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MH 27 11.99% (mh27-il)

MH 27 11.99% - Martin Hepperle MH 27 for F3D Pylon Racing (extended laminar flow)


Airfoil mh27-il
Details Dat file Parser  
(mh27-il) MH 27 11.99%
Martin Hepperle MH 27 for F3D Pylon Racing (extended laminar flow)
Max thickness 12% at 42.4% chord.
Max camber 1.4% at 42.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 27  11.99% 
  1.00000000  0.00000000
  0.99571520  0.00058599
  0.98395553  0.00317054
  0.96643186  0.00805747
  0.94421230  0.01463593
  0.91796571  0.02233068
  0.88818558  0.03054279
  0.85529895  0.03863330
  0.81933175  0.04589121
  0.78006805  0.05217030
  0.73770911  0.05769095
  0.69276997  0.06251127
  0.64571814  0.06657998
  0.59707351  0.06990379
  0.54738051  0.07242470
  0.49717719  0.07411522
  0.44700220  0.07492857
  0.39739254  0.07485367
  0.34887198  0.07385693
  0.30194424  0.07194567
  0.25709348  0.06911284
  0.21477403  0.06538736
  0.17540438  0.06078322
  0.13935004  0.05535946
  0.10694272  0.04918021
  0.07845951  0.04235095
  0.05413964  0.03498850
  0.03415342  0.02726114
  0.01864760  0.01938149
  0.00770890  0.01164516
  0.00190285  0.00517434
  0.00082903  0.00316506
  0.00018081  0.00130439
  0.00000364  0.00017361
  0.00009279 -0.00082226
  0.00052969 -0.00175607
  0.00129790 -0.00272626
  0.00293235 -0.00423585
  0.00508815 -0.00580795
  0.00593836 -0.00635887
  0.01719356 -0.01171349
  0.03366873 -0.01695866
  0.05517405 -0.02187453
  0.08153586 -0.02635800
  0.11251971 -0.03038274
  0.14780184 -0.03396403
  0.18695226 -0.03710479
  0.22951674 -0.03976194
  0.27500196 -0.04190602
  0.32292277 -0.04347012
  0.37279279 -0.04446501
  0.42406984 -0.04491264
  0.47616234 -0.04485172
  0.52847177 -0.04427557
  0.58039711 -0.04320850
  0.63134080 -0.04163737
  0.68071608 -0.03957671
  0.72796029 -0.03699090
  0.77254303 -0.03388729
  0.81392820 -0.03013320
  0.85195686 -0.02554222
  0.88662912 -0.02043718
  0.91746745 -0.01523863
  0.94417642 -0.01001220
  0.96669689 -0.00530630
  0.98437310 -0.00194796
  0.99593329 -0.00033203
  1.00000000  0.00000000
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Polars for MH 27 11.99% (mh27-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh27-il50,000933.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh27-il50,000530.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh27-il100,000949.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh27-il100,000546.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh27-il200,000969.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh27-il200,000554.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh27-il500,000973.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh27-il500,000554.7 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh27-il1,000,000973.1 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh27-il1,000,000561.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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