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MH 114 13.02% (mh114-il)

MH 114 13.02% - Martin Hepperle MH 114 for a propeller for ultralight


Airfoil mh114-il
Details Dat file Parser  
(mh114-il) MH 114 13.02%
Martin Hepperle MH 114 for a propeller for ultralight
Max thickness 13% at 28.1% chord.
Max camber 6.4% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 114  13.02% 
  1.00000000  0.00000000
  0.99667566  0.00127091
  0.98731466  0.00508030
  0.97294285  0.01102133
  0.95394941  0.01828860
  0.93028455  0.02649819
  0.90217220  0.03564269
  0.87010598  0.04559033
  0.83458560  0.05609031
  0.79610663  0.06685087
  0.75515297  0.07756051
  0.71219794  0.08789714
  0.66769773  0.09753021
  0.62204386  0.10612640
  0.57556669  0.11344647
  0.52862389  0.11933627
  0.48159244  0.12368504
  0.43486602  0.12642440
  0.38885365  0.12751147
  0.34396060  0.12692343
  0.30058729  0.12465754
  0.25910372  0.12072122
  0.21984312  0.11515990
  0.18310506  0.10804821
  0.14914254  0.09951468
  0.11819963  0.08974616
  0.09051427  0.07895233
  0.06629112  0.06735503
  0.04568918  0.05520889
  0.02883347  0.04280482
  0.01580501  0.03047906
  0.00665698  0.01863245
  0.00139717  0.00777183
  0.00021738  0.00285253
  0.00000128  0.00020630
  0.00015578 -0.00218399
  0.00047748 -0.00360344
  0.00102029 -0.00482311
  0.00188207 -0.00589101
  0.00307710 -0.00690420
  0.00536346 -0.00833777
  0.00818256 -0.00966916
  0.01396759 -0.01167125
  0.02998040 -0.01489783
  0.05146211 -0.01693984
  0.07820223 -0.01780217
  0.10998679 -0.01752983
  0.14654017 -0.01622017
  0.18753106 -0.01399145
  0.23256226 -0.01100035
  0.28117044 -0.00741551
  0.33282653 -0.00342225
  0.38695746  0.00080409
  0.44295096  0.00506331
  0.50015235  0.00915869
  0.55787098  0.01286723
  0.61535885  0.01597279
  0.67182118  0.01826471
  0.72640660  0.01957527
  0.77822736  0.01980849
  0.82641818  0.01896858
  0.87014991  0.01711775
  0.90865700  0.01440675
  0.94123377  0.01098584
  0.96708092  0.00711905
  0.98551223  0.00347938
  0.99640825  0.00091297
  1.00000000  0.00000000
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Polars for MH 114 13.02% (mh114-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh114-il50,00099.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh114-il50,000526 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   mh114-il100,000956.2 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh114-il100,000560.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh114-il200,000989.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh114-il200,000588.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh114-il500,0009131.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh114-il500,0005121 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh114-il1,000,0009161 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   mh114-il1,000,0005140.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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