Rhode St. Genese 32 (rhodesg32-il)
Rhode St. Genese 32 - Rhode St. Genese 32 airfoil
| Details | Dat file | Parser | |
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(rhodesg32-il) Rhode St. Genese 32 Rhode St. Genese 32 airfoil Max thickness 11.9% at 30% chord. Max camber 3.9% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Rhode St. Genese 32 1.0000 0.0000 0.9500 0.0128 0.9000 0.0248 0.8000 0.0495 0.7000 0.0715 0.6000 0.0898 0.5000 0.1045 0.4000 0.1137 0.3000 0.1190 0.2000 0.1178 0.1500 0.1085 0.1000 0.0962 0.0750 0.0880 0.0500 0.0762 0.0250 0.0623 0.0125 0.0525 0.0000 0.0293 0.0125 0.0130 0.0250 0.0072 0.0500 0.0037 0.0750 0.0019 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 32 (rhodesg32-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| rhodesg32-il | 50,000 | 9 | 24.3 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg32-il | 50,000 | 5 | 33.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rhodesg32-il | 100,000 | 9 | 45.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg32-il | 100,000 | 5 | 48.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rhodesg32-il | 200,000 | 9 | 64.3 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg32-il | 200,000 | 5 | 64.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rhodesg32-il | 500,000 | 9 | 92.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg32-il | 500,000 | 5 | 89.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rhodesg32-il | 1,000,000 | 9 | 115 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rhodesg32-il | 1,000,000 | 5 | 108 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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