MH 106 13.07% (mh106-il)
MH 106 13.07% - Martin Hepperle MH 106 for stall controlled wind turbines
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(mh106-il) MH 106 13.07% Martin Hepperle MH 106 for stall controlled wind turbines Max thickness 13.1% at 27.4% chord. Max camber 0.9% at 27.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 106 13.07% 1.00000000 0.00000000 0.99633896 0.00013538 0.98572712 0.00081905 0.96892525 0.00231554 0.94642367 0.00436480 0.91836006 0.00685652 0.88503080 0.00997739 0.84699594 0.01384794 0.80487420 0.01847791 0.75933341 0.02382341 0.71107117 0.02978175 0.66080012 0.03620038 0.60923092 0.04288363 0.55705830 0.04960002 0.50494863 0.05609305 0.45352913 0.06209195 0.40338113 0.06731599 0.35503575 0.07151328 0.30907144 0.07437120 0.26580358 0.07534795 0.22506456 0.07420479 0.18681819 0.07124411 0.15136966 0.06678403 0.11904212 0.06102631 0.09013672 0.05417502 0.06493704 0.04641532 0.04366599 0.03792242 0.02646761 0.02891578 0.01345480 0.01968641 0.00469764 0.01063397 0.00188777 0.00623331 0.00081003 0.00381469 0.00016743 0.00154754 0.00000165 0.00014605 0.00010756 -0.00112503 0.00055967 -0.00234500 0.00133663 -0.00361403 0.00297835 -0.00558815 0.00513535 -0.00763363 0.00962388 -0.01106732 0.02257288 -0.01833048 0.04024689 -0.02560254 0.06232892 -0.03260747 0.08853194 -0.03907257 0.11858805 -0.04471630 0.15229113 -0.04928617 0.18946321 -0.05259526 0.22996674 -0.05458014 0.27356298 -0.05533977 0.31988227 -0.05499133 0.36851477 -0.05367172 0.41896127 -0.05156813 0.47063693 -0.04884164 0.52291335 -0.04562226 0.57515779 -0.04198170 0.62679552 -0.03799545 0.67724636 -0.03378661 0.72590864 -0.02947190 0.77219558 -0.02515173 0.81554287 -0.02092181 0.85541258 -0.01687058 0.89129875 -0.01307891 0.92273025 -0.00962032 0.94927172 -0.00653679 0.97060783 -0.00384979 0.98649788 -0.00172690 0.99652470 -0.00043016 1.00000000 0.00000000 |
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Polars for MH 106 13.07% (mh106-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh106-il | 50,000 | 9 | 14.9 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 50,000 | 5 | 27.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 100,000 | 9 | 42.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 100,000 | 5 | 44.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 200,000 | 9 | 61.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 200,000 | 5 | 60.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 500,000 | 9 | 86.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 500,000 | 5 | 79.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 1,000,000 | 9 | 103.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 1,000,000 | 5 | 87.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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