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MH 80 12.72% (mh80-il)

MH 80 12.72% - Martin Hepperle MH 80 for flying wings (hang glider)


Airfoil mh80-il
Details Dat file Parser  
(mh80-il) MH 80 12.72%
Martin Hepperle MH 80 for flying wings (hang glider)
Max thickness 12.7% at 21.7% chord.
Max camber 2.8% at 21.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 80  12.72% 
  1.00000000  0.00000000
  0.99660556  0.00000514
  0.98645333  0.00016607
  0.96968276  0.00076337
  0.94658098  0.00205454
  0.91756694  0.00424726
  0.88317350  0.00749048
  0.84402414  0.01185586
  0.80081067  0.01734315
  0.75426720  0.02386933
  0.70514958  0.03128653
  0.65421180  0.03937743
  0.60219064  0.04788137
  0.54978763  0.05649349
  0.49765983  0.06489440
  0.44640900  0.07275031
  0.39657775  0.07974248
  0.34864660  0.08556501
  0.30303389  0.08995208
  0.26010133  0.09266608
  0.22015603  0.09352479
  0.18347245  0.09232061
  0.15008882  0.08885420
  0.11991466  0.08321496
  0.09296953  0.07563989
  0.06925895  0.06640879
  0.04882234  0.05594764
  0.03181396  0.04467971
  0.01834927  0.03299435
  0.00850385  0.02133690
  0.00232828  0.01028433
  0.00024095  0.00305228
  0.00000348  0.00034871
  0.00013904 -0.00211528
  0.00044985 -0.00359353
  0.00098996 -0.00488008
  0.00186551 -0.00603085
  0.00309213 -0.00715275
  0.00545368 -0.00880826
  0.00838081 -0.01044426
  0.01151718 -0.01192930
  0.02649037 -0.01705899
  0.04672421 -0.02169346
  0.07183447 -0.02565888
  0.10162766 -0.02874405
  0.13599855 -0.03096346
  0.17464593 -0.03250071
  0.21708451 -0.03347591
  0.26280322 -0.03394179
  0.31125714 -0.03395360
  0.36187560 -0.03354703
  0.41406444 -0.03276581
  0.46721388 -0.03163888
  0.52070354 -0.03020434
  0.57390980 -0.02848532
  0.62621187 -0.02651289
  0.67699845 -0.02429873
  0.72567384 -0.02185281
  0.77168250 -0.01912550
  0.81461756 -0.01606837
  0.85417627 -0.01277466
  0.89000484 -0.00947188
  0.92167906 -0.00641121
  0.94871229 -0.00383528
  0.97057090 -0.00191386
  0.98671189 -0.00071077
  0.99664289 -0.00014303
  1.00000000  0.00000000
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Polars for MH 80 12.72% (mh80-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh80-il50,000912.3 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh80-il50,000522.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh80-il100,000928.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh80-il100,000539.7 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   mh80-il200,000950.5 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh80-il200,000558.3 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   mh80-il500,000982.7 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh80-il500,000585.7 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh80-il1,000,0009109.2 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh80-il1,000,0005108.1 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
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