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Wing Area for given Moment Produced by Vertical Tail Formula

GoWing Area for given Yawing Moment Coefficient Formula

GoWing Area for given Vertical Tail Volume Ratio Formula

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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. Check FAQs

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

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

Wing Area for given Moment Produced by Vertical Tail Example

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

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

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

5.0819 = \frac{5.4}{1.4 \cdot 0.66 \cdot 1.15}

5.0819m² = \frac{5.4N*m}{1.4 \cdot 0.66Pa \cdot 1.15m}

5.0819 = \frac{5.4}{1.4 \cdot 0.66 \cdot 1.15}

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Wing Area for given Moment Produced by Vertical Tail Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

S = \frac{5.4N*m}{1.4 \cdot 0.66Pa \cdot 1.15m}

Next Step Prepare to Evaluate

∴

S = \frac{5.4}{1.4 \cdot 0.66 \cdot 1.15}

Next Step Evaluate

∴

S = 5.08187464709204m²

LAST Step Rounding Answer

∴

S = 5.0819m²

Wing Area for given Moment Produced by Vertical Tail Formula Elements

Variables

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 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

Other Formulas to find Reference Area

Go Wing Area for given Yawing Moment Coefficient

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

Go Wing Area for given Vertical Tail Volume Ratio

S = 𝒍 v \cdot \frac{S v}{b \cdot V v}

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 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}

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}

How to Evaluate Wing Area for given Moment Produced by Vertical Tail?

Wing Area for given Moment Produced by Vertical Tail evaluator uses Reference Area = Vertical Tail Moment/(Yawing Moment Coefficient*Wing Dynamic Pressure*Wingspan) to evaluate the Reference Area, Wing Area for given Moment Produced by Vertical Tail is a measure of the required area of the vertical tail to produce a specific yawing moment, dependent on the yawing moment coefficient, dynamic pressure, and wingspan of the aircraft. Reference Area is denoted by S symbol.

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

FAQs on Wing Area for given Moment Produced by Vertical Tail

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

The formula of Wing Area for given Moment Produced by Vertical Tail is expressed as Reference Area = Vertical Tail Moment/(Yawing Moment Coefficient*Wing Dynamic Pressure*Wingspan). Here is an example- 5.081875 = 5.4/(1.4*0.66*1.15).

How to calculate Wing Area for given Moment Produced by Vertical Tail?

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

What are the other ways to Calculate Reference Area?

Here are the different ways to Calculate Reference Area-

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

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

No, the Wing Area for given Moment Produced by Vertical Tail, measured in Area cannot be negative.

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

Wing Area for given Moment Produced by Vertical Tail 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 Wing Area for given Moment Produced by Vertical Tail can be measured.

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Wing Area for given Moment Produced by Vertical Tail Formula

​GoWing Area for given Yawing Moment Coefficient Formula

​GoWing Area for given Vertical Tail Volume Ratio Formula

Wing Area for given Moment Produced by Vertical Tail Example

Wing Area for given Moment Produced by Vertical Tail Solution

Wing Area for given Moment Produced by Vertical Tail Formula Elements

Other Formulas to find Reference Area

Other formulas in Wing Tail Interaction category

How to Evaluate Wing Area for given Moment Produced by Vertical Tail?

FAQs on Wing Area for given Moment Produced by Vertical Tail

Variable Name

GoWing Area for given Yawing Moment Coefficient Formula

GoWing Area for given Vertical Tail Volume Ratio Formula