Aerodynamics and hydrodynamics profiles performances database proposed by FYN.
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Best CL/CD = NaN at °
Lifting point at CL/CD max: %
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Speed
m/s
Wing length
m
Chord width
m
Attack angle
º
Fluid
Temperature
If you change a value, click calculate to update performances.
Performances
2D performances of infinite wing length: the 3D effects of the tip losses vertices are not includes in this free school tool. Lift losses could reach 60% for small length/width ratios. Use Heliciel software to include tip losses and compute 3D prototype for wings, foils, fins, turbines, propellers projects.