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Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Formula

GoVertical Tail Dynamic Pressure for given Moment Formula

GoDynamic Pressure at Vertical Tail for given Yawing Moment Coefficient Formula

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Vertical Tail Dynamic Pressure is the dynamic pressure associated with the vertical tail of an aircraft. Check FAQs

Q v = η v \cdot Q w

Q_v - Vertical Tail Dynamic Pressure?η_v - Vertical Tail Efficiency?Q_w - Wing Dynamic Pressure?

Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Example

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Here is how the Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency equation looks like with Values.

Here is how the Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency equation looks like with Units.

Here is how the Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency equation looks like.

10.9956 = 16.66 \cdot 0.66

10.9956Pa = 16.66 \cdot 0.66Pa

10.9956 = 16.66 \cdot 0.66

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Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Solution

Follow our step by step solution on how to calculate Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency?

FIRST Step Consider the formula

Q v = η v \cdot Q w

Next Step Substitute values of Variables

∴

Q v = 16.66 \cdot 0.66Pa

Next Step Prepare to Evaluate

∴

Q v = 16.66 \cdot 0.66

LAST Step Evaluate

∴

Q v = 10.9956Pa

Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Formula Elements

Variables

Vertical Tail Dynamic Pressure

Vertical Tail Dynamic Pressure is the dynamic pressure associated with the vertical tail of an aircraft.

Symbol: Q_v

Measurement: PressureUnit: Pa

Note: Value should be greater than 0.

Formulas to find Vertical Tail Dynamic Pressure

Vertical Tail Efficiency

Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft.

Symbol: η_v

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Vertical Tail Efficiency

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 Vertical Tail Dynamic Pressure

Go Vertical Tail Dynamic Pressure for given Moment

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

Go Dynamic Pressure at Vertical Tail for given Yawing Moment Coefficient

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

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 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}

How to Evaluate Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency?

Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency evaluator uses Vertical Tail Dynamic Pressure = Vertical Tail Efficiency*Wing Dynamic Pressure to evaluate the Vertical Tail Dynamic Pressure, Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency is a measure of the pressure exerted by the air flowing over the vertical tail of an aircraft, influenced by the efficiency of the vertical tail and the dynamic pressure of the wing, it is an important factor in determining the stability and control of the aircraft during flight, the formula calculates this pressure based on the vertical tail efficiency and wing dynamic pressure, providing a critical input for aircraft design and performance analysis. Vertical Tail Dynamic Pressure is denoted by Q_v symbol.

How to evaluate Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency using this online evaluator? To use this online evaluator for Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency, enter Vertical Tail Efficiency (η_v) & Wing Dynamic Pressure (Q_w) and hit the calculate button.

FAQs on Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency

What is the formula to find Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency?

The formula of Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency is expressed as Vertical Tail Dynamic Pressure = Vertical Tail Efficiency*Wing Dynamic Pressure. Here is an example- 10.9956 = 16.66*0.66.

How to calculate Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency?

With Vertical Tail Efficiency (η_v) & Wing Dynamic Pressure (Q_w) we can find Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency using the formula - Vertical Tail Dynamic Pressure = Vertical Tail Efficiency*Wing Dynamic Pressure.

What are the other ways to Calculate Vertical Tail Dynamic Pressure?

Here are the different ways to Calculate Vertical Tail Dynamic Pressure-

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

Can the Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency be negative?

No, the Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency, measured in Pressure cannot be negative.

Which unit is used to measure Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency?

Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency 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 Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency can be measured.

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Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Formula

​GoVertical Tail Dynamic Pressure for given Moment Formula

​GoDynamic Pressure at Vertical Tail for given Yawing Moment Coefficient Formula

Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Example

Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Solution

Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Formula Elements

Other Formulas to find Vertical Tail Dynamic Pressure

Other formulas in Wing Tail Interaction category

How to Evaluate Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency?

FAQs on Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency

Variable Name

GoVertical Tail Dynamic Pressure for given Moment Formula

GoDynamic Pressure at Vertical Tail for given Yawing Moment Coefficient Formula