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Vertical tail area for given vertical tail volume ratio Formula

GoVertical Tail Area for given Vertical Tail Side Force 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 = V v \cdot S \cdot \frac{b}{𝒍 v}

S_v - Vertical Tail Area?V_v - Vertical Tail Volume Ratio?S - Reference Area?b - Wingspan?𝒍_v - Vertical Tail Moment Arm?

Vertical tail area for given vertical tail volume ratio Example

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Here is how the Vertical tail area for given vertical tail volume ratio equation looks like with Values.

Here is how the Vertical tail area for given vertical tail volume ratio equation looks like with Units.

Here is how the Vertical tail area for given vertical tail volume ratio equation looks like.

4.9657 = 1.02 \cdot 5.08 \cdot \frac{1.15}{1.2}

4.9657m² = 1.02 \cdot 5.08m² \cdot \frac{1.15m}{1.2m}

4.9657 = 1.02 \cdot 5.08 \cdot \frac{1.15}{1.2}

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Vertical tail area for given vertical tail volume ratio Solution

Follow our step by step solution on how to calculate Vertical tail area for given vertical tail volume ratio?

FIRST Step Consider the formula

S v = V v \cdot S \cdot \frac{b}{𝒍 v}

Next Step Substitute values of Variables

∴

S v = 1.02 \cdot 5.08m² \cdot \frac{1.15m}{1.2m}

Next Step Prepare to Evaluate

∴

S v = 1.02 \cdot 5.08 \cdot \frac{1.15}{1.2}

LAST Step Evaluate

∴

S v = 4.9657m²

Vertical tail area for given vertical tail volume ratio 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 Volume Ratio

Vertical Tail Volume Ratio relates to the area of the vertical tail, the distance between the centroid of vertical tail area and aircraft's e.g., the wing area, and the wingspan.

Symbol: V_v

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Vertical Tail Volume Ratio

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

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

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 Area

Go Vertical Tail Area for given Vertical Tail Side Force

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

Vertical tail area for given vertical tail volume ratio evaluator uses Vertical Tail Area = Vertical Tail Volume Ratio*Reference Area*Wingspan/Vertical Tail Moment Arm to evaluate the Vertical Tail Area, Vertical Tail Area for Given Vertical Tail Volume Ratio is a calculation that determines the vertical tail area of an aircraft based on the vertical tail volume ratio, reference area, wingspan, and vertical tail moment arm, this formula is essential in aircraft design, as it helps to ensure the stability and control of the aircraft during flight. Vertical Tail Area is denoted by S_v symbol.

How to evaluate Vertical tail area for given vertical tail volume ratio using this online evaluator? To use this online evaluator for Vertical tail area for given vertical tail volume ratio, enter Vertical Tail Volume Ratio (V_v), Reference Area (S), Wingspan (b) & Vertical Tail Moment Arm (𝒍_v) and hit the calculate button.

FAQs on Vertical tail area for given vertical tail volume ratio

What is the formula to find Vertical tail area for given vertical tail volume ratio?

The formula of Vertical tail area for given vertical tail volume ratio is expressed as Vertical Tail Area = Vertical Tail Volume Ratio*Reference Area*Wingspan/Vertical Tail Moment Arm. Here is an example- 5.306483 = 1.02*5.08*1.15/1.2.

How to calculate Vertical tail area for given vertical tail volume ratio?

With Vertical Tail Volume Ratio (V_v), Reference Area (S), Wingspan (b) & Vertical Tail Moment Arm (𝒍_v) we can find Vertical tail area for given vertical tail volume ratio using the formula - Vertical Tail Area = Vertical Tail Volume Ratio*Reference Area*Wingspan/Vertical Tail Moment Arm.

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 Side Force)/(Vertical Tail Lift Curve Slope*Vertical Tail Angle of Attack*Vertical Tail Dynamic Pressure)
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 volume ratio be negative?

No, the Vertical tail area for given vertical tail volume ratio, measured in Area cannot be negative.

Which unit is used to measure Vertical tail area for given vertical tail volume ratio?

Vertical tail area for given vertical tail volume ratio 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 volume ratio can be measured.

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Vertical tail area for given vertical tail volume ratio Formula

​GoVertical Tail Area for given Vertical Tail Side Force Formula

​GoVertical Tail Area for given Yawing Moment Coefficient Formula

Vertical tail area for given vertical tail volume ratio Example

Vertical tail area for given vertical tail volume ratio Solution

Vertical tail area for given vertical tail volume ratio 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 volume ratio?

FAQs on Vertical tail area for given vertical tail volume ratio

Variable Name

GoVertical Tail Area for given Vertical Tail Side Force Formula

GoVertical Tail Area for given Yawing Moment Coefficient Formula