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Aircraft Mechanics
Hinge Moment Coefficient in Longitudinal Control Formulas
Hinge Moment Coefficient is the coefficient associated with the hinge moment of the control surface of an aircraft. And is denoted by Ch
e
.
Formulas to find Hinge Moment Coefficient in Longitudinal Control
f
x
Elevator Hinge moment coefficient
Go
f
x
Hinge Moment Coefficient given Stick Force
Go
Longitudinal Control formulas that make use of Hinge Moment Coefficient
f
x
Elevator Hinge Moment given Hinge Moment Coefficient
Go
f
x
Flight Velocity given Elevator Hinge Moment Coefficient
Go
f
x
Elevator Area given Hinge Moment Coefficient
Go
f
x
Elevator Chord Length given Hinge Moment Coefficient
Go
f
x
Gearing Ratio given Hinge Moment Coefficient
Go
f
x
Elevator Stick Force given Hinge Moment Coefficient
Go
f
x
Flight Velocity for given Stick Force
Go
f
x
Elevator Area given Stick Force
Go
f
x
Elevator Chord Length given Stick Force
Go
List of variables in Longitudinal Control formulas
f
x
Hinge Moment
Go
f
x
Density
Go
f
x
Flight Velocity
Go
f
x
Elevator Area
Go
f
x
Elevator Chord
Go
f
x
Stick Force
Go
f
x
Gearing Ratio
Go
FAQ
What is the Hinge Moment Coefficient?
Hinge Moment Coefficient is the coefficient associated with the hinge moment of the control surface of an aircraft.
Can the Hinge Moment Coefficient be negative?
{YesorNo}, the Hinge Moment Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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