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Aerodynamic Normal Force Formula

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Aerodynamic Normal Force is the component of aerodynamic force along the yaw axis of an aircraft. Check FAQs

Z = C z \cdot q \cdot S

Z - Aerodynamic Normal Force?C_z - Normal Force Coefficient?q - Dynamic Pressure?S - Reference Area?

Aerodynamic Normal Force Example

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Here is how the Aerodynamic Normal Force equation looks like with Values.

Here is how the Aerodynamic Normal Force equation looks like with Units.

Here is how the Aerodynamic Normal Force equation looks like.

19.304 = 0.38 \cdot 10 \cdot 5.08

19.304N = 0.38 \cdot 10Pa \cdot 5.08m²

19.304 = 0.38 \cdot 10 \cdot 5.08

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Aerodynamic Normal Force Solution

Follow our step by step solution on how to calculate Aerodynamic Normal Force?

FIRST Step Consider the formula

Z = C z \cdot q \cdot S

Next Step Substitute values of Variables

∴

Z = 0.38 \cdot 10Pa \cdot 5.08m²

Next Step Prepare to Evaluate

∴

Z = 0.38 \cdot 10 \cdot 5.08

LAST Step Evaluate

∴

Z = 19.304N

Aerodynamic Normal Force Formula Elements

Variables

Aerodynamic Normal Force

Aerodynamic Normal Force is the component of aerodynamic force along the yaw axis of an aircraft.

Symbol: Z

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Aerodynamic Normal Force

Normal Force Coefficient

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

Symbol: C_z

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Normal Force Coefficient

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 Side force coefficient

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

Go Normal Force Coefficient with Aerodynamic Normal Force

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

How to Evaluate Aerodynamic Normal Force?

Aerodynamic Normal Force evaluator uses Aerodynamic Normal Force = Normal Force Coefficient*Dynamic Pressure*Reference Area to evaluate the Aerodynamic Normal Force, Aerodynamic Normal Force is a measure of the force exerted by the air pressure on an object, perpendicular to the surface of the object, resulting from the air's resistance to the object's motion, it is a crucial concept in aerodynamics, essential for understanding and predicting the behavior of aircraft, wind turbines, and other systems interacting with air. Aerodynamic Normal Force is denoted by Z symbol.

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

FAQs on Aerodynamic Normal Force

What is the formula to find Aerodynamic Normal Force?

The formula of Aerodynamic Normal Force is expressed as Aerodynamic Normal Force = Normal Force Coefficient*Dynamic Pressure*Reference Area. Here is an example- 19.304 = 0.38*10*5.08.

How to calculate Aerodynamic Normal Force?

With Normal Force Coefficient (C_z), Dynamic Pressure (q) & Reference Area (S) we can find Aerodynamic Normal Force using the formula - Aerodynamic Normal Force = Normal Force Coefficient*Dynamic Pressure*Reference Area.

Can the Aerodynamic Normal Force be negative?

Yes, the Aerodynamic Normal Force, measured in Force can be negative.

Which unit is used to measure Aerodynamic Normal Force?

Aerodynamic Normal Force is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Aerodynamic Normal Force can be measured.

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Aerodynamic Normal Force Formula

Aerodynamic Normal Force Example

Aerodynamic Normal Force Solution

Aerodynamic Normal Force Formula Elements

Other formulas in Aircraft Dynamics Nomenclature category

How to Evaluate Aerodynamic Normal Force?

FAQs on Aerodynamic Normal Force

Variable Name