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MH 113 14.62% (mh113-il)

MH 113 14.62% - Martin Hepperle MH 113 for a propeller for ultralight


Airfoil mh113-il
Details Dat file Parser  
(mh113-il) MH 113 14.62%
Martin Hepperle MH 113 for a propeller for ultralight
Max thickness 14.7% at 29.7% chord.
Max camber 6.4% at 47.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 113  14.62% 
  1.00000000  0.00000000
  0.99657911  0.00129859
  0.98693705  0.00520599
  0.97212357  0.01135726
  0.95257144  0.01898648
  0.92829218  0.02772077
  0.89956132  0.03753655
  0.86691136  0.04827937
  0.83087727  0.05966726
  0.79197587  0.07136829
  0.75069934  0.08303447
  0.70752493  0.09431152
  0.66290785  0.10483599
  0.61722787  0.11424445
  0.57079623  0.12228128
  0.52396079  0.12878840
  0.47709646  0.13364568
  0.43058995  0.13677292
  0.38483958  0.13811951
  0.34024152  0.13766085
  0.29718995  0.13539236
  0.25604833  0.13132100
  0.21714499  0.12549098
  0.18077094  0.11797452
  0.14716671  0.10890207
  0.11656500  0.09846885
  0.08919680  0.08689463
  0.06526129  0.07441188
  0.04491583  0.06128609
  0.02828712  0.04781828
  0.01547607  0.03434589
  0.00654829  0.02121442
  0.00144037  0.00885691
  0.00009164 -0.00197262
  0.00326044 -0.00986391
  0.01232056 -0.01515340
  0.02750123 -0.01912951
  0.04823829 -0.02180405
  0.07429146 -0.02316140
  0.10544287 -0.02324596
  0.14142733 -0.02214665
  0.18192638 -0.01998599
  0.22655720 -0.01692333
  0.27486968 -0.01313926
  0.32634580 -0.00883033
  0.38042147 -0.00418990
  0.43649054  0.00056375
  0.49390135  0.00520970
  0.55196243  0.00949915
  0.60991651  0.01318332
  0.66695052  0.01602203
  0.72218249  0.01781699
  0.77468331  0.01845890
  0.82354878  0.01794965
  0.86791482  0.01636346
  0.90699372  0.01386781
  0.94006831  0.01063360
  0.96634857  0.00693486
  0.98515215  0.00341917
  0.99631237  0.00090458
  1.00000000  0.00000000
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Polars for MH 113 14.62% (mh113-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh113-il50,00096 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh113-il50,000520.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh113-il100,000950.1 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh113-il100,000556 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh113-il200,000984.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh113-il200,000583.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh113-il500,0009124.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh113-il500,0005114.2 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh113-il1,000,0009153 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh113-il1,000,0005132.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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