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MH 106 13.07% (mh106-il)

MH 106 13.07% - Martin Hepperle MH 106 for stall controlled wind turbines


Airfoil mh106-il
Details Dat file Parser  
(mh106-il) MH 106 13.07%
Martin Hepperle MH 106 for stall controlled wind turbines
Max thickness 13.1% at 27.4% chord.
Max camber 0.9% at 27.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 106  13.07% 
  1.00000000  0.00000000
  0.99633896  0.00013538
  0.98572712  0.00081905
  0.96892525  0.00231554
  0.94642367  0.00436480
  0.91836006  0.00685652
  0.88503080  0.00997739
  0.84699594  0.01384794
  0.80487420  0.01847791
  0.75933341  0.02382341
  0.71107117  0.02978175
  0.66080012  0.03620038
  0.60923092  0.04288363
  0.55705830  0.04960002
  0.50494863  0.05609305
  0.45352913  0.06209195
  0.40338113  0.06731599
  0.35503575  0.07151328
  0.30907144  0.07437120
  0.26580358  0.07534795
  0.22506456  0.07420479
  0.18681819  0.07124411
  0.15136966  0.06678403
  0.11904212  0.06102631
  0.09013672  0.05417502
  0.06493704  0.04641532
  0.04366599  0.03792242
  0.02646761  0.02891578
  0.01345480  0.01968641
  0.00469764  0.01063397
  0.00188777  0.00623331
  0.00081003  0.00381469
  0.00016743  0.00154754
  0.00000165  0.00014605
  0.00010756 -0.00112503
  0.00055967 -0.00234500
  0.00133663 -0.00361403
  0.00297835 -0.00558815
  0.00513535 -0.00763363
  0.00962388 -0.01106732
  0.02257288 -0.01833048
  0.04024689 -0.02560254
  0.06232892 -0.03260747
  0.08853194 -0.03907257
  0.11858805 -0.04471630
  0.15229113 -0.04928617
  0.18946321 -0.05259526
  0.22996674 -0.05458014
  0.27356298 -0.05533977
  0.31988227 -0.05499133
  0.36851477 -0.05367172
  0.41896127 -0.05156813
  0.47063693 -0.04884164
  0.52291335 -0.04562226
  0.57515779 -0.04198170
  0.62679552 -0.03799545
  0.67724636 -0.03378661
  0.72590864 -0.02947190
  0.77219558 -0.02515173
  0.81554287 -0.02092181
  0.85541258 -0.01687058
  0.89129875 -0.01307891
  0.92273025 -0.00962032
  0.94927172 -0.00653679
  0.97060783 -0.00384979
  0.98649788 -0.00172690
  0.99652470 -0.00043016
  1.00000000  0.00000000
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Polars for MH 106 13.07% (mh106-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh106-il50,000914.9 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   mh106-il50,000527.3 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   mh106-il100,000942.1 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   mh106-il100,000544.6 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   mh106-il200,000961.4 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh106-il200,000560.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh106-il500,000986.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh106-il500,000579.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh106-il1,000,0009103.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh106-il1,000,000587.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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