MH 18 11.16% (mh18-il)
MH 18 11.16% - Martin Hepperle MH 18 for F3D Pylon Racing
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(mh18-il) MH 18 11.16% Martin Hepperle MH 18 for F3D Pylon Racing Max thickness 11.1% at 36.8% chord. Max camber 2.7% at 42.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 18 11.16% 1.00000000 0.00000000 0.99641612 -0.00002507 0.98568442 0.00017532 0.96798792 0.00122548 0.94390264 0.00371768 0.91434811 0.00790159 0.88021535 0.01363898 0.84225727 0.02066581 0.80117125 0.02866143 0.75759887 0.03726667 0.71213267 0.04610808 0.66532610 0.05481464 0.61770563 0.06304091 0.56985066 0.07039094 0.52213148 0.07626608 0.47449168 0.08032624 0.42698074 0.08275117 0.38003715 0.08379475 0.33419752 0.08352664 0.28994684 0.08196650 0.24771896 0.07910980 0.20787901 0.07499041 0.17076098 0.06967181 0.13664587 0.06327118 0.10581259 0.05595576 0.07852519 0.04791337 0.05501782 0.03933457 0.03545635 0.03045771 0.02000670 0.02158339 0.00881186 0.01306906 0.00206748 0.00538847 0.00092298 0.00329691 0.00021665 0.00141327 0.00000953 0.00027737 0.00007301 -0.00071624 0.00048234 -0.00164333 0.00121501 -0.00260352 0.00278078 -0.00408775 0.00485251 -0.00561460 0.01511210 -0.01059202 0.03051630 -0.01516893 0.05095935 -0.01907373 0.07633892 -0.02224615 0.10647490 -0.02467282 0.14113183 -0.02639251 0.17999376 -0.02748541 0.22265880 -0.02805801 0.26863463 -0.02821517 0.31736769 -0.02804072 0.36824543 -0.02759227 0.42065626 -0.02687788 0.47399254 -0.02592580 0.52763713 -0.02475532 0.58096932 -0.02340049 0.63337191 -0.02187991 0.68423783 -0.02022639 0.73297653 -0.01845619 0.77902077 -0.01659925 0.82183215 -0.01466757 0.86090764 -0.01268637 0.89578347 -0.01065697 0.92604144 -0.00859445 0.95130318 -0.00642146 0.97149797 -0.00403818 0.98672845 -0.00180657 0.99655036 -0.00041174 1.00000000 0.00000000 |
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Polars for MH 18 11.16% (mh18-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh18-il | 50,000 | 9 | 32.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh18-il | 50,000 | 5 | 31.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh18-il | 100,000 | 9 | 53.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh18-il | 100,000 | 5 | 53.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh18-il | 200,000 | 9 | 77.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh18-il | 200,000 | 5 | 74.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh18-il | 500,000 | 9 | 108.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh18-il | 500,000 | 5 | 96.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh18-il | 1,000,000 | 9 | 127.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh18-il | 1,000,000 | 5 | 107.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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