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MH 115 11.06% (mh115-il)

MH 115 11.06% - Martin Hepperle MH 115 for a propeller for ultralight


Airfoil mh115-il
Details Dat file Parser  
(mh115-il) MH 115 11.06%
Martin Hepperle MH 115 for a propeller for ultralight
Max thickness 11.1% at 29.8% chord.
Max camber 5.5% at 46% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 115  11.06% 
  1.00000000  0.00000000
  0.99674566  0.00104546
  0.98749507  0.00420491
  0.97313696  0.00917838
  0.95406083  0.01529495
  0.93027275  0.02221117
  0.90199575  0.02990813
  0.86969551  0.03827613
  0.83385141  0.04708744
  0.79491906  0.05607895
  0.75332317  0.06501166
  0.70953970  0.07369232
  0.66408448  0.08188293
  0.61744199  0.08932477
  0.57006351  0.09577091
  0.52236480  0.10100258
  0.47472315  0.10485199
  0.42750717  0.10721862
  0.38107486  0.10805718
  0.33581107  0.10739733
  0.29213489  0.10526383
  0.25043484  0.10168814
  0.21107556  0.09672020
  0.17438403  0.09043777
  0.14065894  0.08294253
  0.11015046  0.07436606
  0.08306868  0.06488165
  0.05959692  0.05472346
  0.03994100  0.04413071
  0.02421451  0.03330030
  0.01239244  0.02252916
  0.00442595  0.01233725
  0.00069857  0.00437441
  0.00016371  0.00197385
  0.00000179 -0.00019390
  0.00011571 -0.00148174
  0.00045986 -0.00258950
  0.00112633 -0.00357520
  0.00211854 -0.00453745
  0.00408531 -0.00594230
  0.00657061 -0.00729619
  0.00768550 -0.00781423
  0.02015328 -0.01156879
  0.03800525 -0.01423278
  0.06110941 -0.01574891
  0.08933311 -0.01613566
  0.12247340 -0.01547900
  0.16025579 -0.01389519
  0.20233415 -0.01153157
  0.24829570 -0.00855767
  0.29764598 -0.00517063
  0.34981349 -0.00155002
  0.40418640  0.00213342
  0.46011715  0.00571533
  0.51692182  0.00902612
  0.57388416  0.01191204
  0.63026148  0.01422380
  0.68528991  0.01584103
  0.73819142  0.01666217
  0.78818207  0.01663427
  0.83448365  0.01574448
  0.87633804  0.01405771
  0.91305213  0.01170364
  0.94399942  0.00884122
  0.96852822  0.00569981
  0.98609072  0.00278939
  0.99654075  0.00073435
  1.00000000  0.00000000
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Polars for MH 115 11.06% (mh115-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh115-il50,000928.6 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh115-il50,000537.5 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh115-il100,000961.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh115-il100,000564.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh115-il200,000991.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh115-il200,000590 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh115-il500,0009130.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh115-il500,0005120.4 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh115-il1,000,0009158.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   mh115-il1,000,0005140.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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