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MH 102 16.99% (mh102-il)

MH 102 16.99% - Martin Hepperle MH 102 for stall controlled wind turbines (root)


Airfoil mh102-il
Details Dat file Parser  
(mh102-il) MH 102 16.99%
Martin Hepperle MH 102 for stall controlled wind turbines (root)
Max thickness 17% at 27.7% chord.
Max camber 2.8% at 37.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 102  16.99% 
  1.00000000  0.00000000
  0.99614983  0.00063728
  0.98520565  0.00282240
  0.96830620  0.00663188
  0.94602565  0.01147142
  0.91839872  0.01707581
  0.88572075  0.02361176
  0.84861962  0.03110739
  0.80774299  0.03943785
  0.76375323  0.04841341
  0.71730911  0.05779135
  0.66905176  0.06728927
  0.61959790  0.07661096
  0.56953125  0.08544960
  0.51940362  0.09351302
  0.46973112  0.10052213
  0.42099874  0.10622572
  0.37366109  0.11040973
  0.32820037  0.11284147
  0.28491185  0.11316925
  0.24380784  0.11130183
  0.20506012  0.10746400
  0.16901281  0.10181653
  0.13594111  0.09447235
  0.10608263  0.08559329
  0.07964163  0.07536521
  0.05678511  0.06401791
  0.03764823  0.05182014
  0.02233251  0.03908978
  0.01090201  0.02621339
  0.00343089  0.01372124
  0.00081810  0.00624945
  0.00020021  0.00293804
  0.00000082 -0.00018316
  0.00011982 -0.00213265
  0.00049708 -0.00393552
  0.00120839 -0.00566457
  0.00224072 -0.00741951
  0.00426419 -0.01009532
  0.00680138 -0.01281177
  0.01050141 -0.01613427
  0.02399365 -0.02525514
  0.04201295 -0.03405036
  0.06417737 -0.04212709
  0.09020108 -0.04904123
  0.11995663 -0.05434164
  0.15349856 -0.05770634
  0.19094712 -0.05910127
  0.23224820 -0.05877018
  0.27709212 -0.05700227
  0.32507665 -0.05405209
  0.37570590 -0.05021288
  0.42839057 -0.04576400
  0.48243404 -0.04098262
  0.53707390 -0.03601968
  0.59162389 -0.03098315
  0.64540959 -0.02601644
  0.69772762 -0.02126360
  0.74788348 -0.01683072
  0.79520092 -0.01281888
  0.83902670 -0.00929883
  0.87873741 -0.00633322
  0.91374386 -0.00395207
  0.94349459 -0.00217278
  0.96747412 -0.00097467
  0.98520055 -0.00030404
  0.99622182 -0.00005550
  1.00000000  0.00000000
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Polars for MH 102 16.99% (mh102-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh102-il50,00095.5 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh102-il50,000523.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh102-il100,000937.8 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh102-il100,000545.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh102-il200,000963.5 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   mh102-il200,000565.2 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh102-il500,000994.2 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   mh102-il500,000591 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   mh102-il1,000,0009118.7 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh102-il1,000,0005110.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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