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Vertical Tail Side Force for Given Moment Formula

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Vertical Tail Side Force is the side force acting on the vertical tail of an aircraft. Check FAQs

Y v = - (\frac{N v}{𝒍 v})

Y_v - Vertical Tail Side Force?N_v - Vertical Tail Moment?𝒍_v - Vertical Tail Moment Arm?

Vertical Tail Side Force for Given Moment Example

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Here is how the Vertical Tail Side Force for Given Moment equation looks like with Values.

Here is how the Vertical Tail Side Force for Given Moment equation looks like with Units.

Here is how the Vertical Tail Side Force for Given Moment equation looks like.

-4.5 = - (\frac{5.4}{1.2})

-4.5N = - (\frac{5.4N*m}{1.2m})

-4.5 = - (\frac{5.4}{1.2})

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Vertical Tail Side Force for Given Moment Solution

Follow our step by step solution on how to calculate Vertical Tail Side Force for Given Moment?

FIRST Step Consider the formula

Y v = - (\frac{N v}{𝒍 v})

Next Step Substitute values of Variables

∴

Y v = - (\frac{5.4N*m}{1.2m})

Next Step Prepare to Evaluate

∴

Y v = - (\frac{5.4}{1.2})

LAST Step Evaluate

∴

Y v = -4.5N

Vertical Tail Side Force for Given Moment Formula Elements

Variables

Vertical Tail Side Force

Vertical Tail Side Force is the side force acting on the vertical tail of an aircraft.

Symbol: Y_v

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Vertical Tail Side Force

Vertical Tail Moment

Vertical Tail Moment is the moment produced by the vertical tailplane of an aircraft due to the side force acting on it.

Symbol: N_v

Measurement: Moment of ForceUnit: N*m

Note: Value can be positive or negative.

Formulas to find Vertical Tail Moment

Vertical Tail Moment Arm

The Vertical Tail Moment Arm is the distance between the centroid of the vertical tail shape and the center of gravity of the aircraft.

Symbol: 𝒍_v

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Vertical Tail Moment Arm

Other Formulas to find Vertical Tail Side Force

Go Vertical Tail Side Force

Y v = - C v \cdot α v \cdot S v \cdot Q v

Other formulas in Vertical Tail Contribution category

Go Vertical Tail Angle of Attack

α v = σ + β

Go Vertical Tail Lift Curve Slope

C v = - (\frac{Y v}{α v \cdot Q v \cdot S v})

Go Vertical Tail Angle of Attack for given Vertical Tail Side Force

α v = - (\frac{Y v}{C v \cdot Q v \cdot S v})

Go Vertical Tail Dynamic Pressure for given Vertical Tail Side Force

Q v = - (\frac{Y v}{C v \cdot α v \cdot S v})

How to Evaluate Vertical Tail Side Force for Given Moment?

Vertical Tail Side Force for Given Moment evaluator uses Vertical Tail Side Force = -(Vertical Tail Moment/Vertical Tail Moment Arm) to evaluate the Vertical Tail Side Force, Vertical Tail Side Force for Given Moment is a measure of the force exerted by the vertical tail of an aircraft in response to a moment or turning force, calculated by dividing the moment produced by the vertical tail by the vertical tail moment arm, providing a critical parameter in aircraft design and stability analysis. Vertical Tail Side Force is denoted by Y_v symbol.

How to evaluate Vertical Tail Side Force for Given Moment using this online evaluator? To use this online evaluator for Vertical Tail Side Force for Given Moment, enter Vertical Tail Moment (N_v) & Vertical Tail Moment Arm (𝒍_v) and hit the calculate button.

FAQs on Vertical Tail Side Force for Given Moment

What is the formula to find Vertical Tail Side Force for Given Moment?

The formula of Vertical Tail Side Force for Given Moment is expressed as Vertical Tail Side Force = -(Vertical Tail Moment/Vertical Tail Moment Arm). Here is an example- -4.5 = -(5.4/1.2).

How to calculate Vertical Tail Side Force for Given Moment?

With Vertical Tail Moment (N_v) & Vertical Tail Moment Arm (𝒍_v) we can find Vertical Tail Side Force for Given Moment using the formula - Vertical Tail Side Force = -(Vertical Tail Moment/Vertical Tail Moment Arm).

What are the other ways to Calculate Vertical Tail Side Force?

Here are the different ways to Calculate Vertical Tail Side Force-

Vertical Tail Side Force=-Vertical Tail Lift Curve Slope*Vertical Tail Angle of Attack*Vertical Tail Area*Vertical Tail Dynamic Pressure

Can the Vertical Tail Side Force for Given Moment be negative?

Yes, the Vertical Tail Side Force for Given Moment, measured in Force can be negative.

Which unit is used to measure Vertical Tail Side Force for Given Moment?

Vertical Tail Side Force for Given Moment is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Vertical Tail Side Force for Given Moment can be measured.

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