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MH 26 10.99% (mh26-il)

MH 26 10.99% - Martin Hepperle MH 26 for F3D Pylon Racing (extended laminar flow)


Airfoil mh26-il
Details Dat file Parser  
(mh26-il) MH 26 10.99%
Martin Hepperle MH 26 for F3D Pylon Racing (extended laminar flow)
Max thickness 11% at 42.3% chord.
Max camber 1.4% at 42.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 26  10.99% 
  1.00000000  0.00000000
  0.99601781  0.00046831
  0.98473175  0.00248610
  0.96741634  0.00651912
  0.94515820  0.01227929
  0.91873452  0.01926938
  0.88872819  0.02691697
  0.85561228  0.03455836
  0.81944363  0.04146234
  0.78000170  0.04745488
  0.73748441  0.05275405
  0.69240304  0.05741421
  0.64522702  0.06138663
  0.59647521  0.06467396
  0.54669436  0.06722025
  0.49642217  0.06899243
  0.44619893  0.06994448
  0.39656117  0.07005849
  0.34803353  0.06930017
  0.30111871  0.06766885
  0.25630079  0.06515540
  0.21403239  0.06177982
  0.17473071  0.05755263
  0.13875834  0.05252349
  0.10644453  0.04675219
  0.07806222  0.04033465
  0.05384673  0.03338246
  0.03396206  0.02605438
  0.01854895  0.01855724
  0.00768316  0.01117645
  0.00187433  0.00493409
  0.00081881  0.00301619
  0.00018015  0.00124527
  0.00000397  0.00017301
  0.00008904 -0.00076520
  0.00051730 -0.00163957
  0.00127385 -0.00254651
  0.00288623 -0.00395604
  0.00501517 -0.00542464
  0.01687170 -0.01082804
  0.03318330 -0.01565441
  0.05452977 -0.02012518
  0.08074741 -0.02415094
  0.11160822 -0.02771464
  0.14679334 -0.03084557
  0.18587433 -0.03355543
  0.22839759 -0.03581251
  0.27386950 -0.03759285
  0.32180470 -0.03883850
  0.37171646 -0.03956364
  0.42306202 -0.03979884
  0.47524771 -0.03958505
  0.52767311 -0.03892214
  0.57973433 -0.03783462
  0.63083169 -0.03631376
  0.68037516 -0.03437271
  0.72780057 -0.03197813
  0.77257463 -0.02913554
  0.81416230 -0.02571283
  0.85240703 -0.02152702
  0.88731280 -0.01691915
  0.91838421 -0.01235216
  0.94522412 -0.00793007
  0.96763381 -0.00409126
  0.98495940 -0.00145091
  0.99611690 -0.00024070
  1.00000000  0.00000000
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Polars for MH 26 10.99% (mh26-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh26-il50,000934.3 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh26-il50,000532 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh26-il100,000951.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh26-il100,000547.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh26-il200,000971.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh26-il200,000557.8 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh26-il500,000977.8 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   mh26-il500,000558.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh26-il1,000,000974.8 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh26-il1,000,000566.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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