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Dynamic Pressure at Wing for given Vertical Tail Efficiency Formula

GoWing Dynamic Pressure for given Yawing Moment Coefficient Formula

GoDynamic Pressure at Wing for given Yawing Moment Coefficient Formula

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

Q w = \frac{Q v}{η v}

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

Dynamic Pressure at Wing for given Vertical Tail Efficiency Example

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

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

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

0.6603 = \frac{11}{16.66}

0.6603Pa = \frac{11Pa}{16.66}

0.6603 = \frac{11}{16.66}

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Dynamic Pressure at Wing for given Vertical Tail Efficiency Solution

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

FIRST Step Consider the formula

Q w = \frac{Q v}{η v}

Next Step Substitute values of Variables

∴

Q w = \frac{11Pa}{16.66}

Next Step Prepare to Evaluate

∴

Q w = \frac{11}{16.66}

Next Step Evaluate

∴

Q w = 0.660264105642257Pa

LAST Step Rounding Answer

∴

Q w = 0.6603Pa

Dynamic Pressure at Wing for given Vertical Tail Efficiency 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 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

Other Formulas to find Wing Dynamic Pressure

Go Wing Dynamic Pressure for given Yawing Moment Coefficient

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

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 Dynamic Pressure at Wing for given Vertical Tail Efficiency?

Dynamic Pressure at Wing for given Vertical Tail Efficiency evaluator uses Wing Dynamic Pressure = Vertical Tail Dynamic Pressure/Vertical Tail Efficiency to evaluate the Wing Dynamic Pressure, Dynamic Pressure at Wing for given Vertical Tail Efficiency is the measure of the pressure exerted on an aircraft's wing, calculated by dividing the vertical tail's dynamic pressure by its efficiency, which determines the wing's ability to generate lift and stability during flight. Wing Dynamic Pressure is denoted by Q_w symbol.

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

FAQs on Dynamic Pressure at Wing for given Vertical Tail Efficiency

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

The formula of Dynamic Pressure at Wing for given Vertical Tail Efficiency is expressed as Wing Dynamic Pressure = Vertical Tail Dynamic Pressure/Vertical Tail Efficiency. Here is an example- 0.660264 = 11/16.66.

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

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

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/(Yawing Moment Coefficient*Reference Area*Wingspan)
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)

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

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

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

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

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: Value
: Unit

Dynamic Pressure at Wing for given Vertical Tail Efficiency Formula

​GoWing Dynamic Pressure for given Yawing Moment Coefficient Formula

​GoDynamic Pressure at Wing for given Yawing Moment Coefficient Formula

Dynamic Pressure at Wing for given Vertical Tail Efficiency Example

Dynamic Pressure at Wing for given Vertical Tail Efficiency Solution

Dynamic Pressure at Wing for given Vertical Tail Efficiency Formula Elements

Other Formulas to find Wing Dynamic Pressure

Other formulas in Wing Tail Interaction category

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

FAQs on Dynamic Pressure at Wing for given Vertical Tail Efficiency

Variable Name

GoWing Dynamic Pressure for given Yawing Moment Coefficient Formula

GoDynamic Pressure at Wing for given Yawing Moment Coefficient Formula