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Moment Produced by Vertical Tail for given Side Force Formula

GoMoment Produced by Vertical Tail for given Lift Curve Slope Formula

GoMoment Produced by Vertical Tail for given Moment Coefficient Formula

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

N v = - (𝒍 v \cdot Y v)

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

Moment Produced by Vertical Tail for given Side Force Example

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

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

Here is how the Moment Produced by Vertical Tail for given Side Force equation looks like.

5.082 = - (1.2 \cdot -4.235)

5.082N*m = - (1.2m \cdot -4.235N)

5.082 = - (1.2 \cdot -4.235)

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Moment Produced by Vertical Tail for given Side Force Solution

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

FIRST Step Consider the formula

N v = - (𝒍 v \cdot Y v)

Next Step Substitute values of Variables

∴

N v = - (1.2m \cdot -4.235N)

Next Step Prepare to Evaluate

∴

N v = - (1.2 \cdot -4.235)

LAST Step Evaluate

∴

N v = 5.082N*m

Moment Produced by Vertical Tail for given Side Force Formula Elements

Variables

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

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

Other Formulas to find Vertical Tail Moment

Go Moment Produced by Vertical Tail for given Lift Curve Slope

N v = 𝒍 v \cdot C v \cdot (β + σ) \cdot Q v \cdot S v

Go Moment Produced by Vertical Tail for given Moment Coefficient

N v = C n \cdot Q w \cdot b \cdot S

Other formulas in Vertical Tail Contribution category

Go Vertical Tail Angle of Attack

α v = σ + β

Go Vertical Tail Side Force

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

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})

How to Evaluate Moment Produced by Vertical Tail for given Side Force?

Moment Produced by Vertical Tail for given Side Force evaluator uses Vertical Tail Moment = -(Vertical Tail Moment Arm*Vertical Tail Side Force) to evaluate the Vertical Tail Moment, Moment Produced by Vertical Tail for given Side Force is a measure of the rotating force that the vertical tail of an aircraft produces in response to a sideways force, calculated as the product of the vertical tail's moment arm and the side force, with the moment arm being the distance from the aircraft's axis of rotation to the vertical tail's centre of pressure, and the side force being the horizontal force acting on the vertical tail. Vertical Tail Moment is denoted by N_v symbol.

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

FAQs on Moment Produced by Vertical Tail for given Side Force

What is the formula to find Moment Produced by Vertical Tail for given Side Force?

The formula of Moment Produced by Vertical Tail for given Side Force is expressed as Vertical Tail Moment = -(Vertical Tail Moment Arm*Vertical Tail Side Force). Here is an example- 5.082 = -(1.2*(-4.235)).

How to calculate Moment Produced by Vertical Tail for given Side Force?

With Vertical Tail Moment Arm (𝒍_v) & Vertical Tail Side Force (Y_v) we can find Moment Produced by Vertical Tail for given Side Force using the formula - Vertical Tail Moment = -(Vertical Tail Moment Arm*Vertical Tail Side Force).

What are the other ways to Calculate Vertical Tail Moment?

Here are the different ways to Calculate Vertical Tail Moment-

Vertical Tail Moment=Vertical Tail Moment Arm*Vertical Tail Lift Curve Slope*(Sideslip Angle+Sidewash Angle)*Vertical Tail Dynamic Pressure*Vertical Tail Area
Vertical Tail Moment=Yawing Moment Coefficient*Wing Dynamic Pressure*Wingspan*Reference Area

Can the Moment Produced by Vertical Tail for given Side Force be negative?

Yes, the Moment Produced by Vertical Tail for given Side Force, measured in Moment of Force can be negative.

Which unit is used to measure Moment Produced by Vertical Tail for given Side Force?

Moment Produced by Vertical Tail for given Side Force is usually measured using the Newton Meter[N*m] for Moment of Force. Kilonewton Meter[N*m], Millinewton Meter[N*m], Micronewton Meter[N*m] are the few other units in which Moment Produced by Vertical Tail for given Side Force can be measured.

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