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MH 201 13.08% (mh201-il)

MH 201 13.08% - Martin Hepperle MH 201 for a canard airplane (canard)


Airfoil mh201-il
Details Dat file Parser  
(mh201-il) MH 201 13.08%
Martin Hepperle MH 201 for a canard airplane (canard)
Max thickness 13% at 38.1% chord.
Max camber 2.5% at 48.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 201  13.08% 
  1.00000000  0.00000000
  0.99656789  0.00095473
  0.98687599  0.00389591
  0.97196794  0.00851415
  0.95226366  0.01402658
  0.92767454  0.02006559
  0.89837640  0.02670727
  0.86485652  0.03392207
  0.82762512  0.04156867
  0.78722794  0.04947216
  0.74423437  0.05741170
  0.69923009  0.06512321
  0.65280025  0.07223609
  0.60530062  0.07828560
  0.55687451  0.08310525
  0.50788998  0.08677991
  0.45887051  0.08929239
  0.41027604  0.09059454
  0.36257864  0.09069796
  0.31626235  0.08960164
  0.27178729  0.08731824
  0.22959145  0.08386618
  0.19007998  0.07928766
  0.15363166  0.07363032
  0.12056975  0.06695830
  0.09116986  0.05936158
  0.06565468  0.05096868
  0.04422060  0.04193182
  0.02698038  0.03241454
  0.01397005  0.02266973
  0.00518508  0.01307097
  0.00085149  0.00482642
  0.00023039  0.00236360
  0.00000043  0.00009610
  0.00008139 -0.00127830
  0.00040774 -0.00248990
  0.00107413 -0.00360381
  0.00208167 -0.00472355
  0.00409681 -0.00642000
  0.00665868 -0.00813782
  0.01995142 -0.01428476
  0.03767845 -0.01977123
  0.06027978 -0.02478188
  0.08754050 -0.02917637
  0.11919577 -0.03288123
  0.15494345 -0.03584764
  0.19443073 -0.03806197
  0.23726330 -0.03953853
  0.28295446 -0.04033285
  0.33093935 -0.04043141
  0.38068971 -0.03978034
  0.43171287 -0.03837672
  0.48343059 -0.03628783
  0.53518729 -0.03344972
  0.58648383 -0.02970569
  0.63695210 -0.02494143
  0.68647091 -0.01908444
  0.73516675 -0.01258226
  0.78262750 -0.00641108
  0.82788647 -0.00126676
  0.86992377  0.00246584
  0.90771526  0.00459957
  0.94026672  0.00506834
  0.96644799  0.00401635
  0.98523920  0.00217691
  0.99634706  0.00059777
  1.00000000  0.00000000
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Polars for MH 201 13.08% (mh201-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh201-il50,000933.9 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   mh201-il50,000534.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh201-il100,000955 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh201-il100,000552.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh201-il200,000973.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh201-il200,000567 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh201-il500,000995.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh201-il500,000585.1 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh201-il1,000,0009113.6 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh201-il1,000,000595.9 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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