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Yawing Moment Coefficient using Wingspan Formula

GoYawing Moment Coefficient for given Vertical Tail Lift Curve Slope Formula

GoYawing Moment Coefficient for given Vertical Tail Volume Ratio Formula

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Yawing Moment Coefficient is the coefficient associated with the moment that tends to rotate an airplane about its vertical (or yaw) axis. Check FAQs

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

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

Yawing Moment Coefficient using Wingspan Example

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

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

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

1.4005 = \frac{5.4}{0.66 \cdot 5.08 \cdot 1.15}

1.4005 = \frac{5.4N*m}{0.66Pa \cdot 5.08m² \cdot 1.15m}

1.4005 = \frac{5.4}{0.66 \cdot 5.08 \cdot 1.15}

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Yawing Moment Coefficient using Wingspan Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

C n = \frac{5.4N*m}{0.66Pa \cdot 5.08m² \cdot 1.15m}

Next Step Prepare to Evaluate

∴

C n = \frac{5.4}{0.66 \cdot 5.08 \cdot 1.15}

Next Step Evaluate

∴

C n = 1.40051663502537

LAST Step Rounding Answer

∴

C n = 1.4005

Yawing Moment Coefficient using Wingspan Formula Elements

Variables

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

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

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

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

Other Formulas to find Yawing Moment Coefficient

Go Yawing Moment Coefficient for given Vertical Tail Lift Curve Slope

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

Go Yawing Moment Coefficient for given Vertical Tail Volume Ratio

C n = V v \cdot η v \cdot C v \cdot (β + σ)

Other formulas in Aerodynamic Parameters category

Go Sideslip Angle for Aircraft

β = α v - σ

Go Sidewash angle

σ = α v - β

Go Sidewash Angle for given Moment Produced by Vertical Tail

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

Go Sideslip Angle for given Moment Produced by Vertical Tail

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

How to Evaluate Yawing Moment Coefficient using Wingspan?

Yawing Moment Coefficient using Wingspan evaluator uses Yawing Moment Coefficient = Vertical Tail Moment/(Wing Dynamic Pressure*Reference Area*Wingspan) to evaluate the Yawing Moment Coefficient, Yawing Moment Coefficient using Wingspan formula is a measure of the rotational force that causes an aircraft to rotate around its vertical axis, calculated by dividing the moment produced by the vertical tail by the product of wing dynamic pressure, reference area, and wingspan, this coefficient is a crucial factor in evaluating an aircraft's directional stability and control characteristics. Yawing Moment Coefficient is denoted by C_n symbol.

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

FAQs on Yawing Moment Coefficient using Wingspan

What is the formula to find Yawing Moment Coefficient using Wingspan?

The formula of Yawing Moment Coefficient using Wingspan is expressed as Yawing Moment Coefficient = Vertical Tail Moment/(Wing Dynamic Pressure*Reference Area*Wingspan). Here is an example- 1.400517 = 5.4/(0.66*5.08*1.15).

How to calculate Yawing Moment Coefficient using Wingspan?

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

What are the other ways to Calculate Yawing Moment Coefficient?

Here are the different ways to Calculate Yawing Moment Coefficient-

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

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Yawing Moment Coefficient using Wingspan Formula

​GoYawing Moment Coefficient for given Vertical Tail Lift Curve Slope Formula

​GoYawing Moment Coefficient for given Vertical Tail Volume Ratio Formula

Yawing Moment Coefficient using Wingspan Example

Yawing Moment Coefficient using Wingspan Solution

Yawing Moment Coefficient using Wingspan Formula Elements

Other Formulas to find Yawing Moment Coefficient

Other formulas in Aerodynamic Parameters category

How to Evaluate Yawing Moment Coefficient using Wingspan?

FAQs on Yawing Moment Coefficient using Wingspan

Variable Name

GoYawing Moment Coefficient for given Vertical Tail Lift Curve Slope Formula

GoYawing Moment Coefficient for given Vertical Tail Volume Ratio Formula