Eiffel 430 (Lachassgne) (eiffel430-il)
Eiffel 430 (Lachassgne) - Eiffel 430 (Lachassgne) airfoil
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(eiffel430-il) Eiffel 430 (Lachassgne) Eiffel 430 (Lachassgne) airfoil Max thickness 9.7% at 15% chord. Max camber 4.5% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Eiffel 430 (Lachassgne) 1.0000 0.0050 0.9500 0.0169 0.9000 0.0280 0.8000 0.0510 0.7000 0.0700 0.6000 0.0860 0.5000 0.1020 0.4000 0.1100 0.3000 0.1020 0.2000 0.1060 0.1500 0.1017 0.1000 0.0910 0.0750 0.0848 0.0500 0.0757 0.0250 0.0621 0.0125 0.0509 0.0000 0.0270 0.0125 0.0090 0.0250 0.0042 0.0500 0.0014 0.0750 0.0000 0.1000 0.0010 0.1500 0.0048 0.2000 0.0120 0.3000 0.0160 0.4000 0.0160 0.5000 0.0140 0.6000 0.0110 0.7000 0.0060 0.8000 0.0030 0.9000 0.0000 0.9500 0.0014 1.0000 0.0050 |
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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 Eiffel 430 (Lachassgne) (eiffel430-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| eiffel430-il | 50,000 | 9 | 36.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel430-il | 50,000 | 5 | 32.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eiffel430-il | 100,000 | 9 | 47.2 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel430-il | 100,000 | 5 | 43.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eiffel430-il | 200,000 | 9 | 58 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel430-il | 200,000 | 5 | 58.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eiffel430-il | 500,000 | 9 | 84.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel430-il | 500,000 | 5 | 71.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eiffel430-il | 1,000,000 | 9 | 92.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel430-il | 1,000,000 | 5 | 85.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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