MH 108 11.98% (mh108-il)
MH 108 11.98% - Martin Hepperle MH 108 for stall controlled wind turbines
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(mh108-il) MH 108 11.98% Martin Hepperle MH 108 for stall controlled wind turbines Max thickness 11.9% at 22.8% chord. Max camber 1% at 22.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 108 11.98% 1.00000000 0.00000000 0.99643033 0.00010286 0.98603763 0.00066669 0.96947896 0.00192106 0.94720078 0.00365936 0.91935509 0.00579598 0.88623754 0.00850390 0.84838241 0.01189976 0.80638582 0.01600336 0.76089491 0.02078583 0.71259079 0.02616460 0.66217346 0.03201092 0.61034600 0.03815523 0.55780031 0.04439373 0.50520434 0.05049864 0.45319097 0.05622665 0.40234976 0.06132989 0.35322031 0.06556690 0.30628931 0.06870603 0.26198966 0.07055264 0.22076101 0.07087754 0.18280706 0.06932533 0.14799337 0.06584228 0.11636066 0.06076102 0.08817487 0.05435476 0.06365534 0.04681824 0.04296243 0.03836070 0.02617902 0.02924957 0.01338734 0.01987044 0.00471080 0.01069468 0.00213785 0.00668444 0.00097387 0.00421472 0.00024125 0.00189559 0.00001521 0.00045547 0.00005978 -0.00086338 0.00043863 -0.00214136 0.00112303 -0.00347361 0.00259625 -0.00554510 0.00455379 -0.00768327 0.00918245 -0.01162830 0.02136259 -0.01892355 0.03811696 -0.02578767 0.05940336 -0.03194090 0.08512326 -0.03723697 0.11512209 -0.04157934 0.14919903 -0.04492245 0.18709655 -0.04726839 0.22848557 -0.04866214 0.27296544 -0.04915622 0.32009677 -0.04880995 0.36940148 -0.04770014 0.42036942 -0.04591650 0.47246265 -0.04358113 0.52506272 -0.04083367 0.57751487 -0.03773249 0.62923986 -0.03431645 0.67967031 -0.03068146 0.72821823 -0.02692405 0.77431230 -0.02312859 0.81740436 -0.01937698 0.85697399 -0.01574752 0.89253305 -0.01231192 0.92362931 -0.00913872 0.94984553 -0.00626002 0.97090521 -0.00369000 0.98661374 -0.00162560 0.99655052 -0.00038512 1.00000000 0.00000000 |
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Polars for MH 108 11.98% (mh108-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh108-il | 50,000 | 9 | 16.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh108-il | 50,000 | 5 | 25.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh108-il | 100,000 | 9 | 36.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh108-il | 100,000 | 5 | 42.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh108-il | 200,000 | 9 | 56.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh108-il | 200,000 | 5 | 58.5 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh108-il | 500,000 | 9 | 82.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh108-il | 500,000 | 5 | 79.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh108-il | 1,000,000 | 9 | 102 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh108-il | 1,000,000 | 5 | 93.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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