FormulaDen.com

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

Velocity of Airfoil for Circulation developed on Airfoil Formula

Fx Copy

LaTeX Copy

The Velocity of Airfoil is the air velocity of a stream located in the airfoil where the flow has to part near the leading edge. Check FAQs

U = \frac{Γ}{π \cdot C \cdot \sin (α)}

U - Velocity of Airfoil?Γ - Circulation on Airfoil?C - Chord Length of Airfoil?α - Angle of Attack on Airfoil?π - Archimedes' constant?

Velocity of Airfoil for Circulation developed on Airfoil Example

With values

With units

Only example

Here is how the Velocity of Airfoil for Circulation developed on Airfoil equation looks like with Values.

Here is how the Velocity of Airfoil for Circulation developed on Airfoil equation looks like with Units.

Here is how the Velocity of Airfoil for Circulation developed on Airfoil equation looks like.

81.0858 = \frac{62}{3.1416 \cdot 2.15 \cdot \sin (6.5)}

81.0858m/s = \frac{62m²/s}{3.1416 \cdot 2.15m \cdot \sin (6.5°)}

81.0858 = \frac{62}{3.1416 \cdot 2.15 \cdot \sin (6.5)}

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Mechanical » Category

Fluid Mechanics » fx Velocity of Airfoil for Circulation developed on Airfoil

Velocity of Airfoil for Circulation developed on Airfoil Solution

Follow our step by step solution on how to calculate Velocity of Airfoil for Circulation developed on Airfoil?

FIRST Step Consider the formula

U = \frac{Γ}{π \cdot C \cdot \sin (α)}

Next Step Substitute values of Variables

∴

U = \frac{62m²/s}{π \cdot 2.15m \cdot \sin (6.5°)}

Next Step Substitute values of Constants

∴

U = \frac{62m²/s}{3.1416 \cdot 2.15m \cdot \sin (6.5°)}

Next Step Convert Units

∴

U = \frac{62m²/s}{3.1416 \cdot 2.15m \cdot \sin (0.1134rad)}

Next Step Prepare to Evaluate

∴

U = \frac{62}{3.1416 \cdot 2.15 \cdot \sin (0.1134)}

Next Step Evaluate

∴

U = 81.0857616613482m/s

LAST Step Rounding Answer

∴

U = 81.0858m/s

Velocity of Airfoil for Circulation developed on Airfoil Formula Elements

Variables

Constants

Functions

Velocity of Airfoil

The Velocity of Airfoil is the air velocity of a stream located in the airfoil where the flow has to part near the leading edge.

Symbol: U

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Velocity of Airfoil

Circulation on Airfoil

Circulation on Airfoil is a scalar integral quantity, and is a macroscopic measure of rotation for a finite area of the fluid around an airfoil.

Symbol: Γ

Measurement: Momentum DiffusivityUnit: m²/s

Note: Value should be greater than 0.

Formulas to find Circulation on Airfoil

Chord Length of Airfoil

Chord Length of Airfoil is an imaginary straight line joining the leading edge and trailing edge of an airfoil.

Symbol: C

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Chord Length of Airfoil

Angle of Attack on Airfoil

Angle of Attack on Airfoil is the angle between a reference line on an airfoil and the vector representing the relative motion between the airfoil and the fluid through which it is moving.

Symbol: α

Measurement: AngleUnit: °

Note: Value should be greater than 0.

Formulas to find Angle of Attack on Airfoil

Archimedes' constant

Archimedes' constant is a mathematical constant that represents the ratio of the circumference of a circle to its diameter.

Symbol: π

Value: 3.14159265358979323846264338327950288

sin

Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse.

Syntax: sin(Angle)

Other formulas in Lift and Circulation category

Go Circulation developed on Airfoil

Γ = π \cdot U \cdot C \cdot \sin (α)

Go Chord Length for Circulation developed on Airfoil

C = \frac{Γ}{π \cdot U \cdot \sin (α)}

Go Angle of Attack for Circulation developed on Airfoil

α = a \sin (\frac{Γ}{π \cdot U \cdot C})

Go Coefficient of Lift for Airfoil

C L airfoil = 2 \cdot π \cdot \sin (α)

How to Evaluate Velocity of Airfoil for Circulation developed on Airfoil?

Velocity of Airfoil for Circulation developed on Airfoil evaluator uses Velocity of Airfoil = Circulation on Airfoil/(pi*Chord Length of Airfoil*sin(Angle of Attack on Airfoil)) to evaluate the Velocity of Airfoil, The Velocity of airfoil for circulation developed on airfoil formula is known while considering the ratio of circulation to the chord length, and the angle of attack. Velocity of Airfoil is denoted by U symbol.

How to evaluate Velocity of Airfoil for Circulation developed on Airfoil using this online evaluator? To use this online evaluator for Velocity of Airfoil for Circulation developed on Airfoil, enter Circulation on Airfoil (Γ), Chord Length of Airfoil (C) & Angle of Attack on Airfoil (α) and hit the calculate button.

FAQs on Velocity of Airfoil for Circulation developed on Airfoil

What is the formula to find Velocity of Airfoil for Circulation developed on Airfoil?

The formula of Velocity of Airfoil for Circulation developed on Airfoil is expressed as Velocity of Airfoil = Circulation on Airfoil/(pi*Chord Length of Airfoil*sin(Angle of Attack on Airfoil)). Here is an example- 81.08576 = 62/(pi*2.15*sin(0.11344640137961)).

How to calculate Velocity of Airfoil for Circulation developed on Airfoil?

With Circulation on Airfoil (Γ), Chord Length of Airfoil (C) & Angle of Attack on Airfoil (α) we can find Velocity of Airfoil for Circulation developed on Airfoil using the formula - Velocity of Airfoil = Circulation on Airfoil/(pi*Chord Length of Airfoil*sin(Angle of Attack on Airfoil)). This formula also uses Archimedes' constant and Sine (sin) function(s).

Can the Velocity of Airfoil for Circulation developed on Airfoil be negative?

No, the Velocity of Airfoil for Circulation developed on Airfoil, measured in Speed cannot be negative.

Which unit is used to measure Velocity of Airfoil for Circulation developed on Airfoil?

Velocity of Airfoil for Circulation developed on Airfoil is usually measured using the Meter per Second[m/s] for Speed. Meter per Minute[m/s], Meter per Hour[m/s], Kilometer per Hour[m/s] are the few other units in which Velocity of Airfoil for Circulation developed on Airfoil can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Velocity of Airfoil for Circulation developed on Airfoil Formula

Velocity of Airfoil for Circulation developed on Airfoil Example

Velocity of Airfoil for Circulation developed on Airfoil Solution

Velocity of Airfoil for Circulation developed on Airfoil Formula Elements

Other formulas in Lift and Circulation category

How to Evaluate Velocity of Airfoil for Circulation developed on Airfoil?

FAQs on Velocity of Airfoil for Circulation developed on Airfoil

Variable Name