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MH 46 9.1% (mh46-il)

MH 46 9.1% - Martin Hepperle MH 46 for flying wings


Airfoil mh46-il
Details Dat file Parser  
(mh46-il) MH 46 9.1%
Martin Hepperle MH 46 for flying wings
Max thickness 9.1% at 27.1% chord.
Max camber 1.4% at 36.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 46  9.1% 
  1.00000000  0.00000000
  0.99660628  0.00007530
  0.98659970  0.00046905
  0.97034659  0.00146183
  0.94824670  0.00319141
  0.92074548  0.00572233
  0.88834784  0.00907650
  0.85162727  0.01321065
  0.81117042  0.01800095
  0.76756278  0.02330778
  0.72142066  0.02896462
  0.67338120  0.03475286
  0.62402278  0.04038516
  0.57385043  0.04561155
  0.52333083  0.05020801
  0.47288401  0.05404424
  0.42299544  0.05706033
  0.37418094  0.05916110
  0.32689683  0.06024308
  0.28157129  0.06024689
  0.23859447  0.05912200
  0.19830608  0.05687718
  0.16104048  0.05356562
  0.12711727  0.04925862
  0.09681401  0.04402979
  0.07034567  0.03799371
  0.04789723  0.03130523
  0.02960151  0.02416364
  0.01557729  0.01683540
  0.00592692  0.00965020
  0.00186536  0.00495302
  0.00081858  0.00306199
  0.00018419  0.00129408
  0.00000555  0.00021179
  0.00007847 -0.00074930
  0.00047557 -0.00165663
  0.00118006 -0.00259900
  0.00268698 -0.00405780
  0.00468035 -0.00556344
  0.00713805 -0.00711394
  0.01857097 -0.01215623
  0.03490541 -0.01690024
  0.05596763 -0.02111990
  0.08163023 -0.02466358
  0.11170798 -0.02745354
  0.14598771 -0.02944757
  0.18418975 -0.03065925
  0.22598714 -0.03112477
  0.27097846 -0.03092655
  0.31870122 -0.03013255
  0.36866042 -0.02882459
  0.42033648 -0.02709151
  0.47316448 -0.02505807
  0.52654273 -0.02283514
  0.57982934 -0.02055175
  0.63235205 -0.01828451
  0.68344904 -0.01609558
  0.73247600 -0.01400083
  0.77883825 -0.01201064
  0.82199199 -0.01012964
  0.86141749 -0.00839040
  0.89662628 -0.00679146
  0.92718206 -0.00533590
  0.95270417 -0.00399617
  0.97287443 -0.00274101
  0.98753161 -0.00147086
  0.99673858 -0.00040341
  1.00000000  0.00000000
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Polars for MH 46 9.1% (mh46-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh46-il50,000930.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh46-il50,000533.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh46-il100,000946 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh46-il100,000546.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh46-il200,000961.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh46-il200,000558.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh46-il500,000981.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh46-il500,000574.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh46-il1,000,000994.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh46-il1,000,000585.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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