MH 43 8.5% (mh43-il)
MH 43 8.5% - Martin Hepperle MH 43 for F3B and F3E
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(mh43-il) MH 43 8.5% Martin Hepperle MH 43 for F3B and F3E Max thickness 8.5% at 31.4% chord. Max camber 1.7% at 36.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 43 8.5% 1.00000000 0.00000000 0.99678486 0.00013989 0.98724370 0.00065258 0.97162281 0.00171201 0.95023700 0.00342007 0.92346510 0.00583822 0.89174251 0.00898818 0.85555897 0.01288571 0.81550435 0.01752803 0.77227150 0.02281222 0.72651791 0.02850315 0.67884862 0.03435871 0.62984285 0.04011378 0.58004643 0.04551084 0.52995115 0.05028210 0.47998917 0.05422592 0.43057688 0.05718663 0.38210922 0.05907246 0.33497730 0.05983036 0.28955539 0.05947085 0.24624388 0.05804883 0.20546171 0.05562153 0.16759092 0.05222221 0.13295698 0.04792192 0.10186489 0.04281533 0.07458035 0.03701813 0.05133201 0.03065680 0.03228253 0.02389128 0.01755915 0.01692189 0.00720549 0.01003306 0.00206553 0.00478406 0.00095018 0.00299648 0.00024451 0.00134790 0.00001882 0.00035028 0.00004844 -0.00052433 0.00040489 -0.00134555 0.00106742 -0.00220256 0.00250562 -0.00353268 0.00442405 -0.00490946 0.00581609 -0.00576795 0.01645235 -0.01030331 0.03208388 -0.01453392 0.05252390 -0.01826639 0.07760830 -0.02133674 0.10718942 -0.02360971 0.14115468 -0.02508121 0.17923181 -0.02587934 0.22102264 -0.02609649 0.26606671 -0.02581908 0.31385233 -0.02510132 0.36384620 -0.02399638 0.41550134 -0.02255140 0.46824184 -0.02084175 0.52147066 -0.01892201 0.57457969 -0.01686396 0.62695594 -0.01471056 0.67800878 -0.01251557 0.72717221 -0.01033745 0.77387178 -0.00827242 0.81753239 -0.00638210 0.85760151 -0.00472825 0.89355570 -0.00333449 0.92491661 -0.00221951 0.95125494 -0.00136904 0.97219656 -0.00076049 0.98744902 -0.00032991 0.99681160 -0.00007579 1.00000000 0.00000000 |
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Polars for MH 43 8.5% (mh43-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh43-il | 50,000 | 9 | 33.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 50,000 | 5 | 35.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 100,000 | 9 | 50.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 100,000 | 5 | 49.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 200,000 | 9 | 66.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 200,000 | 5 | 61.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 500,000 | 9 | 86.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 500,000 | 5 | 76.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 1,000,000 | 9 | 100 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 1,000,000 | 5 | 85.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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