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Stick Force is the force exerted on the control column by the pilot of an airplane in flight. Check FAQs
𝙁=𝑮Che0.5ρV2ceSe
𝙁 - Stick Force?𝑮 - Gearing Ratio?Che - Hinge Moment Coefficient?ρ - Density?V - Flight Velocity?ce - Elevator Chord?Se - Elevator Area?

Elevator Stick Force given Hinge Moment Coefficient Example

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With units
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Here is how the Elevator Stick Force given Hinge Moment Coefficient equation looks like with Values.

Here is how the Elevator Stick Force given Hinge Moment Coefficient equation looks like with Units.

Here is how the Elevator Stick Force given Hinge Moment Coefficient equation looks like.

23.2658Edit=0.9302Edit0.7704Edit0.51.225Edit60Edit20.6Edit0.0245Edit
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Elevator Stick Force given Hinge Moment Coefficient Solution

Follow our step by step solution on how to calculate Elevator Stick Force given Hinge Moment Coefficient?

FIRST Step Consider the formula
𝙁=𝑮Che0.5ρV2ceSe
Next Step Substitute values of Variables
𝙁=0.9302m⁻¹0.77040.51.225kg/m³60m/s20.6m0.0245
Next Step Prepare to Evaluate
𝙁=0.93020.77040.51.2256020.60.0245
Next Step Evaluate
𝙁=23.265840240441N
LAST Step Rounding Answer
𝙁=23.2658N

Elevator Stick Force given Hinge Moment Coefficient Formula Elements

Variables
Stick Force
Stick Force is the force exerted on the control column by the pilot of an airplane in flight.
Symbol: 𝙁
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Gearing Ratio
Gearing Ratio is a measure of the mechanical advantage provided by the control system of an aircraft.
Symbol: 𝑮
Measurement: Reciprocal LengthUnit: m⁻¹
Note: Value should be greater than 0.
Hinge Moment Coefficient
Hinge Moment Coefficient is the coefficient associated with the hinge moment of the control surface of an aircraft.
Symbol: Che
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Density
Density of flow refers to the mass per unit volume of a fluid through which aircraft is moving.
Symbol: ρ
Measurement: DensityUnit: kg/m³
Note: Value should be greater than 0.
Flight Velocity
Flight Velocity refers to the speed at which an aircraft moves through the air.
Symbol: V
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Elevator Chord
Elevator Chord is the chord length of an elevator measured from its hinge line to trailing edge.
Symbol: ce
Measurement: LengthUnit: m
Note: Value should be greater than 0.
Elevator Area
The Elevator Area is the area of the control surface responsible for providing pitching motion to an aircraft.
Symbol: Se
Measurement: AreaUnit:
Note: Value should be greater than 0.

Other Formulas to find Stick Force

​Go Elevator Stick Force
𝙁=δe𝑯𝒆𝒍sδs
​Go Elevator Stick Force given Gearing Ratio
𝙁=𝑮𝑯𝒆

Other formulas in Stick Forces and Hinge Moments category

​Go Elevator Hinge moment coefficient
Che=𝑯𝒆0.5ρV2Sece
​Go Elevator Hinge Moment given Hinge Moment Coefficient
𝑯𝒆=Che0.5ρV2Sece

How to Evaluate Elevator Stick Force given Hinge Moment Coefficient?

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.

FAQs on Elevator Stick Force given Hinge Moment Coefficient

What is the formula to find Elevator Stick Force given Hinge Moment Coefficient?
The formula of Elevator Stick Force given Hinge Moment Coefficient is expressed as Stick Force = Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord*Elevator Area. Here is an example- 23.25503 = 0.930233*0.770358*0.5*1.225*60^2*0.6*0.02454.
How to calculate Elevator Stick Force given Hinge Moment Coefficient?
With Gearing Ratio (𝑮), Hinge Moment Coefficient (Che), Density (ρ), Flight Velocity (V), Elevator Chord (ce) & Elevator Area (Se) we can find Elevator Stick Force given Hinge Moment Coefficient using the formula - Stick Force = Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord*Elevator Area.
What are the other ways to Calculate Stick Force?
Here are the different ways to Calculate Stick Force-
  • Stick Force=Elevator Deflection Angle*Hinge Moment/(Stick Length*Stick Deflection Angle)OpenImg
  • Stick Force=Gearing Ratio*Hinge MomentOpenImg
Can the Elevator Stick Force given Hinge Moment Coefficient be negative?
No, the Elevator Stick Force given Hinge Moment Coefficient, measured in Force cannot be negative.
Which unit is used to measure Elevator Stick Force given Hinge Moment Coefficient?
Elevator Stick Force given Hinge Moment Coefficient is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Elevator Stick Force given Hinge Moment Coefficient can be measured.
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