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MH 30 7.84% (mh30-il)

MH 30 7.84% - Martin Hepperle MH 30 for F3E and F3B


Airfoil mh30-il
Details Dat file Parser  
(mh30-il) MH 30 7.84%
Martin Hepperle MH 30 for F3E and F3B
Max thickness 7.8% at 31% chord.
Max camber 1.7% at 46.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 30  7.84% 
  1.00000000  0.00000000
  0.99675057  0.00027732
  0.98718030  0.00121266
  0.97167883  0.00297958
  0.95067833  0.00561358
  0.92464307  0.00906742
  0.89405358  0.01322248
  0.85940048  0.01792256
  0.82117835  0.02296852
  0.77988141  0.02813781
  0.73595235  0.03316971
  0.68977652  0.03788443
  0.64176843  0.04216636
  0.59237267  0.04596214
  0.54210592  0.04925302
  0.49155985  0.05198481
  0.44127336  0.05402597
  0.39172256  0.05532061
  0.34342570  0.05583807
  0.29687844  0.05551624
  0.25249921  0.05432584
  0.21073105  0.05230412
  0.17200012  0.04942599
  0.13663390  0.04569878
  0.10492830  0.04116581
  0.07712398  0.03590260
  0.05342228  0.03000727
  0.03394587  0.02362912
  0.01880186  0.01697955
  0.00802890  0.01034580
  0.00203588  0.00459383
  0.00093925  0.00287038
  0.00024253  0.00128859
  0.00001883  0.00033525
  0.00004754 -0.00049523
  0.00040083 -0.00127039
  0.00105881 -0.00207821
  0.00248751 -0.00333089
  0.00439501 -0.00462627
  0.01501806 -0.00913705
  0.03016645 -0.01305025
  0.05021239 -0.01646349
  0.07501814 -0.01926314
  0.10439815 -0.02138297
  0.13814663 -0.02281137
  0.17596671 -0.02359774
  0.21749488 -0.02379162
  0.26230291 -0.02346665
  0.30991182 -0.02268114
  0.35980209 -0.02150950
  0.41142345 -0.02000860
  0.46420152 -0.01825496
  0.51754510 -0.01630701
  0.57085128 -0.01424565
  0.62351129 -0.01213247
  0.67491319 -0.01005123
  0.72444741 -0.00805782
  0.77151953 -0.00622148
  0.81555453 -0.00458739
  0.85599372 -0.00321371
  0.89230202 -0.00211473
  0.92398973 -0.00129831
  0.95061656 -0.00073427
  0.97179803 -0.00038165
  0.98723981 -0.00014889
  0.99674839 -0.00002635
  1.00000000  0.00000000
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Polars for MH 30 7.84% (mh30-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh30-il50,000934.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh30-il50,000535.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh30-il100,000951.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh30-il100,000548.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh30-il200,000967.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   mh30-il200,000559.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   mh30-il500,000985.1 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh30-il500,000573.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh30-il1,000,000995.5 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh30-il1,000,000584.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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