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MH 116 9.84% (mh116-il)

MH 116 9.84% - Martin Hepperle MH 116 for a propeller for ultralight


Airfoil mh116-il
Details Dat file Parser  
(mh116-il) MH 116 9.84%
Martin Hepperle MH 116 for a propeller for ultralight
Max thickness 9.9% at 32.4% chord.
Max camber 4.1% at 46.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 116  9.84% 
  1.00000000  0.00000000
  0.99670146  0.00074814
  0.98721743  0.00307583
  0.97230854  0.00688054
  0.95240976  0.01171791
  0.92766355  0.01732983
  0.89836484  0.02369937
  0.86500106  0.03073152
  0.82808656  0.03824262
  0.78813381  0.04599730
  0.74564655  0.05374885
  0.70111701  0.06123259
  0.65502194  0.06819657
  0.60781241  0.07438806
  0.55991093  0.07960072
  0.51172865  0.08365638
  0.46365997  0.08642268
  0.41606636  0.08779284
  0.36926585  0.08776891
  0.32364632  0.08644796
  0.27966531  0.08391535
  0.23775427  0.08021674
  0.19830559  0.07542539
  0.16168504  0.06962024
  0.12821458  0.06291334
  0.09819465  0.05543568
  0.07189000  0.04733540
  0.04951823  0.03875778
  0.03121401  0.02989438
  0.01707861  0.02098180
  0.00710579  0.01236090
  0.00164447  0.00513736
  0.00068511  0.00304275
  0.00012824  0.00114121
  0.00000000  0.00000460
  0.00012587 -0.00098049
  0.00058603 -0.00188406
  0.00136572 -0.00280442
  0.00299737 -0.00420676
  0.00512857 -0.00563013
  0.01652794 -0.01043038
  0.03235571 -0.01419815
  0.05316147 -0.01700865
  0.07888662 -0.01880306
  0.10939639 -0.01958813
  0.14449266 -0.01943482
  0.18388770 -0.01845562
  0.22722412 -0.01678535
  0.27406730 -0.01459252
  0.32390001 -0.01205138
  0.37612573 -0.00932796
  0.43011154 -0.00654727
  0.48519647 -0.00383863
  0.54069749 -0.00129973
  0.59591933  0.00096771
  0.65016027  0.00289580
  0.70272230  0.00441674
  0.75292169  0.00550059
  0.80009726  0.00611414
  0.84361040  0.00625919
  0.88285307  0.00594510
  0.91725959  0.00522485
  0.94630943  0.00415177
  0.96949175  0.00283087
  0.98634699  0.00147768
  0.99657154  0.00041241
  1.00000000  0.00000000
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Polars for MH 116 9.84% (mh116-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh116-il50,000939 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh116-il50,000539.4 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh116-il100,000963 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   mh116-il100,000563 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh116-il200,000989.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh116-il200,000586.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh116-il500,0009125.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh116-il500,0005113.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh116-il1,000,0009150.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   mh116-il1,000,0005131 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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