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MH 82 13.31% (mh82-il)

MH 82 13.31% - Martin Hepperle MH 82 for flying wings (hang glider)


Airfoil mh82-il
Details Dat file Parser  
(mh82-il) MH 82 13.31%
Martin Hepperle MH 82 for flying wings (hang glider)
Max thickness 13.3% at 24.6% chord.
Max camber 3.9% at 24.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 82  13.31% 
  1.00000000  0.00000000
  0.99661459  0.00010716
  0.98648759  0.00057417
  0.96976242  0.00167959
  0.94674359  0.00367565
  0.91787545  0.00675919
  0.88371761  0.01105153
  0.84491677  0.01659048
  0.80217789  0.02332527
  0.75623764  0.03112511
  0.70784007  0.03978495
  0.65771739  0.04904355
  0.60657341  0.05859424
  0.55507239  0.06810553
  0.50383005  0.07723291
  0.45340892  0.08563711
  0.40431563  0.09299494
  0.35700062  0.09901144
  0.31186073  0.10342997
  0.26924218  0.10603084
  0.22944828  0.10664471
  0.19275386  0.10507496
  0.15919742  0.10111480
  0.12865471  0.09486478
  0.10114620  0.08660842
  0.07670830  0.07665259
  0.05541508  0.06541510
  0.03742189  0.05331020
  0.02286177  0.04072192
  0.01180557  0.02807192
  0.00430956  0.01589603
  0.00048929  0.00484950
  0.00007086  0.00175419
  0.00002622 -0.00101996
  0.00034816 -0.00353243
  0.00078039 -0.00502846
  0.00143495 -0.00631603
  0.00242331 -0.00744430
  0.00376965 -0.00852044
  0.00632469 -0.01007170
  0.00946271 -0.01156191
  0.01867771 -0.01481702
  0.03671504 -0.01897587
  0.05993648 -0.02230735
  0.08812913 -0.02462698
  0.12123607 -0.02596768
  0.15896894 -0.02658615
  0.20083798 -0.02664454
  0.24631809 -0.02624375
  0.29484983 -0.02546371
  0.34584166 -0.02437799
  0.39867639 -0.02304567
  0.45271686 -0.02152507
  0.50731291 -0.01986154
  0.56180823 -0.01809995
  0.61554743 -0.01627195
  0.66788318 -0.01440561
  0.71818292 -0.01251060
  0.76584748 -0.01056846
  0.81037800 -0.00854699
  0.85134987 -0.00650607
  0.88832129 -0.00457027
  0.92082546 -0.00287905
  0.94837899 -0.00154846
  0.97049733 -0.00064794
  0.98672053 -0.00016877
  0.99665170 -0.00001402
  1.00000000  0.00000000
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Polars for MH 82 13.31% (mh82-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh82-il50,000911.1 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh82-il50,000523.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh82-il100,000929.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh82-il100,000542.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh82-il200,000953.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   mh82-il200,000561.7 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh82-il500,000987.1 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh82-il500,000590.5 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh82-il1,000,0009115.3 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   mh82-il1,000,0005115.2 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
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