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Side force coefficient Formula

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Side Force Coefficient is the dimensionless coefficient associated with the component of aerodynamic forces along the pitch axis on an aircraft. Check FAQs

C y = \frac{Y}{q \cdot S}

C_y - Side Force Coefficient?Y - Aerodynamic Side Force?q - Dynamic Pressure?S - Reference Area?

Side force coefficient Example

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Here is how the Side force coefficient equation looks like with Values.

Here is how the Side force coefficient equation looks like with Units.

Here is how the Side force coefficient equation looks like.

0.748 = \frac{38}{10 \cdot 5.08}

0.748 = \frac{38N}{10Pa \cdot 5.08m²}

0.748 = \frac{38}{10 \cdot 5.08}

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Side force coefficient Solution

Follow our step by step solution on how to calculate Side force coefficient?

FIRST Step Consider the formula

C y = \frac{Y}{q \cdot S}

Next Step Substitute values of Variables

∴

C y = \frac{38N}{10Pa \cdot 5.08m²}

Next Step Prepare to Evaluate

∴

C y = \frac{38}{10 \cdot 5.08}

Next Step Evaluate

∴

C y = 0.748031496062992

LAST Step Rounding Answer

∴

C y = 0.748

Side force coefficient Formula Elements

Variables

Side Force Coefficient

Side Force Coefficient is the dimensionless coefficient associated with the component of aerodynamic forces along the pitch axis on an aircraft.

Symbol: C_y

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Side Force Coefficient

Aerodynamic Side Force

Aerodynamic Side Force is the component of aerodynamic force along the pitch axis of an aircraft.

Symbol: Y

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Aerodynamic Side Force

Dynamic Pressure

Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.

Symbol: q

Measurement: PressureUnit: Pa

Note: Value should be greater than 0.

Formulas to find 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

Other formulas in Aircraft Dynamics Nomenclature category

Go Aerodynamic Axial Force

X = C x \cdot q \cdot S

Go Aerodynamic Side Force

Y = C y \cdot q \cdot S

Go Aerodynamic Normal Force

Z = C z \cdot q \cdot S

Go Normal Force Coefficient with Aerodynamic Normal Force

C z = \frac{Z}{q \cdot S}

How to Evaluate Side force coefficient?

Side force coefficient evaluator uses Side Force Coefficient = Aerodynamic Side Force/(Dynamic Pressure*Reference Area) to evaluate the Side Force Coefficient, The side force coefficient is a dimensionless quantity that characterizes the lift force generated by an object, typically an airfoil or wing, as it moves through a fluid, such as air or water, and is a critical parameter in aerodynamics and hydrodynamics. Side Force Coefficient is denoted by C_y symbol.

How to evaluate Side force coefficient using this online evaluator? To use this online evaluator for Side force coefficient, enter Aerodynamic Side Force (Y), Dynamic Pressure (q) & Reference Area (S) and hit the calculate button.

FAQs on Side force coefficient

What is the formula to find Side force coefficient?

The formula of Side force coefficient is expressed as Side Force Coefficient = Aerodynamic Side Force/(Dynamic Pressure*Reference Area). Here is an example- 0.748031 = 38/(10*5.08).

How to calculate Side force coefficient?

With Aerodynamic Side Force (Y), Dynamic Pressure (q) & Reference Area (S) we can find Side force coefficient using the formula - Side Force Coefficient = Aerodynamic Side Force/(Dynamic Pressure*Reference Area).

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