MH 94 16.03% (mh94-il)
MH 94 16.03% - Martin Hepperle MH 94 parafoil
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(mh94-il) MH 94 16.03% Martin Hepperle MH 94 parafoil Max thickness 16% at 34.1% chord. Max camber 1.3% at 74.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 94 16.03% 1.00000000 0.00000000 0.99614372 0.00075299 0.98517671 0.00333401 0.96830215 0.00791992 0.94649402 0.01402570 0.92026080 0.02095000 0.88973146 0.02820043 0.85508517 0.03563506 0.81672309 0.04314656 0.77508519 0.05056529 0.73062549 0.05773357 0.68381258 0.06451128 0.63516360 0.07079345 0.58523861 0.07644452 0.53457659 0.08131354 0.48369158 0.08527460 0.43309941 0.08823799 0.38331241 0.09012917 0.33483473 0.09089917 0.28815954 0.09051388 0.24376407 0.08895853 0.20210913 0.08623149 0.16363849 0.08232026 0.12870704 0.07719396 0.09757690 0.07091355 0.07057780 0.06364984 0.04819402 0.05539707 0.03057188 0.04577057 0.01719105 0.03470861 0.00764984 0.02283091 0.00189225 0.01087021 0.00009267 0.00224978 0.00001765 -0.00095529 0.00032505 -0.00396814 0.00075957 -0.00584078 0.00142995 -0.00755383 0.00242711 -0.00916513 0.00375797 -0.01077418 0.00625502 -0.01320275 0.00929562 -0.01565318 0.01213430 -0.01765654 0.02706679 -0.02586635 0.04695544 -0.03392209 0.07139743 -0.04161035 0.10003434 -0.04873110 0.13249136 -0.05506483 0.16846717 -0.06036927 0.20768971 -0.06453603 0.24975415 -0.06750568 0.29425010 -0.06913386 0.34084964 -0.06935266 0.38914135 -0.06817672 0.43872227 -0.06557834 0.48925488 -0.06163067 0.54033971 -0.05651794 0.59150812 -0.05044548 0.64229382 -0.04362756 0.69222519 -0.03635324 0.74077134 -0.02896693 0.78733031 -0.02183431 0.83123834 -0.01530560 0.87176711 -0.00970008 0.90814574 -0.00525534 0.93957516 -0.00213286 0.96521882 -0.00035294 0.98426413 0.00027050 0.99602038 0.00016420 1.00000000 0.00000000 |
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Polars for MH 94 16.03% (mh94-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh94-il | 50,000 | 9 | 29.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh94-il | 50,000 | 5 | 27.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh94-il | 100,000 | 9 | 40.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh94-il | 100,000 | 5 | 36.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh94-il | 200,000 | 9 | 46.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh94-il | 200,000 | 5 | 45.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh94-il | 500,000 | 9 | 62.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh94-il | 500,000 | 5 | 61.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh94-il | 1,000,000 | 9 | 76.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh94-il | 1,000,000 | 5 | 75.8 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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