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Wingspan for given Vertical Tail Volume Ratio Formula

GoWingspan for given Yawing Moment Coefficient Formula

GoWingspan for Yawing Moment Coefficient given Sideslip Angle and Sidewash Angle Formula

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

b = 𝒍 v \cdot \frac{S v}{S \cdot V v}

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

Wingspan for given Vertical Tail Volume Ratio Example

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Here is how the Wingspan for given Vertical Tail Volume Ratio equation looks like with Values.

Here is how the Wingspan for given Vertical Tail Volume Ratio equation looks like with Units.

Here is how the Wingspan for given Vertical Tail Volume Ratio equation looks like.

1.1579 = 1.2 \cdot \frac{5}{5.08 \cdot 1.02}

1.1579m = 1.2m \cdot \frac{5m²}{5.08m² \cdot 1.02}

1.1579 = 1.2 \cdot \frac{5}{5.08 \cdot 1.02}

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Wingspan for given Vertical Tail Volume Ratio Solution

Follow our step by step solution on how to calculate Wingspan for given Vertical Tail Volume Ratio?

FIRST Step Consider the formula

b = 𝒍 v \cdot \frac{S v}{S \cdot V v}

Next Step Substitute values of Variables

∴

b = 1.2m \cdot \frac{5m²}{5.08m² \cdot 1.02}

Next Step Prepare to Evaluate

∴

b = 1.2 \cdot \frac{5}{5.08 \cdot 1.02}

Next Step Evaluate

∴

b = 1.15794349235757m

LAST Step Rounding Answer

∴

b = 1.1579m

Wingspan for given Vertical Tail Volume Ratio Formula Elements

Variables

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

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

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

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

Other Formulas to find Wingspan

Go Wingspan for given Yawing Moment Coefficient

b = \frac{N v}{C n \cdot S \cdot Q w}

Go Wingspan for Yawing Moment Coefficient given Sideslip Angle and Sidewash Angle

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

Other formulas in Wing Tail Interaction category

Go Wing Dynamic Pressure for given Yawing Moment Coefficient

Q w = \frac{N v}{C n \cdot S \cdot b}

Go Wing Area for given Moment Produced by Vertical Tail

S = \frac{N v}{C n \cdot Q w \cdot b}

Go Dynamic Pressure at Wing for given Yawing Moment Coefficient

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

Go Vertical Tail Dynamic Pressure for given Moment

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

How to Evaluate Wingspan for given Vertical Tail Volume Ratio?

Wingspan for given Vertical Tail Volume Ratio evaluator uses Wingspan = Vertical Tail Moment Arm*Vertical Tail Area/(Reference Area*Vertical Tail Volume Ratio) to evaluate the Wingspan, Wingspan for given Vertical Tail Volume Ratio is a measure of the wingspan of an aircraft, calculated by dividing the product of the vertical tail moment arm and vertical tail area by the product of the reference area and the vertical tail volume ratio, providing a critical design parameter for aircraft stability and control. Wingspan is denoted by b symbol.

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

FAQs on Wingspan for given Vertical Tail Volume Ratio

What is the formula to find Wingspan for given Vertical Tail Volume Ratio?

The formula of Wingspan for given Vertical Tail Volume Ratio is expressed as Wingspan = Vertical Tail Moment Arm*Vertical Tail Area/(Reference Area*Vertical Tail Volume Ratio). Here is an example- 1.157943 = 1.2*5/(5.08*1.02).

How to calculate Wingspan for given Vertical Tail Volume Ratio?

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

What are the other ways to Calculate Wingspan?

Here are the different ways to Calculate Wingspan-

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

Can the Wingspan for given Vertical Tail Volume Ratio be negative?

No, the Wingspan for given Vertical Tail Volume Ratio, measured in Length cannot be negative.

Which unit is used to measure Wingspan for given Vertical Tail Volume Ratio?

Wingspan for given Vertical Tail Volume Ratio is usually measured using the Meter[m] for Length. Millimeter[m], Kilometer[m], Decimeter[m] are the few other units in which Wingspan for given Vertical Tail Volume Ratio can be measured.

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: Value
: Unit

Wingspan for given Vertical Tail Volume Ratio Formula

​GoWingspan for given Yawing Moment Coefficient Formula

​GoWingspan for Yawing Moment Coefficient given Sideslip Angle and Sidewash Angle Formula

Wingspan for given Vertical Tail Volume Ratio Example

Wingspan for given Vertical Tail Volume Ratio Solution

Wingspan for given Vertical Tail Volume Ratio Formula Elements

Other Formulas to find Wingspan

Other formulas in Wing Tail Interaction category

How to Evaluate Wingspan for given Vertical Tail Volume Ratio?

FAQs on Wingspan for given Vertical Tail Volume Ratio

Variable Name

GoWingspan for given Yawing Moment Coefficient Formula

GoWingspan for Yawing Moment Coefficient given Sideslip Angle and Sidewash Angle Formula