739603
  0.55796000 -0.01508522
  0.61178825 -0.01282331
  0.66437716 -0.01063056
  0.71510432 -0.00854905
  0.76335935 -0.00661876
  0.80855024 -0.00488174
  0.85011975 -0.00336117
  0.88754749 -0.00209099
  0.92034639 -0.00109300
  0.94806277 -0.00039212
  0.97027225  0.00001004
  0.98657712  0.00013332
  0.99660243  0.00006156
  1.00000000  0.00000000
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Polars for MH 70 11.08% (mh70-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh70-il50,000927.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh70-il50,000535.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh70-il100,000950.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh70-il100,000552.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh70-il200,000970.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh70-il200,000567.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh70-il500,000995 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh70-il500,000587.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh70-il1,000,0009112.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh70-il1,000,0005103.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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