Rhode St. Genese 30 (rhodesg30-il)
Rhode St. Genese 30 - Rhode St. Genese 30 airfoil
| Details | Dat file | Parser | |
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(rhodesg30-il) Rhode St. Genese 30 Rhode St. Genese 30 airfoil Max thickness 9.7% at 30% chord. Max camber 3.2% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Rhode St. Genese 30 1.0000 0.0000 0.9500 0.0105 0.9000 0.0203 0.8000 0.0405 0.7000 0.0585 0.6000 0.0735 0.5000 0.0855 0.4000 0.0930 0.3000 0.0974 0.2000 0.0960 0.1500 0.0890 0.1000 0.0787 0.0750 0.0720 0.0500 0.0623 0.0250 0.0510 0.0125 0.0435 0.0000 0.0241 0.0125 0.0145 0.0250 0.0059 0.0500 0.0030 0.0750 0.0015 0.1000 0.0000 0.1500 0.0000 0.2000 0.0000 0.3000 0.0000 0.4000 0.0000 0.5000 0.0000 0.6000 0.0000 0.7000 0.0000 0.8000 0.0000 0.9000 0.0000 0.9500 0.0000 1.0000 0.0000 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for Rhode St. Genese 30 (rhodesg30-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| rhodesg30-il | 50,000 | 9 | 34.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg30-il | 50,000 | 5 | 36.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rhodesg30-il | 100,000 | 9 | 51.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg30-il | 100,000 | 5 | 51.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rhodesg30-il | 200,000 | 9 | 67.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg30-il | 200,000 | 5 | 66.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rhodesg30-il | 500,000 | 9 | 88.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg30-il | 500,000 | 5 | 84.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rhodesg30-il | 1,000,000 | 9 | 105.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg30-il | 1,000,000 | 5 | 85.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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