MH 22 7.2% (mh22-il)
MH 22 7.2% - Martin Hepperle MH 22 for F3D Pylon Racing
| Details | Dat file | Parser | |
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(mh22-il) MH 22 7.2% Martin Hepperle MH 22 for F3D Pylon Racing Max thickness 7.2% at 27% chord. Max camber 1.8% at 37% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 22 7.2% 1.00000000 0.00000000 0.99679155 0.00013675 0.98733295 0.00067257 0.97198580 0.00174337 0.95107411 0.00330160 0.92485052 0.00532979 0.89365096 0.00788451 0.85793159 0.01100431 0.81820263 0.01467336 0.77502706 0.01886518 0.72901193 0.02351081 0.68080702 0.02852616 0.63110026 0.03379639 0.58071248 0.03913542 0.53038538 0.04400422 0.48035640 0.04786635 0.43072104 0.05067633 0.38190687 0.05259463 0.33446347 0.05361697 0.28888361 0.05369606 0.24560019 0.05275831 0.20496816 0.05078039 0.16730827 0.04777110 0.13288325 0.04380250 0.10195888 0.03900116 0.07478573 0.03350987 0.05158008 0.02747666 0.03248437 0.02109469 0.01764180 0.01463882 0.00718395 0.00841551 0.00240606 0.00426407 0.00116783 0.00270237 0.00035054 0.00128154 0.00005746 0.00043355 0.00002852 -0.00029509 0.00033344 -0.00097346 0.00094593 -0.00168768 0.00230626 -0.00280280 0.00414045 -0.00397511 0.00616717 -0.00507777 0.01685431 -0.00897050 0.03248253 -0.01239559 0.05302498 -0.01515289 0.07843283 -0.01719338 0.10854412 -0.01853642 0.14314411 -0.01923278 0.18192732 -0.01938797 0.22450229 -0.01911882 0.27038279 -0.01855180 0.31901963 -0.01777703 0.36980328 -0.01686904 0.42212370 -0.01583655 0.47537514 -0.01471928 0.52894156 -0.01353240 0.58220369 -0.01231682 0.63454507 -0.01108285 0.68535966 -0.00986547 0.73405747 -0.00866901 0.78007210 -0.00752067 0.82286580 -0.00641773 0.86193649 -0.00537779 0.89682206 -0.00438763 0.92710650 -0.00345133 0.95242177 -0.00251062 0.97258094 -0.00151225 0.98749078 -0.00062085 0.99680701 -0.00012484 1.00000000 0.00000000 |
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Polars for MH 22 7.2% (mh22-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh22-il | 50,000 | 9 | 33.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh22-il | 50,000 | 5 | 35 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh22-il | 100,000 | 9 | 48.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh22-il | 100,000 | 5 | 47.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh22-il | 200,000 | 9 | 63.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh22-il | 200,000 | 5 | 60.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh22-il | 500,000 | 9 | 82.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh22-il | 500,000 | 5 | 74.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh22-il | 1,000,000 | 9 | 92.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh22-il | 1,000,000 | 5 | 81.9 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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