Circulation for Single Stagnation Point Solution

STEP 0: Pre-Calculation Summary
Formula Used
Circulation Around Cylinder = 4*pi*Freestream Velocity of Fluid*Radius of Rotating Cylinder
Γc = 4*pi*V*R
This formula uses 1 Constants, 3 Variables
Constants Used
pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288
Variables Used
Circulation Around Cylinder - (Measured in Square Meter per Second) - Circulation around Cylinder is a macroscopic measure of rotation for a finite area of the fluid around a rotating cylinder.
Freestream Velocity of Fluid - (Measured in Meter per Second) - Freestream Velocity of Fluid is the velocity of fluid far upstream of a body, that is before the body has a chance to deflect, slow down, or compress the fluid.
Radius of Rotating Cylinder - (Measured in Meter) - Radius of Rotating Cylinder is the radius of the cylinder rotating between the flowing fluid.
STEP 1: Convert Input(s) to Base Unit
Freestream Velocity of Fluid: 21.5 Meter per Second --> 21.5 Meter per Second No Conversion Required
Radius of Rotating Cylinder: 0.9 Meter --> 0.9 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Γc = 4*pi*V*R --> 4*pi*21.5*0.9
Evaluating ... ...
Γc = 243.15927138785
STEP 3: Convert Result to Output's Unit
243.15927138785 Square Meter per Second --> No Conversion Required
FINAL ANSWER
243.15927138785 243.1593 Square Meter per Second <-- Circulation Around Cylinder
(Calculation completed in 00.020 seconds)

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Created by Maiarutselvan V
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Amrita School of Engineering (ASE), Vallikavu
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Lift and Circulation Calculators

Angle of Attack for Circulation developed on Airfoil
​ LaTeX ​ Go Angle of Attack on Airfoil = asin(Circulation on Airfoil/(pi*Velocity of Airfoil*Chord Length of Airfoil))
Chord Length for Circulation developed on Airfoil
​ LaTeX ​ Go Chord Length of Airfoil = Circulation on Airfoil/(pi*Velocity of Airfoil*sin(Angle of Attack on Airfoil))
Circulation developed on Airfoil
​ LaTeX ​ Go Circulation on Airfoil = pi*Velocity of Airfoil*Chord Length of Airfoil*sin(Angle of Attack on Airfoil)
Coefficient of Lift for Airfoil
​ LaTeX ​ Go Lift Coefficient for Airfoil = 2*pi*sin(Angle of Attack on Airfoil)

Circulation for Single Stagnation Point Formula

​LaTeX ​Go
Circulation Around Cylinder = 4*pi*Freestream Velocity of Fluid*Radius of Rotating Cylinder
Γc = 4*pi*V*R

What is a stagnation point?

In fluid dynamics, a stagnation point is a point in a flow field where the local velocity of the fluid is zero. Stagnation points exist at the surface of objects in the flow field, where the fluid is brought to rest by the object.

What is circulation in fluid mechanics?

In physics, circulation is the line integral of a vector field around a closed curve. In fluid dynamics, the field is the fluid velocity field. In electrodynamics, it can be the electric or the magnetic field.

How to Calculate Circulation for Single Stagnation Point?

Circulation for Single Stagnation Point calculator uses Circulation Around Cylinder = 4*pi*Freestream Velocity of Fluid*Radius of Rotating Cylinder to calculate the Circulation Around Cylinder, The Circulation for single stagnation point formula is known while considering the terms freestream velocity and the radius of the cylinder. Circulation Around Cylinder is denoted by Γc symbol.

How to calculate Circulation for Single Stagnation Point using this online calculator? To use this online calculator for Circulation for Single Stagnation Point, enter Freestream Velocity of Fluid (V) & Radius of Rotating Cylinder (R) and hit the calculate button. Here is how the Circulation for Single Stagnation Point calculation can be explained with given input values -> 243.1593 = 4*pi*21.5*0.9.

FAQ

What is Circulation for Single Stagnation Point?
The Circulation for single stagnation point formula is known while considering the terms freestream velocity and the radius of the cylinder and is represented as Γc = 4*pi*V*R or Circulation Around Cylinder = 4*pi*Freestream Velocity of Fluid*Radius of Rotating Cylinder. Freestream Velocity of Fluid is the velocity of fluid far upstream of a body, that is before the body has a chance to deflect, slow down, or compress the fluid & Radius of Rotating Cylinder is the radius of the cylinder rotating between the flowing fluid.
How to calculate Circulation for Single Stagnation Point?
The Circulation for single stagnation point formula is known while considering the terms freestream velocity and the radius of the cylinder is calculated using Circulation Around Cylinder = 4*pi*Freestream Velocity of Fluid*Radius of Rotating Cylinder. To calculate Circulation for Single Stagnation Point, you need Freestream Velocity of Fluid (V) & Radius of Rotating Cylinder (R). With our tool, you need to enter the respective value for Freestream Velocity of Fluid & Radius of Rotating Cylinder and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Circulation Around Cylinder?
In this formula, Circulation Around Cylinder uses Freestream Velocity of Fluid & Radius of Rotating Cylinder. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Circulation Around Cylinder = -(sin(Angle at Stagnation Point))*4*pi*Freestream Velocity of Fluid*Radius of Rotating Cylinder
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