Gearing Ratio given Hinge Moment Coefficient evaluator uses Gearing Ratio = Stick Force/(Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area*Elevator Chord) to evaluate the Gearing Ratio, Gearing Ratio given Hinge Moment Coefficient is a dimensionless quantity that relates the stick force required to control the longitudinal axis of an aircraft to the hinge moment coefficient, air density, velocity, and geometric characteristics of the elevator, providing a critical parameter for aircraft designers and pilots to ensure stable and controlled flight operations. Gearing Ratio is denoted by 𝑮 symbol.
How to evaluate Gearing Ratio given Hinge Moment Coefficient using this online evaluator? To use this online evaluator for Gearing Ratio given Hinge Moment Coefficient, enter Stick Force (𝙁), Hinge Moment Coefficient (Che), Density (ρ), Flight Velocity (V), Elevator Area (Se) & Elevator Chord (ce) and hit the calculate button.