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MH 61 10.26% (mh61-il)

MH 61 10.26% - Martin Hepperle MH 61 for flying wings


Airfoil mh61-il
Details Dat file Parser  
(mh61-il) MH 61 10.26%
Martin Hepperle MH 61 for flying wings
Max thickness 10.2% at 27.6% chord.
Max camber 1.4% at 37.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 61  10.26% 
  1.00000000  0.00000000
  0.99662552 -0.00021296
  0.98634442 -0.00058867
  0.96924455 -0.00047375
  0.94585731  0.00056315
  0.91673505  0.00269474
  0.88251392  0.00609338
  0.84398992  0.01077369
  0.80195531  0.01656917
  0.75715989  0.02322682
  0.71033087  0.03042633
  0.66215348  0.03775213
  0.61314451  0.04471331
  0.56364860  0.05095356
  0.51402085  0.05625665
  0.46462009  0.06047633
  0.41583230  0.06354070
  0.36806914  0.06540775
  0.32175184  0.06606308
  0.27730980  0.06549720
  0.23513530  0.06369756
  0.19557573  0.06068599
  0.15893920  0.05651303
  0.12547935  0.05129165
  0.09546190  0.04520923
  0.06917074  0.03845040
  0.04684813  0.03119300
  0.02868571  0.02363888
  0.01483234  0.01603750
  0.00540062  0.00871984
  0.00224694  0.00512990
  0.00104319  0.00323637
  0.00027501  0.00148232
  0.00002448  0.00041540
  0.00004474 -0.00052570
  0.00040935 -0.00141651
  0.00109497 -0.00235178
  0.00259141 -0.00381107
  0.00459453 -0.00532859
  0.00868086 -0.00781260
  0.02108735 -0.01314311
  0.03837857 -0.01833977
  0.06030248 -0.02318942
  0.08663912 -0.02748653
  0.11716742 -0.03106570
  0.15167904 -0.03381596
  0.18990853 -0.03569772
  0.23155319 -0.03669930
  0.27626006 -0.03685835
  0.32363710 -0.03624306
  0.37322832 -0.03497025
  0.42452356 -0.03316183
  0.47695565 -0.03096354
  0.52990961 -0.02849367
  0.58275075 -0.02586412
  0.63483287 -0.02315568
  0.68551931 -0.02044124
  0.73418958 -0.01776873
  0.78025217 -0.01518546
  0.82314952 -0.01272468
  0.86235287 -0.01042910
  0.89736920 -0.00831193
  0.92776030 -0.00638577
  0.95314575 -0.00464029
  0.97320761 -0.00306517
  0.98776461 -0.00159794
  0.99682854 -0.00043667
  1.00000000  0.00000000
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Polars for MH 61 10.26% (mh61-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh61-il50,000931.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il50,000533 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il100,000947.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il100,000547.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il200,000963.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il200,000560.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il500,000984.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il500,000576.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il1,000,000998 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il1,000,000586.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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