Boundary Layer Theory: Displacement & Momentum Thickness Explained

In summary, the displacement thickness and momentum thickness of a boundary layer are measures of the effect of the boundary layer on the flow of mass and momentum in a fluid. The displacement thickness represents the distance the surface would have to be moved in order to achieve the same mass flow rate as in an inviscid case, while the momentum thickness deals with the flow of momentum and shows up in the momentum integral boundary layer equation. These measures help to understand the impact of the boundary layer on the overall flow and are important in analyzing viscous flow around objects such as a flat plate.
  • #1
mrajkumar
11
0
Hi,
could you tell the physical meaning of the displacement and momentum thickness of a boundary layer.And why the stream line diverges away from the body in the boundary layer to conserve mass?
 
  • #3
update - I wan't sure about what you meant by momentum thickness, but thanks to boneh3ad's next post, it's explained there.

Link to flat plate article:

flat plate.htm
 
Last edited:
  • #4
The convexity or concavity of the surface is irrelevant for the question at hand, and by stating that this is a question about boundary layers automatically means this is a viscous flow.

The displacement thickness (##\delta_1## or ##\delta^*##) is a measure of the effect of the boundary layer on the flow of mass in a fluid. Essentially, you can solve the flow inviscidly and come up with a certain overall mass flow rate. Then solve the same flow accounting for the boundary layer, and the mass flow will be slightly smaller. The displacement thickness is the distance the surface would have to be displaced in order that the mass flow in the inviscid case would be the same as that in the viscous case with the original wall position. In essence, it is the distance the wall must move in order to get the same outer flow (inviscid) answer without solving for the boundary layer.

[tex]\delta^* = \int\limits_0^{\infty}\left(1 - \dfrac{u}{U_{\infty}}\right)dy.[/tex]

The momentum thickness (##\delta_2## or ##\theta##) is similar, only it deals with the flow of momentum rather than mass. It shows up in the momentum integral boundary layer equation (as does ##\delta^*##).

[tex]\theta = \int\limits_0^{\infty}\dfrac{u}{U_{\infty}}\left(1 - \dfrac{u}{U_{\infty}}\right)dy[/tex]
 

What is boundary layer theory?

Boundary layer theory is a concept in fluid dynamics that describes the behavior of fluid flow near a solid surface. It specifically focuses on the thin layer of fluid that develops at the boundary between the solid surface and the rest of the fluid flow.

How is displacement thickness defined?

Displacement thickness is a measure of the distance between the original solid surface and the point at which the fluid velocity reaches its free-stream value. It represents the additional distance that the fluid particles have to travel due to the presence of the boundary layer.

What is momentum thickness?

Momentum thickness is a measure of the reduction in momentum of the fluid flow due to the presence of the boundary layer. It is defined as the integral of the difference between the free-stream velocity and the actual velocity at each point in the boundary layer.

How are displacement thickness and momentum thickness related?

Displacement and momentum thickness are related because they both represent the effects of the boundary layer on the fluid flow. However, they are measured differently and represent different aspects of the boundary layer. Displacement thickness primarily accounts for the change in shape of the flow, while momentum thickness accounts for the change in velocity.

What are some applications of boundary layer theory?

Boundary layer theory has many practical applications, including airfoil design, drag reduction in vehicles and aircraft, flow control in pipes and channels, and the study of atmospheric and oceanic currents. It is also used in the design of wind turbines and other energy systems.

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