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MH 112 Airfoil (mh112-il)

MH 112 Airfoil - Martin Hepperle MH 112 for a propeller for ultralight (root)


Airfoil mh112-il
Details Dat file Parser  
(mh112-il) MH 112 Airfoil
Martin Hepperle MH 112 for a propeller for ultralight (root)
Max thickness 16.2% at 31.8% chord.
Max camber 6.7% at 48.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH 112  Airfoil
1.00000000  0.00000000
0.99649058  0.00136330
0.98660368  0.00547709
0.97143035  0.01199665
0.95144341  0.02016652
0.92670131  0.02961565
0.89752683  0.04030415
0.86449272  0.05205068
0.82816738  0.06453411
0.78908692  0.07737681
0.74774914  0.09018520
0.70462892  0.10256493
0.66017070  0.11411477
0.61473811  0.12444329
0.56862372  0.13327372
0.52216328  0.14043722
0.47572481  0.14579553
0.42968835  0.14925105
0.38444902  0.15070762
0.34032550  0.15006923
0.29755052  0.14737924
0.25646503  0.14284242
0.21755026  0.13658085
0.18117792  0.12859862
0.14758049  0.11898092
0.11697865  0.10791633
0.08960025  0.09562226
0.06563801  0.08233394
0.04525115  0.06832104
0.02856435  0.05388872
0.01569521  0.03937555
0.00671543  0.02509061
0.00153301  0.01141669
0.00001242 -0.00096463
0.00024127 -0.00410677
0.00081387 -0.00722284
0.00173454 -0.01004675
0.00255195 -0.01173186
0.00357223 -0.01319148
0.00490827 -0.01446260
0.00659548 -0.01564798
0.00965829 -0.01731512
0.01330108 -0.01886542
0.02415012 -0.02214263
0.04402578 -0.02550975
0.06928121 -0.02743757
0.09968072 -0.02797448
0.13497116 -0.02718773
0.17484399 -0.02520125
0.21893213 -0.02216602
0.26679856 -0.01826931
0.31793754 -0.01370545
0.37179503 -0.00867603
0.42777046 -0.00338197
0.48527553  0.00198303
0.54373728  0.00709861
0.60239110  0.01153371
0.66029295  0.01496970
0.71646983  0.01721591
0.76993975  0.01818017
0.81975105  0.01787304
0.86499658  0.01639631
0.90486064  0.01394373
0.93860949  0.01072049
0.96545654  0.00702160
0.98472163  0.00348974
0.99619815  0.00093082
1.00000000  0.00000000
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Polars for MH 112 Airfoil (mh112-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh112-il50,00095.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh112-il50,000514.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   mh112-il100,000937.5 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   mh112-il100,000548.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh112-il200,000980 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh112-il200,000579.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   mh112-il500,0009120 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh112-il500,0005109.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh112-il1,000,0009147.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   mh112-il1,000,0005126.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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