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Vertical Tail Area for given Vertical Tail Side Force Formula

GoVertical tail area for given vertical tail volume ratio Formula

GoVertical Tail Area for given Yawing Moment Coefficient Formula

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

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

S_v - Vertical Tail Area?Y_v - Vertical Tail Side Force?C_v - Vertical Tail Lift Curve Slope?α_v - Vertical Tail Angle of Attack?Q_v - Vertical Tail Dynamic Pressure?

Vertical Tail Area for given Vertical Tail Side Force Example

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

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

Here is how the Vertical Tail Area for given Vertical Tail Side Force equation looks like.

4.7009 = - \frac{-4.235}{0.7 \cdot 0.117 \cdot 11}

4.7009m² = - \frac{-4.235N}{0.7rad⁻¹ \cdot 0.117rad \cdot 11Pa}

4.7009 = - \frac{-4.235}{0.7 \cdot 0.117 \cdot 11}

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Vertical Tail Area for given Vertical Tail Side Force Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

S v = - \frac{-4.235N}{0.7rad⁻¹ \cdot 0.117rad \cdot 11Pa}

Next Step Prepare to Evaluate

∴

S v = - \frac{-4.235}{0.7 \cdot 0.117 \cdot 11}

Next Step Evaluate

∴

S v = 4.7008547008547m²

LAST Step Rounding Answer

∴

S v = 4.7009m²

Vertical Tail Area for given Vertical Tail Side Force Formula Elements

Variables

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

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 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

Vertical Tail Angle of Attack

Vertical Tail Angle of Attack is the angle of attack experienced by the vertical tailplane of an aircraft.

Symbol: α_v

Measurement: AngleUnit: rad

Note: Value can be positive or negative.

Formulas to find Vertical Tail Angle of Attack

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

Other Formulas to find Vertical Tail Area

Go Vertical tail area for given vertical tail volume ratio

S v = V v \cdot S \cdot \frac{b}{𝒍 v}

Go Vertical Tail Area for given Yawing Moment Coefficient

S v = C n \cdot \frac{S \cdot b \cdot Q w}{𝒍 v \cdot Q v \cdot C v \cdot (β + σ)}

Go Vertical Tail Area for given Moment

S v = \frac{N v}{𝒍 v \cdot C v \cdot (β + σ) \cdot Q 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 Vertical Tail Area for given Vertical Tail Side Force?

Vertical Tail Area for given Vertical Tail Side Force evaluator uses Vertical Tail Area = -(Vertical Tail Side Force)/(Vertical Tail Lift Curve Slope*Vertical Tail Angle of Attack*Vertical Tail Dynamic Pressure) to evaluate the Vertical Tail Area, Vertical Tail Area for given Vertical Tail Side Force is a measure of the surface area of the vertical tail required to produce a given side force, taking into account the lift curve slope, angle of attack, and dynamic pressure. Vertical Tail Area is denoted by S_v symbol.

How to evaluate Vertical Tail Area for given Vertical Tail Side Force using this online evaluator? To use this online evaluator for Vertical Tail Area for given Vertical Tail Side Force, enter Vertical Tail Side Force (Y_v), Vertical Tail Lift Curve Slope (C_v), Vertical Tail Angle of Attack (α_v) & Vertical Tail Dynamic Pressure (Q_v) and hit the calculate button.

FAQs on Vertical Tail Area for given Vertical Tail Side Force

What is the formula to find Vertical Tail Area for given Vertical Tail Side Force?

The formula of Vertical Tail Area for given Vertical Tail Side Force is expressed as Vertical Tail Area = -(Vertical Tail Side Force)/(Vertical Tail Lift Curve Slope*Vertical Tail Angle of Attack*Vertical Tail Dynamic Pressure). Here is an example- 4.700855 = -((-4.235))/(0.7*0.117*11).

How to calculate Vertical Tail Area for given Vertical Tail Side Force?

With Vertical Tail Side Force (Y_v), Vertical Tail Lift Curve Slope (C_v), Vertical Tail Angle of Attack (α_v) & Vertical Tail Dynamic Pressure (Q_v) we can find Vertical Tail Area for given Vertical Tail Side Force using the formula - Vertical Tail Area = -(Vertical Tail Side Force)/(Vertical Tail Lift Curve Slope*Vertical Tail Angle of Attack*Vertical Tail Dynamic Pressure).

What are the other ways to Calculate Vertical Tail Area?

Here are the different ways to Calculate Vertical Tail Area-

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

Can the Vertical Tail Area for given Vertical Tail Side Force be negative?

No, the Vertical Tail Area for given Vertical Tail Side Force, measured in Area cannot be negative.

Which unit is used to measure Vertical Tail Area for given Vertical Tail Side Force?

Vertical Tail Area for given Vertical Tail Side Force is usually measured using the Square Meter[m²] for Area. Square Kilometer[m²], Square Centimeter[m²], Square Millimeter[m²] are the few other units in which Vertical Tail Area for given Vertical Tail Side Force can be measured.

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Vertical Tail Area for given Vertical Tail Side Force Formula

​GoVertical tail area for given vertical tail volume ratio Formula

​GoVertical Tail Area for given Yawing Moment Coefficient Formula

Vertical Tail Area for given Vertical Tail Side Force Example

Vertical Tail Area for given Vertical Tail Side Force Solution

Vertical Tail Area for given Vertical Tail Side Force Formula Elements

Other Formulas to find Vertical Tail Area

Other formulas in Vertical Tail Contribution category

How to Evaluate Vertical Tail Area for given Vertical Tail Side Force?

FAQs on Vertical Tail Area for given Vertical Tail Side Force

Variable Name

GoVertical tail area for given vertical tail volume ratio Formula

GoVertical Tail Area for given Yawing Moment Coefficient Formula