Elevator Stick Force given Hinge Moment Coefficient evaluator uses Stick Force = Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord*Elevator Area to evaluate the Stick Force, Elevator Stick Force given Hinge Moment Coefficient is a calculation that determines the stick force required to control an elevator's longitudinal motion, taking into account the gearing ratio, hinge moment coefficient, density, velocity, chord, and area of the elevator, this formula is essential in aircraft design to ensure proper control and stability of the elevator, a critical flight control surface. Stick Force is denoted by 𝙁 symbol.
How to evaluate Elevator Stick Force given Hinge Moment Coefficient using this online evaluator? To use this online evaluator for Elevator Stick Force given Hinge Moment Coefficient, enter Gearing Ratio (𝑮), Hinge Moment Coefficient (Che), Density (ρ), Flight Velocity (V), Elevator Chord (ce) & Elevator Area (Se) and hit the calculate button.