Lift of a Rotating Cylinder in Inviscid Flow

In summary, the conversation discusses the generation of lift in an inviscid flow around a spinning cylinder. While the no slip condition only applies to viscous fluids, simulations show that there is still lift in an inviscid flow. This is due to the use of a point vortex, which approximates the effect of viscosity. The NASA simulation also explains that the ideal flow field used in the simulation is a combination of an ideal vortex and a uniform free stream flow, with no viscosity present. This breaks the symmetry of the flow and creates a difference in velocity, resulting in lift.
  • #1
Red_CCF
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Hi

I am wondering why a spinning cylinder will produce lift in an inviscid flow. From:
http://www.grc.nasa.gov/WWW/k-12/airplane/cyl.html

one of the mechanisms for lift generation was the sticking of fluid particles to the wall of the cylinder. I thought that the no slip condition only applies to viscous fluids so if the fluid was inviscid I don't see how lift can be generated. However, in the simulations in the link, the flow was simulated inviscid yet there is lift, why is this?

Thanks
 
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  • #2
In a truly inviscid flow it won't. When one analyzes a rotating cylinder with potential flow, one is essentially approximating the effect of viscosity through the use of a point vortex.
 
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  • #3
boneh3ad said:
In a truly inviscid flow it won't. When one analyzes a rotating cylinder with potential flow, one is essentially approximating the effect of viscosity through the use of a point vortex.

Hi

Thanks for the response.

Can you briefly describe what point vortex are? I was never introduced this.

And just to confirm, in the NASA simulation at http://www.grc.nasa.gov/WWW/k-12/airplane/cyl.html they state

This type of flow field is called an ideal flow field. It is produced by superimposing the flow field from an ideal vortex centered in the cylinder with a uniform free stream flow. There is no viscosity in this model (no boundary layer on the cylinder) even though this is the real origin of the circulating flow!

and is the reason that the simulation still shows lift when the cylinder spins because the supposed effect of viscosity is superimposed mathematically to the effect of the flow in the simulation that has no viscosity or boundary layer?

Thanks very much
 
  • #4
You essentially insert manually the fluid rotation that viscosity would have caused. This breaks the symmetry of the flow, making flow on one side of the cylinder faster than the flow on the other one. Velocity is linked to pressure, which is what creates your lift.
 
  • #5
for your question! The concept of lift generation on a spinning cylinder in an inviscid flow can seem counterintuitive at first. However, it is important to understand that lift is not solely dependent on the no-slip condition between the fluid and the surface.

In inviscid flow, there is no friction between the fluid particles and the surface of the cylinder. However, there is still the presence of pressure gradients and circulation around the cylinder due to its rotation. This circulation creates a pressure difference between the upper and lower surfaces of the cylinder, resulting in a net upward force, or lift. This is known as the Magnus effect.

The sticking of fluid particles to the wall of the cylinder is one mechanism for generating lift, but it is not the only mechanism. In inviscid flow, the generation of lift is primarily due to the creation of pressure gradients and circulation, as described above.

The simulations in the link you provided likely take into account the effects of circulation and pressure gradients in the inviscid flow, which result in lift on the spinning cylinder. I hope this helps to clarify the concept of lift generation in an inviscid flow on a rotating cylinder.
 

1. What is the significance of studying the lift of a rotating cylinder in inviscid flow?

The study of lift on a rotating cylinder in inviscid flow is important for understanding the aerodynamics of rotating bodies, which has applications in various fields such as aircraft and wind turbine design. It can also provide insights into the behavior of fluids in the presence of rotating objects.

2. How does the lift on a rotating cylinder change with different rotational speeds?

The lift on a rotating cylinder in inviscid flow is directly proportional to the angular velocity of the cylinder. This means that as the rotational speed increases, the lift force also increases. However, at very high rotational speeds, the lift may not increase proportionally due to the formation of vortices and other complex flow phenomena.

3. What is the difference between lift on a rotating cylinder and a stationary cylinder in inviscid flow?

The main difference is that a rotating cylinder experiences a lift force perpendicular to the direction of the flow, while a stationary cylinder does not experience any lift. This is because the rotation of the cylinder creates a pressure gradient that results in a lift force.

4. How does the lift on a rotating cylinder change with different cylinder shapes?

The lift on a rotating cylinder is influenced by its shape, specifically the diameter and length. Generally, a longer and thinner cylinder will experience a higher lift force compared to a shorter and wider cylinder. This is due to the formation of a larger pressure gradient and vortices around the cylinder.

5. Can the lift on a rotating cylinder in inviscid flow be calculated accurately?

The lift on a rotating cylinder in inviscid flow can be calculated accurately using theoretical models and computational fluid dynamics simulations. However, these calculations may not account for real-world factors such as turbulence and surface roughness, which can affect the accuracy of the results. Experimental data may also be necessary for validation and to account for any discrepancies.

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