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MH 22 7.2% (mh22-il)

MH 22 7.2% - Martin Hepperle MH 22 for F3D Pylon Racing


Airfoil mh22-il
Details Dat file Parser  
(mh22-il) MH 22 7.2%
Martin Hepperle MH 22 for F3D Pylon Racing
Max thickness 7.2% at 27% chord.
Max camber 1.8% at 37% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 22  7.2% 
  1.00000000  0.00000000
  0.99679155  0.00013675
  0.98733295  0.00067257
  0.97198580  0.00174337
  0.95107411  0.00330160
  0.92485052  0.00532979
  0.89365096  0.00788451
  0.85793159  0.01100431
  0.81820263  0.01467336
  0.77502706  0.01886518
  0.72901193  0.02351081
  0.68080702  0.02852616
  0.63110026  0.03379639
  0.58071248  0.03913542
  0.53038538  0.04400422
  0.48035640  0.04786635
  0.43072104  0.05067633
  0.38190687  0.05259463
  0.33446347  0.05361697
  0.28888361  0.05369606
  0.24560019  0.05275831
  0.20496816  0.05078039
  0.16730827  0.04777110
  0.13288325  0.04380250
  0.10195888  0.03900116
  0.07478573  0.03350987
  0.05158008  0.02747666
  0.03248437  0.02109469
  0.01764180  0.01463882
  0.00718395  0.00841551
  0.00240606  0.00426407
  0.00116783  0.00270237
  0.00035054  0.00128154
  0.00005746  0.00043355
  0.00002852 -0.00029509
  0.00033344 -0.00097346
  0.00094593 -0.00168768
  0.00230626 -0.00280280
  0.00414045 -0.00397511
  0.00616717 -0.00507777
  0.01685431 -0.00897050
  0.03248253 -0.01239559
  0.05302498 -0.01515289
  0.07843283 -0.01719338
  0.10854412 -0.01853642
  0.14314411 -0.01923278
  0.18192732 -0.01938797
  0.22450229 -0.01911882
  0.27038279 -0.01855180
  0.31901963 -0.01777703
  0.36980328 -0.01686904
  0.42212370 -0.01583655
  0.47537514 -0.01471928
  0.52894156 -0.01353240
  0.58220369 -0.01231682
  0.63454507 -0.01108285
  0.68535966 -0.00986547
  0.73405747 -0.00866901
  0.78007210 -0.00752067
  0.82286580 -0.00641773
  0.86193649 -0.00537779
  0.89682206 -0.00438763
  0.92710650 -0.00345133
  0.95242177 -0.00251062
  0.97258094 -0.00151225
  0.98749078 -0.00062085
  0.99680701 -0.00012484
  1.00000000  0.00000000
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Polars for MH 22 7.2% (mh22-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh22-il50,000933.8 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh22-il50,000535 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh22-il100,000948.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh22-il100,000547.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh22-il200,000963.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh22-il200,000560.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh22-il500,000982.8 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh22-il500,000574.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh22-il1,000,000992.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   mh22-il1,000,000581.9 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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