MB253515 15.0% smoothed (mb253515sm-il)
MB253515 15.0% smoothed - Mike Bame MB253515 low Reynolds number airfoil
| Details | Dat file | Parser | |
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(mb253515sm-il) MB253515 15.0% smoothed Mike Bame MB253515 low Reynolds number airfoil Max thickness 15% at 35% chord. Max camber 2.5% at 37.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MB253515 15.0% smoothed 1.00000 0.0 0.95000 0.01032 0.90000 0.02033 0.85000 0.03052 0.80000 0.04079 0.75000 0.05095 0.70000 0.06078 0.65000 0.07005 0.60000 0.07849 0.55000 0.08582 0.50000 0.09174 0.45000 0.09602 0.42500 0.09748 0.40000 0.09847 0.37500 0.09898 0.35000 0.09904 0.32500 0.09868 0.30000 0.09788 0.27500 0.09660 0.25000 0.09473 0.22500 0.09211 0.20000 0.08861 0.17500 0.08410 0.15000 0.07844 0.12500 0.07146 0.10000 0.06296 0.08750 0.05807 0.07500 0.05274 0.06250 0.04696 0.05000 0.04072 0.03750 0.03393 0.02500 0.02636 0.01000 0.01521 0.0 -0.00041 0.01000 -0.01223 0.02500 -0.01809 0.03750 -0.02159 0.05000 -0.02461 0.06250 -0.02739 0.07500 -0.03001 0.08750 -0.03246 0.10000 -0.03472 0.12500 -0.03861 0.15000 -0.04175 0.17500 -0.04425 0.20000 -0.04622 0.22500 -0.04776 0.25000 -0.04892 0.27500 -0.04974 0.30000 -0.05026 0.32500 -0.05052 0.35000 -0.05054 0.37500 -0.05035 0.40000 -0.04997 0.42500 -0.04941 0.45000 -0.04866 0.50000 -0.04660 0.55000 -0.04383 0.60000 -0.04036 0.65000 -0.03628 0.70000 -0.03169 0.75000 -0.02669 0.80000 -0.02144 0.85000 -0.01606 0.90000 -0.01070 0.95000 -0.00544 1.00000 0.0 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
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Polars for MB253515 15.0% smoothed (mb253515sm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mb253515sm-il | 50,000 | 9 | 7.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mb253515sm-il | 50,000 | 5 | 25.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mb253515sm-il | 100,000 | 9 | 48.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mb253515sm-il | 100,000 | 5 | 49 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mb253515sm-il | 200,000 | 9 | 70 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mb253515sm-il | 200,000 | 5 | 68.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mb253515sm-il | 500,000 | 9 | 92.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mb253515sm-il | 500,000 | 5 | 83.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mb253515sm-il | 1,000,000 | 9 | 105.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mb253515sm-il | 1,000,000 | 5 | 96.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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