MH 27 11.99% (mh27-il)
MH 27 11.99% - Martin Hepperle MH 27 for F3D Pylon Racing (extended laminar flow)
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(mh27-il) MH 27 11.99% Martin Hepperle MH 27 for F3D Pylon Racing (extended laminar flow) Max thickness 12% at 42.4% chord. Max camber 1.4% at 42.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 27 11.99% 1.00000000 0.00000000 0.99571520 0.00058599 0.98395553 0.00317054 0.96643186 0.00805747 0.94421230 0.01463593 0.91796571 0.02233068 0.88818558 0.03054279 0.85529895 0.03863330 0.81933175 0.04589121 0.78006805 0.05217030 0.73770911 0.05769095 0.69276997 0.06251127 0.64571814 0.06657998 0.59707351 0.06990379 0.54738051 0.07242470 0.49717719 0.07411522 0.44700220 0.07492857 0.39739254 0.07485367 0.34887198 0.07385693 0.30194424 0.07194567 0.25709348 0.06911284 0.21477403 0.06538736 0.17540438 0.06078322 0.13935004 0.05535946 0.10694272 0.04918021 0.07845951 0.04235095 0.05413964 0.03498850 0.03415342 0.02726114 0.01864760 0.01938149 0.00770890 0.01164516 0.00190285 0.00517434 0.00082903 0.00316506 0.00018081 0.00130439 0.00000364 0.00017361 0.00009279 -0.00082226 0.00052969 -0.00175607 0.00129790 -0.00272626 0.00293235 -0.00423585 0.00508815 -0.00580795 0.00593836 -0.00635887 0.01719356 -0.01171349 0.03366873 -0.01695866 0.05517405 -0.02187453 0.08153586 -0.02635800 0.11251971 -0.03038274 0.14780184 -0.03396403 0.18695226 -0.03710479 0.22951674 -0.03976194 0.27500196 -0.04190602 0.32292277 -0.04347012 0.37279279 -0.04446501 0.42406984 -0.04491264 0.47616234 -0.04485172 0.52847177 -0.04427557 0.58039711 -0.04320850 0.63134080 -0.04163737 0.68071608 -0.03957671 0.72796029 -0.03699090 0.77254303 -0.03388729 0.81392820 -0.03013320 0.85195686 -0.02554222 0.88662912 -0.02043718 0.91746745 -0.01523863 0.94417642 -0.01001220 0.96669689 -0.00530630 0.98437310 -0.00194796 0.99593329 -0.00033203 1.00000000 0.00000000 |
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Polars for MH 27 11.99% (mh27-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh27-il | 50,000 | 9 | 33.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh27-il | 50,000 | 5 | 30.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh27-il | 100,000 | 9 | 49.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh27-il | 100,000 | 5 | 46.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh27-il | 200,000 | 9 | 69.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh27-il | 200,000 | 5 | 54.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh27-il | 500,000 | 9 | 73.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh27-il | 500,000 | 5 | 54.7 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh27-il | 1,000,000 | 9 | 73.1 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh27-il | 1,000,000 | 5 | 61.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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