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MH 84 13.69% (mh84-il)

MH 84 13.69% - Martin Hepperle MH 84 for flying wings (hang glider)


Airfoil mh84-il
Details Dat file Parser  
(mh84-il) MH 84 13.69%
Martin Hepperle MH 84 for flying wings (hang glider)
Max thickness 13.7% at 21.5% chord.
Max camber 4.1% at 36.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 84  13.69% 
  1.00000000  0.00000000
  0.99671739  0.00026180
  0.98688171  0.00116145
  0.97061373  0.00292480
  0.94821539  0.00576530
  0.92013789  0.00983488
  0.88694558  0.01519721
  0.84927783  0.02182185
  0.80781377  0.02958546
  0.76324413  0.03828919
  0.71624923  0.04767259
  0.66748558  0.05743803
  0.61757659  0.06726468
  0.56710933  0.07682984
  0.51663236  0.08581784
  0.46665653  0.09393510
  0.41765533  0.10091412
  0.37006588  0.10652253
  0.32428968  0.11056462
  0.28069238  0.11288504
  0.23960477  0.11337099
  0.20132236  0.11194796
  0.16610759  0.10858824
  0.13420133  0.10326333
  0.10570634  0.09595774
  0.08066828  0.08681124
  0.05913804  0.07595355
  0.04095749  0.06361290
  0.02601746  0.05031007
  0.01438281  0.03659414
  0.00613297  0.02298118
  0.00132065  0.01004156
  0.00003458 -0.00150357
  0.00044437 -0.00516696
  0.00115518 -0.00792945
  0.00183922 -0.00958715
  0.00273019 -0.01103519
  0.00393383 -0.01231574
  0.00547787 -0.01353022
  0.00830711 -0.01527031
  0.01169516 -0.01692624
  0.02553345 -0.02160010
  0.04525912 -0.02553700
  0.06987889 -0.02812601
  0.09930219 -0.02925508
  0.13338855 -0.02895226
  0.17194058 -0.02725099
  0.21486007 -0.02430234
  0.26186205 -0.02056410
  0.31231695 -0.01642710
  0.36554948 -0.01213063
  0.42085158 -0.00789148
  0.47748726 -0.00388021
  0.53470358 -0.00025134
  0.59173718  0.00287112
  0.64782480  0.00537552
  0.70221046  0.00715843
  0.75410083  0.00810213
  0.80263864  0.00817586
  0.84700161  0.00749288
  0.88649740  0.00627560
  0.92058677  0.00477865
  0.94887723  0.00325171
  0.97110442  0.00189852
  0.98710230  0.00086222
  0.99676409  0.00021850
  1.00000000  0.00000000
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Polars for MH 84 13.69% (mh84-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh84-il50,000915.2 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh84-il50,000530.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh84-il100,000940.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh84-il100,000548.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh84-il200,000962.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh84-il200,000566.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh84-il500,000992.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   mh84-il500,000592 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   mh84-il1,000,0009116.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh84-il1,000,0005113 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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