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MH 78 14.47% (mh78-il)

MH 78 14.47% - Martin Hepperle MH 78 for flying wings (hang glider)


Airfoil mh78-il
Details Dat file Parser  
(mh78-il) MH 78 14.47%
Martin Hepperle MH 78 for flying wings (hang glider)
Max thickness 14.4% at 22.1% chord.
Max camber 1.9% at 17.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 78  14.47% 
  1.00000000  0.00000000
  0.99647376 -0.00005769
  0.98594343 -0.00006167
  0.96857920  0.00031010
  0.94469065  0.00133916
  0.91471313  0.00325525
  0.87919370  0.00623043
  0.83877336  0.01036549
  0.79416760  0.01568975
  0.74614368  0.02215224
  0.69549919  0.02963028
  0.64303838  0.03792739
  0.58955279  0.04679051
  0.53580093  0.05591397
  0.48249441  0.06496290
  0.43028441  0.07358030
  0.37975519  0.08141319
  0.33141918  0.08811752
  0.28571789  0.09338432
  0.24302652  0.09693173
  0.20366177  0.09853301
  0.16790530  0.09791980
  0.13576599  0.09481689
  0.10710138  0.08926263
  0.08186069  0.08142652
  0.05989520  0.07157890
  0.04115205  0.06026510
  0.02583034  0.04799225
  0.01408202  0.03509813
  0.00588632  0.02196825
  0.00117701  0.00922609
  0.00004071 -0.00160454
  0.00037773 -0.00474011
  0.00106694 -0.00762752
  0.00173681 -0.00938226
  0.00262341 -0.01093910
  0.00383435 -0.01234483
  0.00539475 -0.01370379
  0.00826371 -0.01569514
  0.01170942 -0.01764406
  0.02810394 -0.02422507
  0.04904288 -0.02987339
  0.07490483 -0.03490330
  0.10530986 -0.03917904
  0.13998895 -0.04253225
  0.17874711 -0.04496957
  0.22121381 -0.04664469
  0.26687101 -0.04764926
  0.31517512 -0.04803149
  0.36555838 -0.04783093
  0.41743222 -0.04708522
  0.47019348 -0.04582658
  0.52322981 -0.04409010
  0.57592623 -0.04190422
  0.62767130 -0.03929951
  0.67786291 -0.03629286
  0.72591398 -0.03289037
  0.77128261 -0.02902518
  0.81362617 -0.02461843
  0.85274328 -0.01980018
  0.88835211 -0.01488937
  0.92005707 -0.01025828
  0.94735107 -0.00627581
  0.96962738 -0.00322749
  0.98622391 -0.00124894
  0.99650893 -0.00026574
  1.00000000  0.00000000
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Polars for MH 78 14.47% (mh78-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh78-il50,00099.9 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   mh78-il50,000518.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   mh78-il100,000922.4 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh78-il100,000533.6 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh78-il200,000942.3 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   mh78-il200,000551.3 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh78-il500,000973.6 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   mh78-il500,000577.3 at α=10.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh78-il1,000,000999.2 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh78-il1,000,000597.2 at α=11.25°Mach=0 Ncrit=5Xfoil predictionDetails
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