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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=𝑮𝑯𝒆
𝙁 - Stick Force?𝑮 - Gearing Ratio?𝑯𝒆 - Hinge Moment?

Elevator Stick Force given Gearing Ratio Example

With values
With units
Only example

Here is how the Elevator Stick Force given Gearing Ratio equation looks like with Values.

Here is how the Elevator Stick Force given Gearing Ratio equation looks like with Units.

Here is how the Elevator Stick Force given Gearing Ratio equation looks like.

23.2558Edit=0.9302Edit25Edit
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Elevator Stick Force given Gearing Ratio Solution

Follow our step by step solution on how to calculate Elevator Stick Force given Gearing Ratio?

FIRST Step Consider the formula
𝙁=𝑮𝑯𝒆
Next Step Substitute values of Variables
𝙁=0.9302m⁻¹25N*m
Next Step Prepare to Evaluate
𝙁=0.930225
Next Step Evaluate
𝙁=23.255825N
LAST Step Rounding Answer
𝙁=23.2558N

Elevator Stick Force given Gearing Ratio 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
Hinge Moment is the moment acting on a control surface that the pilot must overcome by exerting a force on the control stick.
Symbol: 𝑯𝒆
Measurement: Moment of ForceUnit: N*m
Note: Value can be positive or negative.

Other Formulas to find Stick Force

​Go Elevator Stick Force
𝙁=δe𝑯𝒆𝒍sδs
​Go Elevator Stick Force given Hinge Moment Coefficient
𝙁=𝑮Che0.5ρV2ceSe

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
​Go Flight Velocity given Elevator Hinge Moment Coefficient
V=𝑯𝒆Che0.5ρSece
​Go Elevator Area given Hinge Moment Coefficient
Se=𝑯𝒆Che0.5ρV2ce

How to Evaluate Elevator Stick Force given Gearing Ratio?

Elevator Stick Force given Gearing Ratio evaluator uses Stick Force = Gearing Ratio*Hinge Moment to evaluate the Stick Force, Elevator Stick Force given Gearing Ratio is the calculation of the longitudinal control stick force required in an aircraft, which is directly proportional to the gearing ratio and hinge moment, thus providing a critical safety parameter for pilots and aircraft designers. Stick Force is denoted by 𝙁 symbol.

How to evaluate Elevator Stick Force given Gearing Ratio using this online evaluator? To use this online evaluator for Elevator Stick Force given Gearing Ratio, enter Gearing Ratio (𝑮) & Hinge Moment (𝑯𝒆) and hit the calculate button.

FAQs on Elevator Stick Force given Gearing Ratio

What is the formula to find Elevator Stick Force given Gearing Ratio?
The formula of Elevator Stick Force given Gearing Ratio is expressed as Stick Force = Gearing Ratio*Hinge Moment. Here is an example- 23.25 = 0.930233*25.
How to calculate Elevator Stick Force given Gearing Ratio?
With Gearing Ratio (𝑮) & Hinge Moment (𝑯𝒆) we can find Elevator Stick Force given Gearing Ratio using the formula - Stick Force = Gearing Ratio*Hinge Moment.
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 Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord*Elevator AreaOpenImg
Can the Elevator Stick Force given Gearing Ratio be negative?
No, the Elevator Stick Force given Gearing Ratio, measured in Force cannot be negative.
Which unit is used to measure Elevator Stick Force given Gearing Ratio?
Elevator Stick Force given Gearing Ratio 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 Gearing Ratio can be measured.
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