FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Elevator Chord Length given Stick Force Formula

GoElevator Chord Length given Hinge Moment Coefficient Formula

Fx Copy

LaTeX Copy

Elevator Chord is the chord length of an elevator measured from its hinge line to trailing edge. Check FAQs

c e = \frac{𝙁}{𝑮 \cdot Ch e \cdot 0.5 \cdot ρ \cdot V^{2} \cdot S e}

c_e - Elevator Chord?𝙁 - Stick Force?𝑮 - Gearing Ratio?Ch_e - Hinge Moment Coefficient?ρ - Density?V - Flight Velocity?S_e - Elevator Area?

Elevator Chord Length given Stick Force Example

With values

With units

Only example

Here is how the Elevator Chord Length given Stick Force equation looks like with Values.

Here is how the Elevator Chord Length given Stick Force equation looks like with Units.

Here is how the Elevator Chord Length given Stick Force equation looks like.

0.5997 = \frac{23.2558}{0.9302 \cdot 0.7704 \cdot 0.5 \cdot 1.225 \cdot 60^{2} \cdot 0.0245}

0.5997m = \frac{23.2558N}{0.9302m⁻¹ \cdot 0.7704 \cdot 0.5 \cdot 1.225kg/m³ \cdot {60m/s}^{2} \cdot 0.0245m²}

0.5997 = \frac{23.2558}{0.9302 \cdot 0.7704 \cdot 0.5 \cdot 1.225 \cdot 60^{2} \cdot 0.0245}

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Aerospace » Category

Aircraft Mechanics » fx Elevator Chord Length given Stick Force

Elevator Chord Length given Stick Force Solution

Follow our step by step solution on how to calculate Elevator Chord Length given Stick Force?

FIRST Step Consider the formula

c e = \frac{𝙁}{𝑮 \cdot Ch e \cdot 0.5 \cdot ρ \cdot V^{2} \cdot S e}

Next Step Substitute values of Variables

∴

c e = \frac{23.2558N}{0.9302m⁻¹ \cdot 0.7704 \cdot 0.5 \cdot 1.225kg/m³ \cdot {60m/s}^{2} \cdot 0.0245m²}

Next Step Prepare to Evaluate

∴

c e = \frac{23.2558}{0.9302 \cdot 0.7704 \cdot 0.5 \cdot 1.225 \cdot 60^{2} \cdot 0.0245}

Next Step Evaluate

∴

c e = 0.599741331316541m

LAST Step Rounding Answer

∴

c e = 0.5997m

Elevator Chord Length given Stick Force Formula Elements

Variables

Elevator Chord

Elevator Chord is the chord length of an elevator measured from its hinge line to trailing edge.

Symbol: c_e

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Elevator Chord

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.

Formulas to find Stick Force

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.

Formulas to find Gearing Ratio

Hinge Moment Coefficient

Hinge Moment Coefficient is the coefficient associated with the hinge moment of the control surface of an aircraft.

Symbol: Ch_e

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Hinge Moment Coefficient

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.

Formulas to find Density

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.

Formulas to find Flight Velocity

Elevator Area

The Elevator Area is the area of the control surface responsible for providing pitching motion to an aircraft.

Symbol: S_e

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Elevator Area

Other Formulas to find Elevator Chord

Go Elevator Chord Length given Hinge Moment Coefficient

c e = \frac{𝑯 𝒆}{Ch e \cdot 0.5 \cdot ρ \cdot V^{2} \cdot S e}

Other formulas in Stick Forces and Hinge Moments category

Go Elevator Hinge moment coefficient

Ch e = \frac{𝑯 𝒆}{0.5 \cdot ρ \cdot V^{2} \cdot S e \cdot c e}

Go Elevator Hinge Moment given Hinge Moment Coefficient

𝑯 𝒆 = Ch e \cdot 0.5 \cdot ρ \cdot V^{2} \cdot S e \cdot c e

How to Evaluate Elevator Chord Length given Stick Force?

Elevator Chord Length given Stick Force evaluator uses Elevator Chord = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area) to evaluate the Elevator Chord, Elevator Chord Length given Stick Force is a measure of the length of an elevator chord in an aircraft, calculated by considering the stick force, gearing ratio, hinge moment coefficient, air density, velocity and elevator area, providing a critical parameter for aircraft design and stability analysis. Elevator Chord is denoted by c_e symbol.

How to evaluate Elevator Chord Length given Stick Force using this online evaluator? To use this online evaluator for Elevator Chord Length given Stick Force, enter Stick Force (𝙁), Gearing Ratio (𝑮), Hinge Moment Coefficient (Ch_e), Density (ρ), Flight Velocity (V) & Elevator Area (S_e) and hit the calculate button.

FAQs on Elevator Chord Length given Stick Force

What is the formula to find Elevator Chord Length given Stick Force?

The formula of Elevator Chord Length given Stick Force is expressed as Elevator Chord = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area). Here is an example- 0.60002 = 23.25581/(0.930233*0.770358*0.5*1.225*60^2*0.02454).

How to calculate Elevator Chord Length given Stick Force?

With Stick Force (𝙁), Gearing Ratio (𝑮), Hinge Moment Coefficient (Ch_e), Density (ρ), Flight Velocity (V) & Elevator Area (S_e) we can find Elevator Chord Length given Stick Force using the formula - Elevator Chord = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area).

What are the other ways to Calculate Elevator Chord?

Here are the different ways to Calculate Elevator Chord-

Elevator Chord=Hinge Moment/(Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area)

Can the Elevator Chord Length given Stick Force be negative?

No, the Elevator Chord Length given Stick Force, measured in Length cannot be negative.

Which unit is used to measure Elevator Chord Length given Stick Force?

Elevator Chord Length given Stick Force is usually measured using the Meter[m] for Length. Millimeter[m], Kilometer[m], Decimeter[m] are the few other units in which Elevator Chord Length given Stick Force can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Elevator Chord Length given Stick Force Formula

​GoElevator Chord Length given Hinge Moment Coefficient Formula

Elevator Chord Length given Stick Force Example

Elevator Chord Length given Stick Force Solution

Elevator Chord Length given Stick Force Formula Elements

Other Formulas to find Elevator Chord

Other formulas in Stick Forces and Hinge Moments category

How to Evaluate Elevator Chord Length given Stick Force?

FAQs on Elevator Chord Length given Stick Force

Variable Name

GoElevator Chord Length given Hinge Moment Coefficient Formula