MH 44 9.66% (mh44-il)
MH 44 9.66% - Martin Hepperle MH 44 for flying wings
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(mh44-il) MH 44 9.66% Martin Hepperle MH 44 for flying wings Max thickness 9.6% at 27.1% chord. Max camber 1.5% at 36.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 44 9.66% 1.00000000 0.00000000 0.99653011 0.00006570 0.98631190 0.00045598 0.96974340 0.00149517 0.94725184 0.00334612 0.91930910 0.00609337 0.88644951 0.00977957 0.84928493 0.01440044 0.80853520 0.01988463 0.76501741 0.02593772 0.71928426 0.03201301 0.67158211 0.03781515 0.62232193 0.04331441 0.57208418 0.04841899 0.52140861 0.05295553 0.47079118 0.05680855 0.42076549 0.05988591 0.37185888 0.06206495 0.32453101 0.06322567 0.27921124 0.06329856 0.23629096 0.06222447 0.19611034 0.06000566 0.15900561 0.05668847 0.12529908 0.05233411 0.09526462 0.04699913 0.06910337 0.04078625 0.04698628 0.03384119 0.02902831 0.02635644 0.01532232 0.01857810 0.00589505 0.01084457 0.00142333 0.00486961 0.00055408 0.00283988 0.00008249 0.00095342 0.00000391 -0.00019591 0.00016998 -0.00121038 0.00066308 -0.00215426 0.00147537 -0.00312101 0.00316245 -0.00460778 0.00535666 -0.00613866 0.00687346 -0.00706058 0.01851334 -0.01222489 0.03515031 -0.01724079 0.05648923 -0.02189643 0.08226781 -0.02596502 0.11229580 -0.02921248 0.14645533 -0.03153390 0.18453207 -0.03294836 0.22624958 -0.03352073 0.27121906 -0.03338609 0.31895653 -0.03264354 0.36894467 -0.03138667 0.42064059 -0.02970406 0.47346260 -0.02770997 0.52679860 -0.02549695 0.58001348 -0.02317072 0.63245725 -0.02079951 0.68348629 -0.01845282 0.73247007 -0.01616283 0.77880961 -0.01396515 0.82194185 -0.01186964 0.86134328 -0.00990001 0.89653379 -0.00805521 0.92708001 -0.00634860 0.95259909 -0.00476002 0.97276882 -0.00326398 0.98743380 -0.00175502 0.99669367 -0.00048443 1.00000000 0.00000000 |
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Polars for MH 44 9.66% (mh44-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh44-il | 50,000 | 9 | 29.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 50,000 | 5 | 32.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh44-il | 100,000 | 9 | 44.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 100,000 | 5 | 45.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh44-il | 200,000 | 9 | 60.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 200,000 | 5 | 58.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh44-il | 500,000 | 9 | 80.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 500,000 | 5 | 74.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh44-il | 1,000,000 | 9 | 94.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 1,000,000 | 5 | 87.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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