FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Circulation by Kutta-Joukowski Theorem Formula

Fx Copy

LaTeX Copy

Vortex Strength quantifies the intensity or magnitude of a vortex in fluid dynamics. Check FAQs

Γ = \frac{L'}{ρ ∞ \cdot V ∞}

Γ - Vortex Strength?L' - Lift per Unit Span?ρ_∞ - Freestream Density?V_∞ - Freestream Velocity?

Circulation by Kutta-Joukowski Theorem Example

With values

With units

Only example

Here is how the Circulation by Kutta-Joukowski Theorem equation looks like with Values.

Here is how the Circulation by Kutta-Joukowski Theorem equation looks like with Units.

Here is how the Circulation by Kutta-Joukowski Theorem equation looks like.

0.698 = \frac{5.9}{1.225 \cdot 6.9}

0.698m²/s = \frac{5.9N/m}{1.225kg/m³ \cdot 6.9m/s}

0.698 = \frac{5.9}{1.225 \cdot 6.9}

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Aerospace » Category

Aerodynamics » fx Circulation by Kutta-Joukowski Theorem

Circulation by Kutta-Joukowski Theorem Solution

Follow our step by step solution on how to calculate Circulation by Kutta-Joukowski Theorem?

FIRST Step Consider the formula

Γ = \frac{L'}{ρ ∞ \cdot V ∞}

Next Step Substitute values of Variables

∴

Γ = \frac{5.9N/m}{1.225kg/m³ \cdot 6.9m/s}

Next Step Prepare to Evaluate

∴

Γ = \frac{5.9}{1.225 \cdot 6.9}

Next Step Evaluate

∴

Γ = 0.698018337769891m²/s

LAST Step Rounding Answer

∴

Γ = 0.698m²/s

Circulation by Kutta-Joukowski Theorem Formula Elements

Variables

Vortex Strength

Vortex Strength quantifies the intensity or magnitude of a vortex in fluid dynamics.

Symbol: Γ

Measurement: Velocity PotentialUnit: m²/s

Note: Value can be positive or negative.

Formulas to find Vortex Strength

Lift per Unit Span

Lift per Unit Span is defined for a two-dimensional body. The lift is the component of resultant force (caused by pressure and shear stress distribution) perpendicular to the freestream velocity.

Symbol: L'

Measurement: Surface TensionUnit: N/m

Note: Value can be positive or negative.

Formulas to find Lift per Unit Span

Freestream Density

Freestream Density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude.

Symbol: ρ_∞

Measurement: DensityUnit: kg/m³

Note: Value can be positive or negative.

Formulas to find Freestream Density

Freestream Velocity

The Freestream Velocity signifies the speed or velocity of a fluid flow far from any disturbances or obstacles.

Symbol: V_∞

Measurement: SpeedUnit: m/s

Note: Value can be positive or negative.

Formulas to find Freestream Velocity

Other formulas in Kutta Joukowski Lift Theorem category

Go Lift Per Unit Span by Kutta-Joukowski Theorem

L' = ρ ∞ \cdot V ∞ \cdot Γ

Go Freestream Velocity by Kutta-Joukowski Theorem

V ∞ = \frac{L'}{ρ ∞ \cdot Γ}

Go Freestream Density by Kutta-Joukowski Theorem

ρ ∞ = \frac{L'}{V ∞ \cdot Γ}

How to Evaluate Circulation by Kutta-Joukowski Theorem?

Circulation by Kutta-Joukowski Theorem evaluator uses Vortex Strength = Lift per Unit Span/(Freestream Density*Freestream Velocity) to evaluate the Vortex Strength, The Circulation by Kutta-Joukowski theorem formula is defined as the function of freestream velocity, lift per unit span and freestream density. The strength of the vortex is circulation. Vortex Strength is denoted by Γ symbol.

How to evaluate Circulation by Kutta-Joukowski Theorem using this online evaluator? To use this online evaluator for Circulation by Kutta-Joukowski Theorem, enter Lift per Unit Span (L'), Freestream Density (ρ_∞) & Freestream Velocity (V_∞) and hit the calculate button.

FAQs on Circulation by Kutta-Joukowski Theorem

What is the formula to find Circulation by Kutta-Joukowski Theorem?

The formula of Circulation by Kutta-Joukowski Theorem is expressed as Vortex Strength = Lift per Unit Span/(Freestream Density*Freestream Velocity). Here is an example- 128.1159 = 5.9/(1.225*6.9).

How to calculate Circulation by Kutta-Joukowski Theorem?

With Lift per Unit Span (L'), Freestream Density (ρ_∞) & Freestream Velocity (V_∞) we can find Circulation by Kutta-Joukowski Theorem using the formula - Vortex Strength = Lift per Unit Span/(Freestream Density*Freestream Velocity).

Can the Circulation by Kutta-Joukowski Theorem be negative?

Yes, the Circulation by Kutta-Joukowski Theorem, measured in Velocity Potential can be negative.

Which unit is used to measure Circulation by Kutta-Joukowski Theorem?

Circulation by Kutta-Joukowski Theorem is usually measured using the Square Meter per Second[m²/s] for Velocity Potential. are the few other units in which Circulation by Kutta-Joukowski Theorem can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

Circulation by Kutta-Joukowski Theorem Formula

Circulation by Kutta-Joukowski Theorem Example

Circulation by Kutta-Joukowski Theorem Solution

Circulation by Kutta-Joukowski Theorem Formula Elements

Other formulas in Kutta Joukowski Lift Theorem category

How to Evaluate Circulation by Kutta-Joukowski Theorem?

FAQs on Circulation by Kutta-Joukowski Theorem

Variable Name