MH 24 9.01% (mh24-il)
MH 24 9.01% - Martin Hepperle MH 24 for F3D Pylon Racing (extended laminar flow)
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(mh24-il) MH 24 9.01% Martin Hepperle MH 24 for F3D Pylon Racing (extended laminar flow) Max thickness 9% at 37.3% chord. Max camber 1.2% at 37.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 24 9.01% 1.00000000 0.00000000 0.99653760 0.00038212 0.98634807 0.00161986 0.96996782 0.00405471 0.94809733 0.00783396 0.92150372 0.01284763 0.89093983 0.01878857 0.85708606 0.02507311 0.82017551 0.03093875 0.78003746 0.03611152 0.73686505 0.04077694 0.69117051 0.04497972 0.64343680 0.04866890 0.59419119 0.05183220 0.54398634 0.05440522 0.49335709 0.05634183 0.44284668 0.05759688 0.39299531 0.05814083 0.34433221 0.05793405 0.29736125 0.05695943 0.25256823 0.05519914 0.21040406 0.05265352 0.17128388 0.04932135 0.13556438 0.04523095 0.10356891 0.04042923 0.07556060 0.03498993 0.05176450 0.02901142 0.03232942 0.02263045 0.01738015 0.01604395 0.00697118 0.00951717 0.00187861 0.00446207 0.00083339 0.00274576 0.00019347 0.00116298 0.00000722 0.00020915 0.00007287 -0.00061650 0.00047217 -0.00137861 0.00119252 -0.00216775 0.00273968 -0.00339259 0.00478997 -0.00467544 0.00618978 -0.00544385 0.01737737 -0.00977695 0.03371541 -0.01390389 0.05504475 -0.01763250 0.08123207 -0.02088081 0.11207413 -0.02365199 0.14726809 -0.02600639 0.18638708 -0.02797979 0.22897883 -0.02956258 0.27454898 -0.03075095 0.32260049 -0.03151272 0.37262478 -0.03186577 0.42407057 -0.03183544 0.47634566 -0.03145621 0.52885168 -0.03073089 0.58098576 -0.02968091 0.63215058 -0.02830006 0.68175727 -0.02659806 0.72924518 -0.02454284 0.77408284 -0.02213685 0.81574277 -0.01924851 0.85407585 -0.01570149 0.88909271 -0.01186178 0.92027479 -0.00824741 0.94708314 -0.00500338 0.96914746 -0.00239831 0.98585111 -0.00075472 0.99638531 -0.00011183 1.00000000 0.00000000 |
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Polars for MH 24 9.01% (mh24-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh24-il | 50,000 | 9 | 34.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 50,000 | 5 | 33 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 100,000 | 9 | 50.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 100,000 | 5 | 47 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 200,000 | 9 | 68.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 200,000 | 5 | 59.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 500,000 | 9 | 79.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 500,000 | 5 | 61.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 1,000,000 | 9 | 74.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 1,000,000 | 5 | 70.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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