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Vertical Tail Angle of Attack for given Vertical Tail Side Force Formula

GoVertical Tail Angle of Attack Formula

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Vertical Tail Angle of Attack is the angle of attack experienced by the vertical tailplane of an aircraft. Check FAQs

α v = - (\frac{Y v}{C v \cdot Q v \cdot S v})

α_v - Vertical Tail Angle of Attack?Y_v - Vertical Tail Side Force?C_v - Vertical Tail Lift Curve Slope?Q_v - Vertical Tail Dynamic Pressure?S_v - Vertical Tail Area?

Vertical Tail Angle of Attack for given Vertical Tail Side Force Example

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Here is how the Vertical Tail Angle of Attack for given Vertical Tail Side Force equation looks like with Values.

Here is how the Vertical Tail Angle of Attack for given Vertical Tail Side Force equation looks like with Units.

Here is how the Vertical Tail Angle of Attack for given Vertical Tail Side Force equation looks like.

0.11 = - (\frac{-4.235}{0.7 \cdot 11 \cdot 5})

0.11rad = - (\frac{-4.235N}{0.7rad⁻¹ \cdot 11Pa \cdot 5m²})

0.11 = - (\frac{-4.235}{0.7 \cdot 11 \cdot 5})

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Vertical Tail Angle of Attack for given Vertical Tail Side Force Solution

Follow our step by step solution on how to calculate Vertical Tail Angle of Attack for given Vertical Tail Side Force?

FIRST Step Consider the formula

α v = - (\frac{Y v}{C v \cdot Q v \cdot S v})

Next Step Substitute values of Variables

∴

α v = - (\frac{-4.235N}{0.7rad⁻¹ \cdot 11Pa \cdot 5m²})

Next Step Prepare to Evaluate

∴

α v = - (\frac{-4.235}{0.7 \cdot 11 \cdot 5})

LAST Step Evaluate

∴

α v = 0.11rad

Vertical Tail Angle of Attack for given Vertical Tail Side Force Formula Elements

Variables

Vertical Tail Angle of Attack

Vertical Tail Angle of Attack is the angle of attack experienced by the vertical tailplane of an aircraft.

Symbol: α_v

Measurement: AngleUnit: rad

Note: Value can be positive or negative.

Formulas to find Vertical Tail Angle of Attack

Vertical Tail Side Force

Vertical Tail Side Force is the side force acting on the vertical tail of an aircraft.

Symbol: Y_v

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Vertical Tail Side Force

Vertical Tail Lift Curve Slope

The Vertical Tail Lift Curve Slope is the slope associated with the lift curve of a vertical tailplane of an aircraft.

Symbol: C_v

Measurement: Reciprocal AngleUnit: rad⁻¹

Note: Value can be positive or negative.

Formulas to find Vertical Tail Lift Curve Slope

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 Area

The Vertical Tail Area is the area of the surface of the vertical tail, including the submerged area to the fuselage centerline.

Symbol: S_v

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Vertical Tail Area

Other Formulas to find Vertical Tail Angle of Attack

Go Vertical Tail Angle of Attack

α v = σ + β

Other formulas in Vertical Tail Contribution category

Go Vertical Tail Side Force

Y v = - C v \cdot α v \cdot S v \cdot Q v

Go Vertical Tail Lift Curve Slope

C v = - (\frac{Y v}{α v \cdot Q v \cdot S v})

Go Vertical Tail Dynamic Pressure for given Vertical Tail Side Force

Q v = - (\frac{Y v}{C v \cdot α v \cdot S v})

Go Vertical Tail Area for given Vertical Tail Side Force

S v = - \frac{Y v}{C v \cdot α v \cdot Q v}

How to Evaluate Vertical Tail Angle of Attack for given Vertical Tail Side Force?

Vertical Tail Angle of Attack for given Vertical Tail Side Force evaluator uses Vertical Tail Angle of Attack = -(Vertical Tail Side Force/(Vertical Tail Lift Curve Slope*Vertical Tail Dynamic Pressure*Vertical Tail Area)) to evaluate the Vertical Tail Angle of Attack, Vertical Tail Angle of Attack for given Vertical Tail Side Force is a measure of the angle at which the vertical tail of an aircraft meets the oncoming airflow, calculated by dividing the vertical tail side force by the product of the vertical tail lift curve slope, dynamic pressure, and area. This angle is critical in determining the stability and control of the aircraft during flight and is essential for ensuring safe and efficient flight operations. Vertical Tail Angle of Attack is denoted by α_v symbol.

How to evaluate Vertical Tail Angle of Attack for given Vertical Tail Side Force using this online evaluator? To use this online evaluator for Vertical Tail Angle of Attack for given Vertical Tail Side Force, enter Vertical Tail Side Force (Y_v), Vertical Tail Lift Curve Slope (C_v), Vertical Tail Dynamic Pressure (Q_v) & Vertical Tail Area (S_v) and hit the calculate button.

FAQs on Vertical Tail Angle of Attack for given Vertical Tail Side Force

What is the formula to find Vertical Tail Angle of Attack for given Vertical Tail Side Force?

The formula of Vertical Tail Angle of Attack for given Vertical Tail Side Force is expressed as Vertical Tail Angle of Attack = -(Vertical Tail Side Force/(Vertical Tail Lift Curve Slope*Vertical Tail Dynamic Pressure*Vertical Tail Area)). Here is an example- 0.11 = -((-4.235)/(0.7*11*5)).

How to calculate Vertical Tail Angle of Attack for given Vertical Tail Side Force?

With Vertical Tail Side Force (Y_v), Vertical Tail Lift Curve Slope (C_v), Vertical Tail Dynamic Pressure (Q_v) & Vertical Tail Area (S_v) we can find Vertical Tail Angle of Attack for given Vertical Tail Side Force using the formula - Vertical Tail Angle of Attack = -(Vertical Tail Side Force/(Vertical Tail Lift Curve Slope*Vertical Tail Dynamic Pressure*Vertical Tail Area)).

What are the other ways to Calculate Vertical Tail Angle of Attack?

Here are the different ways to Calculate Vertical Tail Angle of Attack-

Vertical Tail Angle of Attack=Sidewash Angle+Sideslip Angle

Can the Vertical Tail Angle of Attack for given Vertical Tail Side Force be negative?

Yes, the Vertical Tail Angle of Attack for given Vertical Tail Side Force, measured in Angle can be negative.

Which unit is used to measure Vertical Tail Angle of Attack for given Vertical Tail Side Force?

Vertical Tail Angle of Attack for given Vertical Tail Side Force is usually measured using the Radian[rad] for Angle. Degree[rad], Minute[rad], Second[rad] are the few other units in which Vertical Tail Angle of Attack for given Vertical Tail Side Force can be measured.

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Vertical Tail Angle of Attack for given Vertical Tail Side Force Formula

​GoVertical Tail Angle of Attack Formula

Vertical Tail Angle of Attack for given Vertical Tail Side Force Example

Vertical Tail Angle of Attack for given Vertical Tail Side Force Solution

Vertical Tail Angle of Attack for given Vertical Tail Side Force Formula Elements

Other Formulas to find Vertical Tail Angle of Attack

Other formulas in Vertical Tail Contribution category

How to Evaluate Vertical Tail Angle of Attack for given Vertical Tail Side Force?

FAQs on Vertical Tail Angle of Attack for given Vertical Tail Side Force

Variable Name

GoVertical Tail Angle of Attack Formula