MH 30 7.84% (mh30-il)
MH 30 7.84% - Martin Hepperle MH 30 for F3E and F3B
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(mh30-il) MH 30 7.84% Martin Hepperle MH 30 for F3E and F3B Max thickness 7.8% at 31% chord. Max camber 1.7% at 46.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 30 7.84% 1.00000000 0.00000000 0.99675057 0.00027732 0.98718030 0.00121266 0.97167883 0.00297958 0.95067833 0.00561358 0.92464307 0.00906742 0.89405358 0.01322248 0.85940048 0.01792256 0.82117835 0.02296852 0.77988141 0.02813781 0.73595235 0.03316971 0.68977652 0.03788443 0.64176843 0.04216636 0.59237267 0.04596214 0.54210592 0.04925302 0.49155985 0.05198481 0.44127336 0.05402597 0.39172256 0.05532061 0.34342570 0.05583807 0.29687844 0.05551624 0.25249921 0.05432584 0.21073105 0.05230412 0.17200012 0.04942599 0.13663390 0.04569878 0.10492830 0.04116581 0.07712398 0.03590260 0.05342228 0.03000727 0.03394587 0.02362912 0.01880186 0.01697955 0.00802890 0.01034580 0.00203588 0.00459383 0.00093925 0.00287038 0.00024253 0.00128859 0.00001883 0.00033525 0.00004754 -0.00049523 0.00040083 -0.00127039 0.00105881 -0.00207821 0.00248751 -0.00333089 0.00439501 -0.00462627 0.01501806 -0.00913705 0.03016645 -0.01305025 0.05021239 -0.01646349 0.07501814 -0.01926314 0.10439815 -0.02138297 0.13814663 -0.02281137 0.17596671 -0.02359774 0.21749488 -0.02379162 0.26230291 -0.02346665 0.30991182 -0.02268114 0.35980209 -0.02150950 0.41142345 -0.02000860 0.46420152 -0.01825496 0.51754510 -0.01630701 0.57085128 -0.01424565 0.62351129 -0.01213247 0.67491319 -0.01005123 0.72444741 -0.00805782 0.77151953 -0.00622148 0.81555453 -0.00458739 0.85599372 -0.00321371 0.89230202 -0.00211473 0.92398973 -0.00129831 0.95061656 -0.00073427 0.97179803 -0.00038165 0.98723981 -0.00014889 0.99674839 -0.00002635 1.00000000 0.00000000 |
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Polars for MH 30 7.84% (mh30-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh30-il | 50,000 | 9 | 34.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 50,000 | 5 | 35.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh30-il | 100,000 | 9 | 51.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 100,000 | 5 | 48.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh30-il | 200,000 | 9 | 67.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 200,000 | 5 | 59.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh30-il | 500,000 | 9 | 85.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 500,000 | 5 | 73.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh30-il | 1,000,000 | 9 | 95.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 1,000,000 | 5 | 84.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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