MH 26 10.99% (mh26-il)
MH 26 10.99% - Martin Hepperle MH 26 for F3D Pylon Racing (extended laminar flow)
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(mh26-il) MH 26 10.99% Martin Hepperle MH 26 for F3D Pylon Racing (extended laminar flow) Max thickness 11% at 42.3% chord. Max camber 1.4% at 42.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 26 10.99% 1.00000000 0.00000000 0.99601781 0.00046831 0.98473175 0.00248610 0.96741634 0.00651912 0.94515820 0.01227929 0.91873452 0.01926938 0.88872819 0.02691697 0.85561228 0.03455836 0.81944363 0.04146234 0.78000170 0.04745488 0.73748441 0.05275405 0.69240304 0.05741421 0.64522702 0.06138663 0.59647521 0.06467396 0.54669436 0.06722025 0.49642217 0.06899243 0.44619893 0.06994448 0.39656117 0.07005849 0.34803353 0.06930017 0.30111871 0.06766885 0.25630079 0.06515540 0.21403239 0.06177982 0.17473071 0.05755263 0.13875834 0.05252349 0.10644453 0.04675219 0.07806222 0.04033465 0.05384673 0.03338246 0.03396206 0.02605438 0.01854895 0.01855724 0.00768316 0.01117645 0.00187433 0.00493409 0.00081881 0.00301619 0.00018015 0.00124527 0.00000397 0.00017301 0.00008904 -0.00076520 0.00051730 -0.00163957 0.00127385 -0.00254651 0.00288623 -0.00395604 0.00501517 -0.00542464 0.01687170 -0.01082804 0.03318330 -0.01565441 0.05452977 -0.02012518 0.08074741 -0.02415094 0.11160822 -0.02771464 0.14679334 -0.03084557 0.18587433 -0.03355543 0.22839759 -0.03581251 0.27386950 -0.03759285 0.32180470 -0.03883850 0.37171646 -0.03956364 0.42306202 -0.03979884 0.47524771 -0.03958505 0.52767311 -0.03892214 0.57973433 -0.03783462 0.63083169 -0.03631376 0.68037516 -0.03437271 0.72780057 -0.03197813 0.77257463 -0.02913554 0.81416230 -0.02571283 0.85240703 -0.02152702 0.88731280 -0.01691915 0.91838421 -0.01235216 0.94522412 -0.00793007 0.96763381 -0.00409126 0.98495940 -0.00145091 0.99611690 -0.00024070 1.00000000 0.00000000 |
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Polars for MH 26 10.99% (mh26-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh26-il | 50,000 | 9 | 34.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 50,000 | 5 | 32 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 100,000 | 9 | 51.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 100,000 | 5 | 47.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 200,000 | 9 | 71.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 200,000 | 5 | 57.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 500,000 | 9 | 77.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 500,000 | 5 | 58.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 1,000,000 | 9 | 74.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 1,000,000 | 5 | 66.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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