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MH 44 9.66% (mh44-il)

MH 44 9.66% - Martin Hepperle MH 44 for flying wings


Airfoil mh44-il
Details Dat file Parser  
(mh44-il) MH 44 9.66%
Martin Hepperle MH 44 for flying wings
Max thickness 9.6% at 27.1% chord.
Max camber 1.5% at 36.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 44  9.66% 
  1.00000000  0.00000000
  0.99653011  0.00006570
  0.98631190  0.00045598
  0.96974340  0.00149517
  0.94725184  0.00334612
  0.91930910  0.00609337
  0.88644951  0.00977957
  0.84928493  0.01440044
  0.80853520  0.01988463
  0.76501741  0.02593772
  0.71928426  0.03201301
  0.67158211  0.03781515
  0.62232193  0.04331441
  0.57208418  0.04841899
  0.52140861  0.05295553
  0.47079118  0.05680855
  0.42076549  0.05988591
  0.37185888  0.06206495
  0.32453101  0.06322567
  0.27921124  0.06329856
  0.23629096  0.06222447
  0.19611034  0.06000566
  0.15900561  0.05668847
  0.12529908  0.05233411
  0.09526462  0.04699913
  0.06910337  0.04078625
  0.04698628  0.03384119
  0.02902831  0.02635644
  0.01532232  0.01857810
  0.00589505  0.01084457
  0.00142333  0.00486961
  0.00055408  0.00283988
  0.00008249  0.00095342
  0.00000391 -0.00019591
  0.00016998 -0.00121038
  0.00066308 -0.00215426
  0.00147537 -0.00312101
  0.00316245 -0.00460778
  0.00535666 -0.00613866
  0.00687346 -0.00706058
  0.01851334 -0.01222489
  0.03515031 -0.01724079
  0.05648923 -0.02189643
  0.08226781 -0.02596502
  0.11229580 -0.02921248
  0.14645533 -0.03153390
  0.18453207 -0.03294836
  0.22624958 -0.03352073
  0.27121906 -0.03338609
  0.31895653 -0.03264354
  0.36894467 -0.03138667
  0.42064059 -0.02970406
  0.47346260 -0.02770997
  0.52679860 -0.02549695
  0.58001348 -0.02317072
  0.63245725 -0.02079951
  0.68348629 -0.01845282
  0.73247007 -0.01616283
  0.77880961 -0.01396515
  0.82194185 -0.01186964
  0.86134328 -0.00990001
  0.89653379 -0.00805521
  0.92708001 -0.00634860
  0.95259909 -0.00476002
  0.97276882 -0.00326398
  0.98743380 -0.00175502
  0.99669367 -0.00048443
  1.00000000  0.00000000
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Polars for MH 44 9.66% (mh44-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh44-il50,000929.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh44-il50,000532.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh44-il100,000944.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh44-il100,000545.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh44-il200,000960.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh44-il200,000558.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh44-il500,000980.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh44-il500,000574.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh44-il1,000,000994.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh44-il1,000,000587.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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