How to Calculate Taper Ratio of Airfoil?
Taper Ratio of Airfoil calculator uses Taper_ratio = Tip_chordlength/Root_chordlength to calculate the Taper_ratio, Taper Ratio of Airfoil is defined as ratio of the tip chord to the root chord. Taper_ratio is denoted by λ symbol.
How to calculate Taper Ratio of Airfoil using this online calculator? To use this online calculator for Taper Ratio of Airfoil, enter Tip_chordlength (C_{tip}) & Root_chordlength (C_{root}) and hit the calculate button. Here is how the Taper Ratio of Airfoil calculation can be explained with given input values -> 0.285714 = 2/7.