Radius of Cylinder for Lifting Flow Solution

STEP 0: Pre-Calculation Summary
Formula Used
Cylinder Radius = Vortex Strength/(Lift Coefficient*Freestream Velocity)
R = Γ/(CL*V)
This formula uses 4 Variables
Variables Used
Cylinder Radius - (Measured in Meter) - The Cylinder Radius is the radius of its circular cross section.
Vortex Strength - (Measured in Square Meter per Second) - Vortex Strength quantifies the intensity or magnitude of a vortex in fluid dynamics.
Lift Coefficient - Lift Coefficient is a dimensionless coefficient that relates the lift generated per unit span by a lifting body to the fluid density around the body, the fluid velocity & reference area.
Freestream Velocity - (Measured in Meter per Second) - The Freestream Velocity signifies the speed or velocity of a fluid flow far from any disturbances or obstacles.
STEP 1: Convert Input(s) to Base Unit
Vortex Strength: 0.7 Square Meter per Second --> 0.7 Square Meter per Second No Conversion Required
Lift Coefficient: 1.2 --> No Conversion Required
Freestream Velocity: 6.9 Meter per Second --> 6.9 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
R = Γ/(CL*V) --> 0.7/(1.2*6.9)
Evaluating ... ...
R = 0.0845410628019324
STEP 3: Convert Result to Output's Unit
0.0845410628019324 Meter --> No Conversion Required
FINAL ANSWER
0.0845410628019324 0.084541 Meter <-- Cylinder Radius
(Calculation completed in 00.004 seconds)

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Created by Harsh Raj
Indian Institute of Technology, Kharagpur (IIT KGP), West Bengal
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Lifting Flow over Cylinder Calculators

Surface Pressure Coefficient for Lifting Flow over Circular Cylinder
​ Go Surface Pressure Coefficient = 1-((2*sin(Polar Angle))^2+(2*Vortex Strength*sin(Polar Angle))/(pi*Cylinder Radius*Freestream Velocity)+((Vortex Strength)/(2*pi*Cylinder Radius*Freestream Velocity))^2)
Stream Function for Lifting Flow over Circular Cylinder
​ Go Stream Function = Freestream Velocity*Radial Coordinate*sin(Polar Angle)*(1-(Cylinder Radius/Radial Coordinate)^2)+Vortex Strength/(2*pi)*ln(Radial Coordinate/Cylinder Radius)
Tangential Velocity for Lifting Flow over Circular Cylinder
​ Go Tangential Velocity = -(1+((Cylinder Radius)/(Radial Coordinate))^2)*Freestream Velocity*sin(Polar Angle)-(Vortex Strength)/(2*pi*Radial Coordinate)
Radial Velocity for Lifting Flow over Circular Cylinder
​ Go Radial Velocity = (1-(Cylinder Radius/Radial Coordinate)^2)*Freestream Velocity*cos(Polar Angle)

Radius of Cylinder for Lifting Flow Formula

​Go
Cylinder Radius = Vortex Strength/(Lift Coefficient*Freestream Velocity)
R = Γ/(CL*V)

Can you compare lift and drag on the spinning cylinder and wing of same planform area?

The lift on the spinning cylinder is higher than an airplane wing of the same planform area however the drag on the spinning cylinder is also much higher than the well-designed wing.

How to Calculate Radius of Cylinder for Lifting Flow?

Radius of Cylinder for Lifting Flow calculator uses Cylinder Radius = Vortex Strength/(Lift Coefficient*Freestream Velocity) to calculate the Cylinder Radius, Radius of Cylinder for Lifting Flow formula is defined as a measure that relates the circulation around a cylinder to the lift coefficient and the velocity of the flow, helping to analyze aerodynamic performance in lifting scenarios. Cylinder Radius is denoted by R symbol.

How to calculate Radius of Cylinder for Lifting Flow using this online calculator? To use this online calculator for Radius of Cylinder for Lifting Flow, enter Vortex Strength (Γ), Lift Coefficient (CL) & Freestream Velocity (V) and hit the calculate button. Here is how the Radius of Cylinder for Lifting Flow calculation can be explained with given input values -> 1.570048 = 0.7/(1.2*6.9).

FAQ

What is Radius of Cylinder for Lifting Flow?
Radius of Cylinder for Lifting Flow formula is defined as a measure that relates the circulation around a cylinder to the lift coefficient and the velocity of the flow, helping to analyze aerodynamic performance in lifting scenarios and is represented as R = Γ/(CL*V) or Cylinder Radius = Vortex Strength/(Lift Coefficient*Freestream Velocity). Vortex Strength quantifies the intensity or magnitude of a vortex in fluid dynamics, Lift Coefficient is a dimensionless coefficient that relates the lift generated per unit span by a lifting body to the fluid density around the body, the fluid velocity & reference area & The Freestream Velocity signifies the speed or velocity of a fluid flow far from any disturbances or obstacles.
How to calculate Radius of Cylinder for Lifting Flow?
Radius of Cylinder for Lifting Flow formula is defined as a measure that relates the circulation around a cylinder to the lift coefficient and the velocity of the flow, helping to analyze aerodynamic performance in lifting scenarios is calculated using Cylinder Radius = Vortex Strength/(Lift Coefficient*Freestream Velocity). To calculate Radius of Cylinder for Lifting Flow, you need Vortex Strength (Γ), Lift Coefficient (CL) & Freestream Velocity (V). With our tool, you need to enter the respective value for Vortex Strength, Lift Coefficient & Freestream Velocity 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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