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MH 38 9.68% (mh38-il)

MH 38 9.68% - Martin Hepperle MH 38 for Endurance Model


Airfoil mh38-il
Details Dat file Parser  
(mh38-il) MH 38 9.68%
Martin Hepperle MH 38 for Endurance Model
Max thickness 9.7% at 31.6% chord.
Max camber 3.9% at 45.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 38  9.68% 
  1.00000000  0.00000000
  0.99681503  0.00052829
  0.98744069  0.00206411
  0.97219660  0.00461800
  0.95140806  0.00820800
  0.92548959  0.01281789
  0.89490506  0.01838273
  0.86016416  0.02479642
  0.82181533  0.03191761
  0.78043788  0.03956173
  0.73663624  0.04751042
  0.69102740  0.05547946
  0.64418318  0.06313426
  0.59661875  0.07011860
  0.54875352  0.07607236
  0.50090364  0.08072602
  0.45336696  0.08391210
  0.40640999  0.08556514
  0.36036364  0.08573940
  0.31562154  0.08448700
  0.27256521  0.08186533
  0.23156049  0.07795837
  0.19296831  0.07288249
  0.15714479  0.06675919
  0.12440457  0.05971034
  0.09500846  0.05189461
  0.06919502  0.04351376
  0.04717790  0.03479969
  0.02915078  0.02601488
  0.01528686  0.01746260
  0.00575479  0.00948521
  0.00235064  0.00541874
  0.00111503  0.00342820
  0.00031376  0.00160406
  0.00004242  0.00050128
  0.00003977 -0.00047153
  0.00036581 -0.00138795
  0.00098926 -0.00233639
  0.00235538 -0.00378184
  0.00418802 -0.00522915
  0.00770050 -0.00733786
  0.01930582 -0.01179167
  0.03580768 -0.01540495
  0.05722344 -0.01796634
  0.08354806 -0.01940709
  0.11472174 -0.01979314
  0.15054213 -0.01929586
  0.19065718 -0.01808367
  0.23464739 -0.01630031
  0.28202506 -0.01409517
  0.33225215 -0.01160078
  0.38474591 -0.00895640
  0.43888457 -0.00628764
  0.49401514 -0.00372487
  0.54945063 -0.00138348
  0.60447998  0.00063604
  0.65838377  0.00226561
  0.71044473  0.00346256
  0.75997115  0.00422322
  0.80630433  0.00456190
  0.84883284  0.00452284
  0.88699574  0.00415677
  0.92028513  0.00353829
  0.94826245  0.00274890
  0.97054484  0.00186730
  0.98678139  0.00099194
  0.99667312  0.00027913
  1.00000000  0.00000000
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Polars for MH 38 9.68% (mh38-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh38-il50,000937.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh38-il50,000537.8 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   mh38-il100,000961.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh38-il100,000561.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh38-il200,000986.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh38-il200,000585.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh38-il500,0009122.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh38-il500,0005114.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh38-il1,000,0009149.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh38-il1,000,0005133.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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