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Moment Produced by Vertical Tail for given Moment Coefficient Formula

GoMoment Produced by Vertical Tail for given Side Force Formula

GoMoment Produced by Vertical Tail for given Lift Curve Slope 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 = C n \cdot Q w \cdot b \cdot S

N_v - Vertical Tail Moment?C_n - Yawing Moment Coefficient?Q_w - Wing Dynamic Pressure?b - Wingspan?S - Reference Area?

Moment Produced by Vertical Tail for given Moment Coefficient Example

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

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

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

5.398 = 1.4 \cdot 0.66 \cdot 1.15 \cdot 5.08

5.398N*m = 1.4 \cdot 0.66Pa \cdot 1.15m \cdot 5.08m²

5.398 = 1.4 \cdot 0.66 \cdot 1.15 \cdot 5.08

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Moment Produced by Vertical Tail for given Moment Coefficient Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

N v = 1.4 \cdot 0.66Pa \cdot 1.15m \cdot 5.08m²

Next Step Prepare to Evaluate

∴

N v = 1.4 \cdot 0.66 \cdot 1.15 \cdot 5.08

Next Step Evaluate

∴

N v = 5.398008N*m

LAST Step Rounding Answer

∴

N v = 5.398N*m

Moment Produced by Vertical Tail for given Moment Coefficient 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

Yawing Moment Coefficient

Yawing Moment Coefficient is the coefficient associated with the moment that tends to rotate an airplane about its vertical (or yaw) axis.

Symbol: C_n

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Yawing Moment Coefficient

Wing Dynamic Pressure

Wing Dynamic Pressure is the dynamic pressure associated with the wing of an aircraft.

Symbol: Q_w

Measurement: PressureUnit: Pa

Note: Value should be greater than 0.

Formulas to find Wing Dynamic Pressure

Wingspan

The Wingspan (or just span) of a bird or an airplane is the distance from one wingtip to the other wingtip.

Symbol: b

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Wingspan

Reference Area

The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.

Symbol: S

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Reference Area

Other Formulas to find Vertical Tail Moment

Go Moment Produced by Vertical Tail for given Side Force

N v = - (𝒍 v \cdot Y v)

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

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 Moment Coefficient?

Moment Produced by Vertical Tail for given Moment Coefficient evaluator uses Vertical Tail Moment = Yawing Moment Coefficient*Wing Dynamic Pressure*Wingspan*Reference Area to evaluate the Vertical Tail Moment, Moment Produced by Vertical Tail for given Moment Coefficient is a measure of the rotational force generated by the vertical tail of an aircraft, calculated by multiplying the yawing moment coefficient, wing dynamic pressure, wingspan, and reference area. Vertical Tail Moment is denoted by N_v symbol.

How to evaluate Moment Produced by Vertical Tail for given Moment Coefficient using this online evaluator? To use this online evaluator for Moment Produced by Vertical Tail for given Moment Coefficient, enter Yawing Moment Coefficient (C_n), Wing Dynamic Pressure (Q_w), Wingspan (b) & Reference Area (S) and hit the calculate button.

FAQs on Moment Produced by Vertical Tail for given Moment Coefficient

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

The formula of Moment Produced by Vertical Tail for given Moment Coefficient is expressed as Vertical Tail Moment = Yawing Moment Coefficient*Wing Dynamic Pressure*Wingspan*Reference Area. Here is an example- 5.398008 = 1.4*0.66*1.15*5.08.

How to calculate Moment Produced by Vertical Tail for given Moment Coefficient?

With Yawing Moment Coefficient (C_n), Wing Dynamic Pressure (Q_w), Wingspan (b) & Reference Area (S) we can find Moment Produced by Vertical Tail for given Moment Coefficient using the formula - Vertical Tail Moment = Yawing Moment Coefficient*Wing Dynamic Pressure*Wingspan*Reference Area.

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 Side Force)
Vertical Tail Moment=Vertical Tail Moment Arm*Vertical Tail Lift Curve Slope*(Sideslip Angle+Sidewash Angle)*Vertical Tail Dynamic Pressure*Vertical Tail Area

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

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

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

Moment Produced by Vertical Tail for given Moment Coefficient 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 Moment Coefficient can be measured.

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Moment Produced by Vertical Tail for given Moment Coefficient Formula

​GoMoment Produced by Vertical Tail for given Side Force Formula

​GoMoment Produced by Vertical Tail for given Lift Curve Slope Formula

Moment Produced by Vertical Tail for given Moment Coefficient Example

Moment Produced by Vertical Tail for given Moment Coefficient Solution

Moment Produced by Vertical Tail for given Moment Coefficient Formula Elements

Other Formulas to find Vertical Tail Moment

Other formulas in Vertical Tail Contribution category

How to Evaluate Moment Produced by Vertical Tail for given Moment Coefficient?

FAQs on Moment Produced by Vertical Tail for given Moment Coefficient

Variable Name

GoMoment Produced by Vertical Tail for given Side Force Formula

GoMoment Produced by Vertical Tail for given Lift Curve Slope Formula