Eiffel 10 (Wright) - 1903 Wright Flyer airfoil (eiffel10-il)
Eiffel 10 (Wright) - 1903 Wright Flyer airfoil - Eiffel 10 (Wright) - 1903 Wright Flyer airfoil
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(eiffel10-il) Eiffel 10 (Wright) - 1903 Wright Flyer airfoil Eiffel 10 (Wright) - 1903 Wright Flyer airfoil Max thickness 2.7% at 0% chord. Max camber 6.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Eiffel 10 (Wright) - 1903 Wright Flyer airfoil 1.0000 0.0064 .9500 0.0143 .9000 0.0220 .8000 0.0370 .7000 0.0510 .6000 0.0623 .5000 0.0693 .4000 0.0718 .3000 0.0701 .2000 0.0614 .1500 0.0550 .1000 0.0468 .0750 0.0423 .0500 0.0375 .0250 0.0323 .0125 0.0296 .0000 0.0273 .0000 0.0000 .0125 0.0032 .0250 0.0060 .0500 0.0117 .0750 0.0170 .1000 0.0223 .1500 0.0315 .2000 0.0390 .3000 0.0486 .4000 0.0527 .5000 0.0518 .6000 0.0456 .7000 0.0370 .8000 0.0255 .9000 0.0127 .9500 0.0065 1.0000 0.0000 |
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Polars for Eiffel 10 (Wright) - 1903 Wright Flyer airfoil (eiffel10-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| eiffel10-il | 50,000 | 9 | 25.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel10-il | 50,000 | 5 | 27 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eiffel10-il | 100,000 | 9 | 27.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel10-il | 100,000 | 5 | 29.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eiffel10-il | 200,000 | 9 | 28.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel10-il | 200,000 | 5 | 34.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eiffel10-il | 500,000 | 9 | 32.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel10-il | 500,000 | 5 | 38.4 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eiffel10-il | 1,000,000 | 9 | 36.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eiffel10-il | 1,000,000 | 5 | 45.2 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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