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MH33 (mh33-il)

MH33 - Martin Hepperle MH 33 for F3E and F3B


Airfoil mh33-il
Details Dat file Parser  
(mh33-il) MH33
Martin Hepperle MH 33 for F3E and F3B
Max thickness 7.3% at 29.3% chord.
Max camber 1.1% at 43.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
MH33
1.00000	0.00000
0.99677	0.00029
0.98727	0.00125
0.97194	0.00302
0.95125	0.00558
0.92567	0.00881
0.89564	0.01246
0.86150	0.01634
0.82361	0.02028
0.78231	0.02416
0.73804	0.02795
0.69129	0.03160
0.64259	0.03503
0.59247	0.03815
0.54149	0.04089
0.49020	0.04320
0.43914	0.04500
0.38888	0.04623
0.33993	0.04684
0.29281	0.04678
0.24801	0.04601
0.20596	0.04449
0.16706	0.04221
0.13167	0.03917
0.10009	0.03539
0.07258	0.03092
0.04934	0.02584
0.03048	0.02025
0.01611	0.01435
0.00623	0.00838
0.00091	0.00281
0.00034	0.00165
0.00000	0.00047
0.00002	-0.00054
0.00052	-0.00148
0.00147	-0.00246
0.00654	-0.00574
0.01761	-0.01005
0.03359	-0.01405
0.05440	-0.01756
0.07993	-0.02048
0.10997	-0.02280
0.14429	-0.02449
0.18256	-0.02558
0.22440	-0.02612
0.26940	-0.02614
0.31708	-0.02569
0.36693	-0.02485
0.41841	-0.02367
0.47093	-0.02222
0.52390	-0.02056
0.57671	-0.01875
0.62877	-0.01684
0.67944	-0.01490
0.72813	-0.01294
0.77427	-0.01102
0.81728	-0.00912
0.85667	-0.00723
0.89207	-0.00530
0.92320	-0.00344
0.94970	-0.00186
0.97112	-0.00073
0.98694	-0.00014
0.99670	-0.00001
1.00000	 0.00000
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Lednicer format dat file
Selig format dat file

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Polars for MH33 (mh33-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   mh33-il50,000932.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh33-il50,000531.9 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh33-il100,000946.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   mh33-il100,000542.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh33-il200,000959.5 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh33-il200,000551.2 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   mh33-il500,000972.9 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh33-il500,000564.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh33-il1,000,000981.2 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh33-il1,000,000574.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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