MH 150 23.89% (mh150-il)
MH 150 23.89% - Martin Hepperle MH 150 for marine ruddershaft for torque reduction (schottel units)
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(mh150-il) MH 150 23.89% Martin Hepperle MH 150 for marine ruddershaft for torque reduction (schottel units) Max thickness 23.9% at 27.2% chord. Max camber 4.5% at 53.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 150 23.89% 1.00000000 0.00000000 0.99644661 0.00099198 0.98599750 0.00409490 0.96919242 0.00942886 0.94670696 0.01689974 0.91915510 0.02622435 0.88703099 0.03712173 0.85089668 0.04939594 0.81142869 0.06276083 0.76928235 0.07682294 0.72506308 0.09114541 0.67932580 0.10528216 0.63257730 0.11879834 0.58528450 0.13129209 0.53787982 0.14239887 0.49077061 0.15180601 0.44434332 0.15924285 0.39897129 0.16449405 0.35501813 0.16734612 0.31274016 0.16762568 0.27238346 0.16528234 0.23416603 0.16024476 0.19813583 0.15257967 0.16441463 0.14257680 0.13321631 0.13055358 0.10481236 0.11685630 0.07949044 0.10173431 0.05736685 0.08545489 0.03854929 0.06845572 0.02322394 0.05120440 0.01157876 0.03416415 0.00379429 0.01785014 0.00012154 0.00290344 0.00156398 -0.00964253 0.00918651 -0.02076836 0.02246564 -0.03188553 0.04038338 -0.04249500 0.06256588 -0.05214096 0.08876585 -0.06049132 0.11875450 -0.06726544 0.15230453 -0.07229694 0.18900801 -0.07538481 0.22866140 -0.07607565 0.27145039 -0.07427146 0.31728187 -0.07034009 0.36573599 -0.06458021 0.41638790 -0.05720001 0.46880754 -0.04845179 0.52255163 -0.03861444 0.57716775 -0.02803728 0.63218341 -0.01712206 0.68710592 -0.00637451 0.74139893 0.00361595 0.79446277 0.01207326 0.84557085 0.01800397 0.89335489 0.01969716 0.93425795 0.01623426 0.96489875 0.01003023 0.98511740 0.00444081 0.99638742 0.00105567 1.00000000 0.00000000 |
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Polars for MH 150 23.89% (mh150-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh150-il | 50,000 | 9 | 3.9 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh150-il | 50,000 | 5 | 7.8 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh150-il | 100,000 | 9 | 14.2 at α=0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh150-il | 100,000 | 5 | 38.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh150-il | 200,000 | 9 | 56.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh150-il | 200,000 | 5 | 61.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh150-il | 500,000 | 9 | 90.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh150-il | 500,000 | 5 | 88.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh150-il | 1,000,000 | 9 | 117.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh150-il | 1,000,000 | 5 | 112.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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