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MH 110 10.01% (mh110-il)

MH 110 10.01% - Martin Hepperle MH 110 for stall controlled wind turbines (tip)


Airfoil mh110-il
Details Dat file Parser  
(mh110-il) MH 110 10.01%
Martin Hepperle MH 110 for stall controlled wind turbines (tip)
Max thickness 10% at 23.9% chord.
Max camber 1% at 15.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 110  10.01% 
  1.00000000  0.00000000
  0.99653679 -0.00000839
  0.98640394  0.00020868
  0.97015295  0.00088858
  0.94817712  0.00187970
  0.92061713  0.00312964
  0.88774439  0.00482284
  0.85005668  0.00710281
  0.80812280  0.01002942
  0.76257153  0.01361933
  0.71407609  0.01783903
  0.66333945  0.02260907
  0.61107819  0.02780629
  0.55800744  0.03326766
  0.50482605  0.03879780
  0.45220316  0.04417530
  0.40076651  0.04916328
  0.35109229  0.05351815
  0.30369808  0.05700000
  0.25903745  0.05938370
  0.21749907  0.06046023
  0.17940788  0.06005282
  0.14504302  0.05792865
  0.11434721  0.05380340
  0.08696462  0.04785904
  0.06286228  0.04069252
  0.04230701  0.03279183
  0.02555418  0.02451705
  0.01281496  0.01623683
  0.00429649  0.00837148
  0.00211665  0.00545033
  0.00096208  0.00340260
  0.00023711  0.00150577
  0.00001434  0.00034898
  0.00006123 -0.00067806
  0.00045103 -0.00165194
  0.00116088 -0.00266955
  0.00269267 -0.00425311
  0.00473182 -0.00589158
  0.01020191 -0.00928503
  0.02329198 -0.01496193
  0.04120440 -0.02035040
  0.06381301 -0.02526009
  0.09094732 -0.02958794
  0.12236865 -0.03326391
  0.15780899 -0.03623346
  0.19695727 -0.03849081
  0.23943286 -0.04006268
  0.28478797 -0.04097415
  0.33254591 -0.04124334
  0.38220182 -0.04089743
  0.43324080 -0.03996525
  0.48514078 -0.03851948
  0.53730757 -0.03665724
  0.58911977 -0.03440665
  0.64003009 -0.03178595
  0.68950142 -0.02887417
  0.73697819 -0.02575203
  0.78192326 -0.02249320
  0.82382388 -0.01917110
  0.86219604 -0.01586085
  0.89658864 -0.01263340
  0.92658689 -0.00956236
  0.95181035 -0.00668459
  0.97203228 -0.00402294
  0.98711684 -0.00181207
  0.99667613 -0.00043813
  1.00000000  0.00000000
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Polars for MH 110 10.01% (mh110-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh110-il50,000916.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh110-il50,000525.2 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh110-il100,000939 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   mh110-il100,000541 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh110-il200,000956.3 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh110-il200,000556 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh110-il500,000978.5 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   mh110-il500,000575.9 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh110-il1,000,000994.8 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   mh110-il1,000,000588.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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