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MH 60 10.08% (mh60-il)

MH 60 10.08% - Martin Hepperle MH 60 for flying wings


Airfoil mh60-il
Details Dat file Parser  
(mh60-il) MH 60 10.08%
Martin Hepperle MH 60 for flying wings
Max thickness 10.1% at 26.9% chord.
Max camber 1.7% at 36.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 60  10.08% 
  1.00000000  0.00000000
  0.99666580 -0.00010721
  0.98657699 -0.00021857
  0.96985338  0.00016906
  0.94694030  0.00139128
  0.91831569  0.00361553
  0.88456977  0.00701751
  0.84646618  0.01162313
  0.80476307  0.01726953
  0.76017397  0.02372635
  0.71339610  0.03070281
  0.66509436  0.03783692
  0.61580456  0.04470067
  0.56592867  0.05096619
  0.51585200  0.05640144
  0.46593824  0.06087194
  0.41660837  0.06433255
  0.36833791  0.06674160
  0.32159784  0.06804728
  0.27685111  0.06819799
  0.23450489  0.06712378
  0.19489756  0.06480794
  0.15834304  0.06127542
  0.12511624  0.05659207
  0.09547170  0.05085765
  0.06963185  0.04419104
  0.04775994  0.03671156
  0.02991067  0.02861875
  0.01614537  0.02022454
  0.00650380  0.01192520
  0.00155861  0.00520084
  0.00063331  0.00307449
  0.00010922  0.00111324
  0.00000058 -0.00007665
  0.00014333 -0.00112647
  0.00061755 -0.00210560
  0.00141059 -0.00311039
  0.00306610 -0.00465456
  0.00522627 -0.00623727
  0.00629135 -0.00692140
  0.01755374 -0.01218235
  0.03382614 -0.01721270
  0.05485182 -0.02179248
  0.08041207 -0.02573528
  0.11030623 -0.02887570
  0.14435698 -0.03112840
  0.18232147 -0.03248771
  0.22391347 -0.03299586
  0.26875457 -0.03275882
  0.31638866 -0.03186979
  0.36631877 -0.03043106
  0.41801505 -0.02855000
  0.47089651 -0.02636136
  0.52434002 -0.02397326
  0.57770187 -0.02149393
  0.63032585 -0.01899669
  0.68156522 -0.01655011
  0.73078910 -0.01419344
  0.77739590 -0.01196792
  0.82081805 -0.00989681
  0.86051691 -0.00801475
  0.89599003 -0.00632325
  0.92679048 -0.00482388
  0.95253024 -0.00349330
  0.97288501 -0.00230894
  0.98765801 -0.00120259
  0.99681811 -0.00032621
  1.00000000  0.00000000
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Polars for MH 60 10.08% (mh60-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh60-il50,000927.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il50,000532.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il100,000945 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il100,000546.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il200,000961.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il200,000560 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il500,000982.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il500,000577.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il1,000,000998.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il1,000,000591 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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