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Wingspan for given Yawing Moment Coefficient Formula

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

GoWingspan for given Vertical Tail Volume Ratio 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 = \frac{N v}{C n \cdot S \cdot Q w}

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

Wingspan for given Yawing Moment Coefficient Example

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Here is how the Wingspan for given Yawing Moment Coefficient equation looks like with Values.

Here is how the Wingspan for given Yawing Moment Coefficient equation looks like with Units.

Here is how the Wingspan for given Yawing Moment Coefficient equation looks like.

1.1504 = \frac{5.4}{1.4 \cdot 5.08 \cdot 0.66}

1.1504m = \frac{5.4N*m}{1.4 \cdot 5.08m² \cdot 0.66Pa}

1.1504 = \frac{5.4}{1.4 \cdot 5.08 \cdot 0.66}

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Wingspan for given Yawing Moment Coefficient Solution

Follow our step by step solution on how to calculate Wingspan for given Yawing Moment Coefficient?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

b = \frac{5.4N*m}{1.4 \cdot 5.08m² \cdot 0.66Pa}

Next Step Prepare to Evaluate

∴

b = \frac{5.4}{1.4 \cdot 5.08 \cdot 0.66}

Next Step Evaluate

∴

b = 1.15042437877084m

LAST Step Rounding Answer

∴

b = 1.1504m

Wingspan for given Yawing Moment Coefficient 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

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

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

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

Other Formulas to find Wingspan

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 Wingspan for given Vertical Tail Volume Ratio

b = 𝒍 v \cdot \frac{S v}{S \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 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 Yawing Moment Coefficient?

Wingspan for given Yawing Moment Coefficient evaluator uses Wingspan = Vertical Tail Moment/(Yawing Moment Coefficient*Reference Area*Wing Dynamic Pressure) to evaluate the Wingspan, Wingspan for given Yawing Moment Coefficient is a measure of the wingspan required to balance the yawing moment produced by the vertical tail, taking into account the yawing moment coefficient, reference area and wing dynamic pressure. Wingspan is denoted by b symbol.

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

FAQs on Wingspan for given Yawing Moment Coefficient

What is the formula to find Wingspan for given Yawing Moment Coefficient?

The formula of Wingspan for given Yawing Moment Coefficient is expressed as Wingspan = Vertical Tail Moment/(Yawing Moment Coefficient*Reference Area*Wing Dynamic Pressure). Here is an example- 1.150424 = 5.4/(1.4*5.08*0.66).

How to calculate Wingspan for given Yawing Moment Coefficient?

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

What are the other ways to Calculate Wingspan?

Here are the different ways to Calculate Wingspan-

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)
Wingspan=Vertical Tail Moment Arm*Vertical Tail Area/(Reference Area*Vertical Tail Volume Ratio)

Can the Wingspan for given Yawing Moment Coefficient be negative?

No, the Wingspan for given Yawing Moment Coefficient, measured in Length cannot be negative.

Which unit is used to measure Wingspan for given Yawing Moment Coefficient?

Wingspan for given Yawing Moment Coefficient 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 Yawing Moment Coefficient can be measured.

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Wingspan for given Yawing Moment Coefficient Formula

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

​GoWingspan for given Vertical Tail Volume Ratio Formula

Wingspan for given Yawing Moment Coefficient Example

Wingspan for given Yawing Moment Coefficient Solution

Wingspan for given Yawing Moment Coefficient Formula Elements

Other Formulas to find Wingspan

Other formulas in Wing Tail Interaction category

How to Evaluate Wingspan for given Yawing Moment Coefficient?

FAQs on Wingspan for given Yawing Moment Coefficient

Variable Name

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

GoWingspan for given Vertical Tail Volume Ratio Formula