Tangential Velocity of Cylinder with Lift Coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Tangential Velocity of Cylinder in Fluid = (Lift Coefficient for Rotating Cylinder*Freestream Velocity of Fluid)/(2*pi)
vt = (C'*V)/(2*pi)
This formula uses 1 Constants, 3 Variables
Constants Used
pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288
Variables Used
Tangential Velocity of Cylinder in Fluid - (Measured in Meter per Second) - Tangential Velocity of Cylinder in Fluid is the speed of the periphery of the cylinder rotating in the flowing fluid.
Lift Coefficient for Rotating Cylinder - Lift Coefficient for rotating cylinder relates the lift generated, fluid density around the cylinder, the fluid velocity, and an associated reference area.
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.
STEP 1: Convert Input(s) to Base Unit
Lift Coefficient for Rotating Cylinder: 12.55 --> No Conversion Required
Freestream Velocity of Fluid: 21.5 Meter per Second --> 21.5 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
vt = (C'*V)/(2*pi) --> (12.55*21.5)/(2*pi)
Evaluating ... ...
vt = 42.9439825197707
STEP 3: Convert Result to Output's Unit
42.9439825197707 Meter per Second --> No Conversion Required
FINAL ANSWER
42.9439825197707 42.94398 Meter per Second <-- Tangential Velocity of Cylinder in Fluid
(Calculation completed in 00.020 seconds)

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PSG College of Technology (PSGCT), Coimbatore
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Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
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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)

Tangential Velocity of Cylinder with Lift Coefficient Formula

​LaTeX ​Go
Tangential Velocity of Cylinder in Fluid = (Lift Coefficient for Rotating Cylinder*Freestream Velocity of Fluid)/(2*pi)
vt = (C'*V)/(2*pi)

What is meant by tangential velocity?

Tangential velocity is the linear speed of any object moving along a circular path. A point on the outside edge of a turntable moves a greater distance in one complete rotation than a point near to the center.

What is lift coefficient?

The lift coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity, and an associated reference area.

How to Calculate Tangential Velocity of Cylinder with Lift Coefficient?

Tangential Velocity of Cylinder with Lift Coefficient calculator uses Tangential Velocity of Cylinder in Fluid = (Lift Coefficient for Rotating Cylinder*Freestream Velocity of Fluid)/(2*pi) to calculate the Tangential Velocity of Cylinder in Fluid, The Tangential velocity of cylinder with lift coefficient formula is known while considering the terms lift coefficient and the freestream velocity. Tangential Velocity of Cylinder in Fluid is denoted by vt symbol.

How to calculate Tangential Velocity of Cylinder with Lift Coefficient using this online calculator? To use this online calculator for Tangential Velocity of Cylinder with Lift Coefficient, enter Lift Coefficient for Rotating Cylinder (C') & Freestream Velocity of Fluid (V) and hit the calculate button. Here is how the Tangential Velocity of Cylinder with Lift Coefficient calculation can be explained with given input values -> 42.94398 = (12.55*21.5)/(2*pi).

FAQ

What is Tangential Velocity of Cylinder with Lift Coefficient?
The Tangential velocity of cylinder with lift coefficient formula is known while considering the terms lift coefficient and the freestream velocity and is represented as vt = (C'*V)/(2*pi) or Tangential Velocity of Cylinder in Fluid = (Lift Coefficient for Rotating Cylinder*Freestream Velocity of Fluid)/(2*pi). Lift Coefficient for rotating cylinder relates the lift generated, fluid density around the cylinder, the fluid velocity, and an associated reference area & 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.
How to calculate Tangential Velocity of Cylinder with Lift Coefficient?
The Tangential velocity of cylinder with lift coefficient formula is known while considering the terms lift coefficient and the freestream velocity is calculated using Tangential Velocity of Cylinder in Fluid = (Lift Coefficient for Rotating Cylinder*Freestream Velocity of Fluid)/(2*pi). To calculate Tangential Velocity of Cylinder with Lift Coefficient, you need Lift Coefficient for Rotating Cylinder (C') & Freestream Velocity of Fluid (V). With our tool, you need to enter the respective value for Lift Coefficient for Rotating Cylinder & Freestream Velocity of Fluid and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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