FormulaDen.com

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

Moment Produced by Vertical Tail for given Lift Curve Slope Formula

GoMoment Produced by Vertical Tail for given Side Force Formula

GoMoment Produced by Vertical Tail for given Moment Coefficient Formula

Fx Copy

LaTeX Copy

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 C v \cdot (β + σ) \cdot Q v \cdot S v

N_v - Vertical Tail Moment?𝒍_v - Vertical Tail Moment Arm?C_v - Vertical Tail Lift Curve Slope?β - Sideslip Angle?σ - Sidewash Angle?Q_v - Vertical Tail Dynamic Pressure?S_v - Vertical Tail Area?

Moment Produced by Vertical Tail for given Lift Curve Slope Example

With values

With units

Only example

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

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

Here is how the Moment Produced by Vertical Tail for given Lift Curve Slope equation looks like.

5.4054 = 1.2 \cdot 0.7 \cdot (0.05 + 0.067) \cdot 11 \cdot 5

5.4054N*m = 1.2m \cdot 0.7rad⁻¹ \cdot (0.05rad + 0.067rad) \cdot 11Pa \cdot 5m²

5.4054 = 1.2 \cdot 0.7 \cdot (0.05 + 0.067) \cdot 11 \cdot 5

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 Moment Produced by Vertical Tail for given Lift Curve Slope

Moment Produced by Vertical Tail for given Lift Curve Slope Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

N v = 1.2m \cdot 0.7rad⁻¹ \cdot (0.05rad + 0.067rad) \cdot 11Pa \cdot 5m²

Next Step Prepare to Evaluate

∴

N v = 1.2 \cdot 0.7 \cdot (0.05 + 0.067) \cdot 11 \cdot 5

LAST Step Evaluate

∴

N v = 5.4054N*m

Moment Produced by Vertical Tail for given Lift Curve Slope 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 Lift Curve Slope

The Vertical Tail Lift Curve Slope is the slope associated with the lift curve of a vertical tailplane of an aircraft.

Symbol: C_v

Measurement: Reciprocal AngleUnit: rad⁻¹

Note: Value can be positive or negative.

Formulas to find Vertical Tail Lift Curve Slope

Sideslip Angle

The Sideslip Angle, also called the angle of sideslip, is a term used in fluid dynamics and aerodynamics, and aviation which relates to the rotation of the aircraft centerline from the relative wind.

Symbol: β

Measurement: AngleUnit: rad

Note: Value can be positive or negative.

Formulas to find Sideslip Angle

Sidewash Angle

Sidewash Angle is caused by the flow field distortion due to the wings and fuselage. It is analogous to the downwash angle for the horizontal tailplane.

Symbol: σ

Measurement: AngleUnit: rad

Note: Value can be positive or negative.

Formulas to find Sidewash Angle

Vertical Tail Dynamic Pressure

Vertical Tail Dynamic Pressure is the dynamic pressure associated with the vertical tail of an aircraft.

Symbol: Q_v

Measurement: PressureUnit: Pa

Note: Value should be greater than 0.

Formulas to find Vertical Tail Dynamic Pressure

Vertical Tail Area

The Vertical Tail Area is the area of the surface of the vertical tail, including the submerged area to the fuselage centerline.

Symbol: S_v

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Vertical Tail 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 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

How to Evaluate Moment Produced by Vertical Tail for given Lift Curve Slope?

Moment Produced by Vertical Tail for given Lift Curve Slope evaluator uses Vertical Tail Moment = Vertical Tail Moment Arm*Vertical Tail Lift Curve Slope*(Sideslip Angle+Sidewash Angle)*Vertical Tail Dynamic Pressure*Vertical Tail Area to evaluate the Vertical Tail Moment, Moment produced by vertical tail for given lift curve slope is a measure of the rotational force generated by the vertical tail of an aircraft, calculated by multiplying the vertical tail moment arm, lift curve slope, sideslip angle, sidewash angle, dynamic pressure, and vertical tail area, providing a critical indicator of an aircraft's stability and control during flight. Vertical Tail Moment is denoted by N_v symbol.

How to evaluate Moment Produced by Vertical Tail for given Lift Curve Slope using this online evaluator? To use this online evaluator for Moment Produced by Vertical Tail for given Lift Curve Slope, enter Vertical Tail Moment Arm (𝒍_v), Vertical Tail Lift Curve Slope (C_v), Sideslip Angle (β), Sidewash Angle (σ), Vertical Tail Dynamic Pressure (Q_v) & Vertical Tail Area (S_v) and hit the calculate button.

FAQs on Moment Produced by Vertical Tail for given Lift Curve Slope

What is the formula to find Moment Produced by Vertical Tail for given Lift Curve Slope?

The formula of Moment Produced by Vertical Tail for given Lift Curve Slope is expressed as Vertical Tail Moment = Vertical Tail Moment Arm*Vertical Tail Lift Curve Slope*(Sideslip Angle+Sidewash Angle)*Vertical Tail Dynamic Pressure*Vertical Tail Area. Here is an example- 5.4054 = 1.2*0.7*(0.05+0.067)*11*5.

How to calculate Moment Produced by Vertical Tail for given Lift Curve Slope?

With Vertical Tail Moment Arm (𝒍_v), Vertical Tail Lift Curve Slope (C_v), Sideslip Angle (β), Sidewash Angle (σ), Vertical Tail Dynamic Pressure (Q_v) & Vertical Tail Area (S_v) we can find Moment Produced by Vertical Tail for given Lift Curve Slope using the formula - Vertical Tail Moment = Vertical Tail Moment Arm*Vertical Tail Lift Curve Slope*(Sideslip Angle+Sidewash Angle)*Vertical Tail Dynamic Pressure*Vertical Tail 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=Yawing Moment Coefficient*Wing Dynamic Pressure*Wingspan*Reference Area

Can the Moment Produced by Vertical Tail for given Lift Curve Slope be negative?

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

Which unit is used to measure Moment Produced by Vertical Tail for given Lift Curve Slope?

Moment Produced by Vertical Tail for given Lift Curve Slope 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 Lift Curve Slope can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Moment Produced by Vertical Tail for given Lift Curve Slope Formula

​GoMoment Produced by Vertical Tail for given Side Force Formula

​GoMoment Produced by Vertical Tail for given Moment Coefficient Formula

Moment Produced by Vertical Tail for given Lift Curve Slope Example

Moment Produced by Vertical Tail for given Lift Curve Slope Solution

Moment Produced by Vertical Tail for given Lift Curve Slope 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 Lift Curve Slope?

FAQs on Moment Produced by Vertical Tail for given Lift Curve Slope

Variable Name

GoMoment Produced by Vertical Tail for given Side Force Formula

GoMoment Produced by Vertical Tail for given Moment Coefficient Formula