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MH 20 9.01% (mh20-il)

MH 20 9.01% - Martin Hepperle MH 20 for F3D Pylon Racing


Airfoil mh20-il
Details Dat file Parser  
(mh20-il) MH 20 9.01%
Martin Hepperle MH 20 for F3D Pylon Racing
Max thickness 9% at 32.2% chord.
Max camber 1.9% at 37.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 20  9.01% 
  1.00000000  0.00000000
  0.99663722 -0.00000502
  0.98661979  0.00015827
  0.97016021  0.00083998
  0.94762865  0.00232279
  0.91954306  0.00478393
  0.88649448  0.00827457
  0.84911235  0.01276792
  0.80805809  0.01815911
  0.76400822  0.02428373
  0.71763596  0.03091656
  0.66960153  0.03779462
  0.62054465  0.04463611
  0.57116423  0.05108921
  0.52197689  0.05654881
  0.47303495  0.06058278
  0.42440107  0.06327690
  0.37650891  0.06484632
  0.32990396  0.06532833
  0.28507654  0.06470811
  0.24245961  0.06294654
  0.20241194  0.06004635
  0.16525807  0.05604350
  0.13126736  0.05103062
  0.10070840  0.04515568
  0.07383715  0.03858238
  0.05087461  0.03148085
  0.03197380  0.02406597
  0.01728446  0.01663089
  0.00695149  0.00951360
  0.00230137  0.00483181
  0.00108635  0.00304916
  0.00030031  0.00141854
  0.00003307  0.00043894
  0.00003397 -0.00041277
  0.00037497 -0.00121038
  0.00103088 -0.00204638
  0.00246899 -0.00334802
  0.00439569 -0.00470397
  0.00659525 -0.00600849
  0.01770495 -0.01053427
  0.03378029 -0.01462203
  0.05477004 -0.01806289
  0.08059598 -0.02079484
  0.11108204 -0.02281900
  0.14599903 -0.02417183
  0.18503357 -0.02493978
  0.22778877 -0.02522602
  0.27377743 -0.02513931
  0.32245228 -0.02476081
  0.37320774 -0.02415208
  0.42543910 -0.02331965
  0.47854562 -0.02229529
  0.53191756 -0.02109606
  0.58494209 -0.01975863
  0.63701018 -0.01829908
  0.68752329 -0.01675217
  0.73589960 -0.01513154
  0.78158078 -0.01346836
  0.82403743 -0.01177234
  0.86277561 -0.01006936
  0.89734096 -0.00836027
  0.92732470 -0.00666124
  0.95236187 -0.00491317
  0.97233203 -0.00304938
  0.98724618 -0.00134670
  0.99671459 -0.00030431
  1.00000000  0.00000000
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Polars for MH 20 9.01% (mh20-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh20-il50,000933.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh20-il50,000534.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh20-il100,000950.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh20-il100,000550.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh20-il200,000968.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh20-il200,000564.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh20-il500,000991.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh20-il500,000581.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh20-il1,000,0009105.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh20-il1,000,000593.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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