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MH 83 13.29% (mh83-il)

MH 83 13.29% - Martin Hepperle MH 83 for flying wings (hang glider)


Airfoil mh83-il
Details Dat file Parser  
(mh83-il) MH 83 13.29%
Martin Hepperle MH 83 for flying wings (hang glider)
Max thickness 13.3% at 20.6% chord.
Max camber 4.5% at 32.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 83  13.29% 
  1.00000000  0.00000000
  0.99672899  0.00023531
  0.98692015  0.00105909
  0.97067687  0.00270324
  0.94828399  0.00539362
  0.92017987  0.00930135
  0.88692215  0.01451151
  0.84915122  0.02101885
  0.80755444  0.02872112
  0.76283812  0.03744000
  0.71570277  0.04692639
  0.66682923  0.05689064
  0.61686578  0.06700863
  0.56642450  0.07695042
  0.51607614  0.08638244
  0.46635061  0.09498995
  0.41773609  0.10247569
  0.37067945  0.10857433
  0.32558827  0.11305067
  0.28282991  0.11570049
  0.24273788  0.11635457
  0.20561919  0.11479920
  0.17152651  0.11078192
  0.14030239  0.10437574
  0.11194905  0.09588278
  0.08651914  0.08562563
  0.06410720  0.07401037
  0.04487146  0.06144195
  0.02895817  0.04829127
  0.01643834  0.03496114
  0.00738178  0.02194452
  0.00186084  0.00980901
  0.00001234 -0.00071636
  0.00251705 -0.00820350
  0.01097300 -0.01311972
  0.02576247 -0.01701952
  0.04595299 -0.01988167
  0.07130800 -0.02147549
  0.10180881 -0.02183252
  0.13719509 -0.02122627
  0.17697415 -0.01972974
  0.22087767 -0.01733495
  0.26860005 -0.01436151
  0.31951728 -0.01112325
  0.37296418 -0.00779589
  0.42824721 -0.00454959
  0.48464857 -0.00150842
  0.54143765  0.00120733
  0.59787625  0.00351022
  0.65322965  0.00531493
  0.70677237  0.00654986
  0.75775133  0.00712877
  0.80538094  0.00705020
  0.84892399  0.00640401
  0.88774524  0.00535858
  0.92132880  0.00409926
  0.94927565  0.00281611
  0.97129304  0.00166527
  0.98717606  0.00076798
  0.99678156  0.00019745
  1.00000000  0.00000000
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Polars for MH 83 13.29% (mh83-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh83-il50,000912.8 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   mh83-il50,000526.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh83-il100,000934.1 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh83-il100,000546.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh83-il200,000959.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh83-il200,000567.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh83-il500,000994.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh83-il500,000597.6 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh83-il1,000,0009123.8 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   mh83-il1,000,0005123.9 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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