MH 20 9.01% (mh20-il)
MH 20 9.01% - Martin Hepperle MH 20 for F3D Pylon Racing
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(mh20-il) MH 20 9.01% Martin Hepperle MH 20 for F3D Pylon Racing Max thickness 9% at 32.2% chord. Max camber 1.9% at 37.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 20 9.01% 1.00000000 0.00000000 0.99663722 -0.00000502 0.98661979 0.00015827 0.97016021 0.00083998 0.94762865 0.00232279 0.91954306 0.00478393 0.88649448 0.00827457 0.84911235 0.01276792 0.80805809 0.01815911 0.76400822 0.02428373 0.71763596 0.03091656 0.66960153 0.03779462 0.62054465 0.04463611 0.57116423 0.05108921 0.52197689 0.05654881 0.47303495 0.06058278 0.42440107 0.06327690 0.37650891 0.06484632 0.32990396 0.06532833 0.28507654 0.06470811 0.24245961 0.06294654 0.20241194 0.06004635 0.16525807 0.05604350 0.13126736 0.05103062 0.10070840 0.04515568 0.07383715 0.03858238 0.05087461 0.03148085 0.03197380 0.02406597 0.01728446 0.01663089 0.00695149 0.00951360 0.00230137 0.00483181 0.00108635 0.00304916 0.00030031 0.00141854 0.00003307 0.00043894 0.00003397 -0.00041277 0.00037497 -0.00121038 0.00103088 -0.00204638 0.00246899 -0.00334802 0.00439569 -0.00470397 0.00659525 -0.00600849 0.01770495 -0.01053427 0.03378029 -0.01462203 0.05477004 -0.01806289 0.08059598 -0.02079484 0.11108204 -0.02281900 0.14599903 -0.02417183 0.18503357 -0.02493978 0.22778877 -0.02522602 0.27377743 -0.02513931 0.32245228 -0.02476081 0.37320774 -0.02415208 0.42543910 -0.02331965 0.47854562 -0.02229529 0.53191756 -0.02109606 0.58494209 -0.01975863 0.63701018 -0.01829908 0.68752329 -0.01675217 0.73589960 -0.01513154 0.78158078 -0.01346836 0.82403743 -0.01177234 0.86277561 -0.01006936 0.89734096 -0.00836027 0.92732470 -0.00666124 0.95236187 -0.00491317 0.97233203 -0.00304938 0.98724618 -0.00134670 0.99671459 -0.00030431 1.00000000 0.00000000 |
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Polars for MH 20 9.01% (mh20-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh20-il | 50,000 | 9 | 33.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 50,000 | 5 | 34.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 100,000 | 9 | 50.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 100,000 | 5 | 50.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 200,000 | 9 | 68.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 200,000 | 5 | 64.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 500,000 | 9 | 91.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 500,000 | 5 | 81.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 1,000,000 | 9 | 105.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 1,000,000 | 5 | 93.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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