MH33 (mh33-il)
MH33 - Martin Hepperle MH 33 for F3E and F3B
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(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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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for MH33 (mh33-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh33-il | 50,000 | 9 | 32.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 50,000 | 5 | 31.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 100,000 | 9 | 46.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 100,000 | 5 | 42.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 200,000 | 9 | 59.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 200,000 | 5 | 51.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 500,000 | 9 | 72.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 500,000 | 5 | 64.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 1,000,000 | 9 | 81.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 1,000,000 | 5 | 74.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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