MH 93 15.98% (mh93-il)
MH 93 15.98% - Martin Hepperle MH 93 parafoil
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(mh93-il) MH 93 15.98% Martin Hepperle MH 93 parafoil Max thickness 16% at 27.6% chord. Max camber 1.4% at 15.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 93 15.98% 1.00000000 0.00000000 0.99629901 -0.00000249 0.98529378 0.00022786 0.96727814 0.00113691 0.94272226 0.00306138 0.91223431 0.00621867 0.87651673 0.01069994 0.83632569 0.01647317 0.79243435 0.02340032 0.74560501 0.03125613 0.69656956 0.03975591 0.64601753 0.04857685 0.59459116 0.05738372 0.54288414 0.06584458 0.49144445 0.07364867 0.44077768 0.08051462 0.39135220 0.08619985 0.34360345 0.09050272 0.29793895 0.09326233 0.25474286 0.09435692 0.21438350 0.09366763 0.17712081 0.09106409 0.14310326 0.08653903 0.11249794 0.08017057 0.08538263 0.07204380 0.06174287 0.06244955 0.04175339 0.05181101 0.02563112 0.04037046 0.01334602 0.02841939 0.00492091 0.01653887 0.00058215 0.00532797 0.00022806 0.00326243 0.00000090 0.00019698 0.00017431 -0.00268261 0.00052897 -0.00446817 0.00112589 -0.00609415 0.00205535 -0.00762008 0.00332302 -0.00914645 0.00573295 -0.01145125 0.00869715 -0.01377409 0.01911749 -0.02007239 0.03674103 -0.02784760 0.05919288 -0.03537193 0.08611348 -0.04247013 0.11715332 -0.04895444 0.15198581 -0.05464135 0.19029189 -0.05941607 0.23166376 -0.06318398 0.27573558 -0.06579413 0.32221000 -0.06723924 0.37063765 -0.06764018 0.42043990 -0.06703337 0.47110912 -0.06537816 0.52220287 -0.06273993 0.57318105 -0.05926936 0.62341660 -0.05505167 0.67233908 -0.05006063 0.71955171 -0.04428392 0.76473930 -0.03788000 0.80752560 -0.03112834 0.84747937 -0.02435334 0.88410586 -0.01790393 0.91686442 -0.01210971 0.94516525 -0.00729281 0.96832511 -0.00370331 0.98561221 -0.00141853 0.99634847 -0.00030032 1.00000000 0.00000000 |
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Polars for MH 93 15.98% (mh93-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh93-il | 50,000 | 9 | 14.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 50,000 | 5 | 24.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 100,000 | 9 | 33.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 100,000 | 5 | 39.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 200,000 | 9 | 52.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 200,000 | 5 | 53.2 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 500,000 | 9 | 74.4 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 500,000 | 5 | 71.3 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 1,000,000 | 9 | 92 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 1,000,000 | 5 | 88.9 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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