MH 102 16.99% (mh102-il)
MH 102 16.99% - Martin Hepperle MH 102 for stall controlled wind turbines (root)
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(mh102-il) MH 102 16.99% Martin Hepperle MH 102 for stall controlled wind turbines (root) Max thickness 17% at 27.7% chord. Max camber 2.8% at 37.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 102 16.99% 1.00000000 0.00000000 0.99614983 0.00063728 0.98520565 0.00282240 0.96830620 0.00663188 0.94602565 0.01147142 0.91839872 0.01707581 0.88572075 0.02361176 0.84861962 0.03110739 0.80774299 0.03943785 0.76375323 0.04841341 0.71730911 0.05779135 0.66905176 0.06728927 0.61959790 0.07661096 0.56953125 0.08544960 0.51940362 0.09351302 0.46973112 0.10052213 0.42099874 0.10622572 0.37366109 0.11040973 0.32820037 0.11284147 0.28491185 0.11316925 0.24380784 0.11130183 0.20506012 0.10746400 0.16901281 0.10181653 0.13594111 0.09447235 0.10608263 0.08559329 0.07964163 0.07536521 0.05678511 0.06401791 0.03764823 0.05182014 0.02233251 0.03908978 0.01090201 0.02621339 0.00343089 0.01372124 0.00081810 0.00624945 0.00020021 0.00293804 0.00000082 -0.00018316 0.00011982 -0.00213265 0.00049708 -0.00393552 0.00120839 -0.00566457 0.00224072 -0.00741951 0.00426419 -0.01009532 0.00680138 -0.01281177 0.01050141 -0.01613427 0.02399365 -0.02525514 0.04201295 -0.03405036 0.06417737 -0.04212709 0.09020108 -0.04904123 0.11995663 -0.05434164 0.15349856 -0.05770634 0.19094712 -0.05910127 0.23224820 -0.05877018 0.27709212 -0.05700227 0.32507665 -0.05405209 0.37570590 -0.05021288 0.42839057 -0.04576400 0.48243404 -0.04098262 0.53707390 -0.03601968 0.59162389 -0.03098315 0.64540959 -0.02601644 0.69772762 -0.02126360 0.74788348 -0.01683072 0.79520092 -0.01281888 0.83902670 -0.00929883 0.87873741 -0.00633322 0.91374386 -0.00395207 0.94349459 -0.00217278 0.96747412 -0.00097467 0.98520055 -0.00030404 0.99622182 -0.00005550 1.00000000 0.00000000 |
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Polars for MH 102 16.99% (mh102-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh102-il | 50,000 | 9 | 5.5 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh102-il | 50,000 | 5 | 23.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh102-il | 100,000 | 9 | 37.8 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh102-il | 100,000 | 5 | 45.8 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh102-il | 200,000 | 9 | 63.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh102-il | 200,000 | 5 | 65.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh102-il | 500,000 | 9 | 94.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh102-il | 500,000 | 5 | 91 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh102-il | 1,000,000 | 9 | 118.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh102-il | 1,000,000 | 5 | 110.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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