Taper ratio calculator by K.Prakashbalan

Taper ratio of wing (λ) = ct/cr

ct – Tip chord

cr – Root chord

No SI unit

Taper ratio (λ) is the ratio of the tip chord (ct) to the root chord (cr). Mean aerodynamic chord can be found by integrating the individual section chords across the span.


Effects of Taper Ratio on Aircraft Wing Aerodynamic Parameters: A Comperative Study