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MH 95 15.86% (mh95-il)

MH 95 15.86% - Martin Hepperle MH 95 parafoil


Airfoil mh95-il
Details Dat file Parser  
(mh95-il) MH 95 15.86%
Martin Hepperle MH 95 parafoil
Max thickness 15.8% at 33.6% chord.
Max camber 0.9% at 81.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 95  15.86% 
  1.00000000  0.00000000
  0.99613463  0.00089175
  0.98525133  0.00368100
  0.96849335  0.00829916
  0.94657783  0.01433614
  0.92002417  0.02137586
  0.88924640  0.02901834
  0.85458309  0.03690385
  0.81632849  0.04477352
  0.77483401  0.05247457
  0.73053846  0.05987315
  0.68390550  0.06683561
  0.63544809  0.07325957
  0.58572205  0.07901097
  0.53526323  0.08394066
  0.48458283  0.08792380
  0.43419484  0.09087208
  0.38460973  0.09271123
  0.33633074  0.09339292
  0.28985022  0.09288191
  0.24564576  0.09116145
  0.20417934  0.08822440
  0.16590012  0.08403888
  0.13113128  0.07852833
  0.10005118  0.07175734
  0.07293327  0.06395791
  0.05023285  0.05520734
  0.03212292  0.04523379
  0.01819093  0.03404712
  0.00816384  0.02225781
  0.00209172  0.01048013
  0.00000796 -0.00061143
  0.00264019 -0.00967365
  0.01131284 -0.01725366
  0.02603613 -0.02476388
  0.04594663 -0.03208292
  0.07062714 -0.03903295
  0.09970541 -0.04545496
  0.13279922 -0.05116084
  0.16960433 -0.05594167
  0.20985646 -0.05973603
  0.25314594 -0.06256784
  0.29899844 -0.06439753
  0.34696906 -0.06521703
  0.39652627 -0.06507526
  0.44709454 -0.06395938
  0.49811163 -0.06185897
  0.54899576 -0.05871106
  0.59929429 -0.05438810
  0.64872662 -0.04888129
  0.69702471 -0.04238377
  0.74385415 -0.03520856
  0.78879968 -0.02775361
  0.83135926 -0.02045543
  0.87092428 -0.01376861
  0.90679840 -0.00809418
  0.93819221 -0.00380110
  0.96416369 -0.00111008
  0.98369391  0.00005140
  0.99586173  0.00013530
  1.00000000  0.00000000
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Lednicer format dat file
Selig format dat file

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Polars for MH 95 15.86% (mh95-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh95-il50,000929.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh95-il50,000529 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh95-il100,000944.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   mh95-il100,000537.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh95-il200,000948.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh95-il200,000545.6 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh95-il500,000962.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh95-il500,000560.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh95-il1,000,000978 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh95-il1,000,000574.3 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
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