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MH 92 15.49% (mh92-il)

MH 92 15.49% - Martin Hepperle MH 92 parafoil


Airfoil mh92-il
Details Dat file Parser  
(mh92-il) MH 92 15.49%
Martin Hepperle MH 92 parafoil
Max thickness 15.5% at 27.4% chord.
Max camber 1.4% at 15.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 92  15.49% 
  1.00000000  0.00000000
  0.99633872  0.00001428
  0.98545250  0.00028221
  0.96763131  0.00122590
  0.94333460  0.00316141
  0.91315409  0.00628974
  0.87777187  0.01069168
  0.83792168  0.01633086
  0.79435446  0.02307184
  0.74781233  0.03069732
  0.69901082  0.03893576
  0.64862776  0.04748016
  0.59729909  0.05601314
  0.54561742  0.06421991
  0.49413452  0.07180588
  0.44336376  0.07850262
  0.39378431  0.08407750
  0.34584440  0.08833437
  0.29996511  0.09111414
  0.25654416  0.09229230
  0.21596209  0.09174317
  0.17848702  0.08932537
  0.14427066  0.08502261
  0.11348589  0.07890479
  0.08621359  0.07104318
  0.06243573  0.06171724
  0.04232565  0.05134219
  0.02609688  0.04014595
  0.01370377  0.02841058
  0.00515770  0.01671833
  0.00067451  0.00566514
  0.00023037  0.00322571
  0.00000114  0.00021836
  0.00017002 -0.00260170
  0.00051983 -0.00434660
  0.00111003 -0.00593056
  0.00203193 -0.00741246
  0.00329225 -0.00889275
  0.00569150 -0.01112517
  0.00864532 -0.01337250
  0.01845875 -0.01916801
  0.03586151 -0.02667258
  0.05812042 -0.03392187
  0.08487535 -0.04074726
  0.11577817 -0.04696528
  0.15050330 -0.05239667
  0.18873415 -0.05693040
  0.23006351 -0.06047669
  0.27412687 -0.06288683
  0.32062963 -0.06415794
  0.36912329 -0.06441690
  0.41902716 -0.06370531
  0.46983237 -0.06198523
  0.52109603 -0.05932658
  0.57227601 -0.05588560
  0.62274160 -0.05175359
  0.67191802 -0.04691350
  0.71939255 -0.04136645
  0.76482240 -0.03527140
  0.80780600 -0.02889431
  0.84789317 -0.02253676
  0.88457846 -0.01651882
  0.91732099 -0.01113743
  0.94554239 -0.00668307
  0.96858273 -0.00337886
  0.98574378 -0.00128697
  0.99638426 -0.00027076
  1.00000000  0.00000000
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Polars for MH 92 15.49% (mh92-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh92-il50,000915.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   mh92-il50,000524.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh92-il100,000933.8 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh92-il100,000540 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh92-il200,000952.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   mh92-il200,000554.7 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh92-il500,000976.6 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh92-il500,000573.4 at α=10.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh92-il1,000,000994.2 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh92-il1,000,000590.1 at α=10.25°Mach=0 Ncrit=5Xfoil predictionDetails
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