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Wing Dynamic Pressure for given Yawing Moment Coefficient Formula

GoDynamic Pressure at Wing for given Yawing Moment Coefficient Formula

GoDynamic Pressure at Wing for given Vertical Tail Efficiency Formula

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Wing Dynamic Pressure is the dynamic pressure associated with the wing of an aircraft. Check FAQs

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

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

Wing Dynamic Pressure for given Yawing Moment Coefficient Example

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Here is how the Wing Dynamic Pressure for given Yawing Moment Coefficient equation looks like with Values.

Here is how the Wing Dynamic Pressure for given Yawing Moment Coefficient equation looks like with Units.

Here is how the Wing Dynamic Pressure for given Yawing Moment Coefficient equation looks like.

0.6602 = \frac{5.4}{1.4 \cdot 5.08 \cdot 1.15}

0.6602Pa = \frac{5.4N*m}{1.4 \cdot 5.08m² \cdot 1.15m}

0.6602 = \frac{5.4}{1.4 \cdot 5.08 \cdot 1.15}

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Wing Dynamic Pressure for given Yawing Moment Coefficient Solution

Follow our step by step solution on how to calculate Wing Dynamic Pressure for given Yawing Moment Coefficient?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

Q w = \frac{5.4N*m}{1.4 \cdot 5.08m² \cdot 1.15m}

Next Step Prepare to Evaluate

∴

Q w = \frac{5.4}{1.4 \cdot 5.08 \cdot 1.15}

Next Step Evaluate

∴

Q w = 0.660243556511958Pa

LAST Step Rounding Answer

∴

Q w = 0.6602Pa

Wing Dynamic Pressure for given Yawing Moment Coefficient Formula Elements

Variables

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

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

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 Wing Dynamic Pressure

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 Dynamic Pressure at Wing for given Vertical Tail Efficiency

Q w = \frac{Q v}{η v}

Other formulas in Wing Tail Interaction category

Go Wing Area for given Moment Produced by Vertical Tail

S = \frac{N v}{C n \cdot Q w \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 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 Wing Dynamic Pressure for given Yawing Moment Coefficient?

Wing Dynamic Pressure for given Yawing Moment Coefficient evaluator uses Wing Dynamic Pressure = Vertical Tail Moment/(Yawing Moment Coefficient*Reference Area*Wingspan) to evaluate the Wing Dynamic Pressure, Wing Dynamic Pressure for given Yawing Moment Coefficient is a measure of the pressure exerted on the wing of an aircraft, calculated by dividing the moment produced by the vertical tail by the product of the yawing moment coefficient, reference area and wingspan. Wing Dynamic Pressure is denoted by Q_w symbol.

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

FAQs on Wing Dynamic Pressure for given Yawing Moment Coefficient

What is the formula to find Wing Dynamic Pressure for given Yawing Moment Coefficient?

The formula of Wing Dynamic Pressure for given Yawing Moment Coefficient is expressed as Wing Dynamic Pressure = Vertical Tail Moment/(Yawing Moment Coefficient*Reference Area*Wingspan). Here is an example- 0.660244 = 5.4/(1.4*5.08*1.15).

How to calculate Wing Dynamic Pressure for given Yawing Moment Coefficient?

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

What are the other ways to Calculate Wing Dynamic Pressure?

Here are the different ways to Calculate Wing Dynamic Pressure-

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

Can the Wing Dynamic Pressure for given Yawing Moment Coefficient be negative?

No, the Wing Dynamic Pressure for given Yawing Moment Coefficient, measured in Pressure cannot be negative.

Which unit is used to measure Wing Dynamic Pressure for given Yawing Moment Coefficient?

Wing Dynamic Pressure for given Yawing Moment Coefficient is usually measured using the Pascal[Pa] for Pressure. Kilopascal[Pa], Bar[Pa], Pound Per Square Inch[Pa] are the few other units in which Wing Dynamic Pressure for given Yawing Moment Coefficient can be measured.

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Wing Dynamic Pressure for given Yawing Moment Coefficient Formula

​GoDynamic Pressure at Wing for given Yawing Moment Coefficient Formula

​GoDynamic Pressure at Wing for given Vertical Tail Efficiency Formula

Wing Dynamic Pressure for given Yawing Moment Coefficient Example

Wing Dynamic Pressure for given Yawing Moment Coefficient Solution

Wing Dynamic Pressure for given Yawing Moment Coefficient Formula Elements

Other Formulas to find Wing Dynamic Pressure

Other formulas in Wing Tail Interaction category

How to Evaluate Wing Dynamic Pressure for given Yawing Moment Coefficient?

FAQs on Wing Dynamic Pressure for given Yawing Moment Coefficient

Variable Name

GoDynamic Pressure at Wing for given Yawing Moment Coefficient Formula

GoDynamic Pressure at Wing for given Vertical Tail Efficiency Formula