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Today, we're focusing on displacement thickness. Can anyone explain what displacement thickness is?
Is it the thickness that accounts for the reduction of velocity at the surface of the plate due to the boundary layer?
Exactly! It's the distance a streamline outside the boundary layer is pushed away from the wall due to viscous effects. When we analyze flow around an object, understanding this helps us design better systems.
How do we derive it?
Great question! We typically integrate the difference in velocities across the boundary layer. Remember 6 as in 'delta-dash' represents the displacement thickness in calculations. Let's do an example together.
Next, let's talk about momentum thickness. Who can tell me what it measures?
It's the loss of momentum flux due to the presence of a boundary layer, right?
Exactly! It's crucial for understanding viscous effects. The key formula involves integrating velocities similarly to displacement thickness but includes a momentum term. Remember, loss of momentum is key here.
Can you show how to calculate it with an example?
Certainly! Let's examine a common velocity profile and calculate the momentum thickness together.
Lastly, let’s discuss energy thickness. What does that represent?
It's about the reduction in kinetic energy due to velocity defects, right?
Precisely! While we won't derive it completely, it involves kinetic energy considerations. By understanding energy thickness, we can improve system efficiency.
Are there practical implications, like in engineering design?
Absolutely! Engineers use these concepts to optimize flow behavior around structures. Let's also do a practical example to see how energy thickness influences design.
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The section outlines essential concepts in boundary layer theory, including the definitions and derivations of displacement thickness, momentum thickness, and energy thickness, alongside practical examples demonstrating their applications in hydraulic engineering.
This section of the chapter focuses on the practical aspects of boundary layer theory in hydraulic engineering, specifically elaborating on three critical concepts: displacement thickness, momentum thickness, and energy thickness.
The latter part of the section includes example problems that enable students to apply their understanding of these thicknesses in computed scenarios, thereby reinforcing their theoretical and practical knowledge within the context of hydraulic engineering.
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Now we have to make note of some important point, that is, the boundary layer theory is based on the fact that the boundary layer is thin. So, at any location, at any location x, this x must be very much greater than delta, boundary layer thickness and also the displacement thickness. This x must also be greater than momentum thickness and also the energy thickness. This is these four things, means that, the boundary layer is thin. Boundary layer thickness, delta is a function of x. This has to be assumed, these are the 1, 2 and 3.
This chunk introduces the concept of the boundary layer and emphasizes that it is generally thin compared to the overall flow. The 'x' position in the flow must be significantly larger than the different thicknesses, namely the boundary layer thickness (delta), displacement thickness, momentum thickness, and energy thickness. This understanding is crucial in analyzing fluid flow, particularly in laminar and turbulent conditions.
Imagine you're observing a river. Near the banks, the water flows slower due to friction with the bank – this is like the boundary layer. If you're standing far from the bank on a bridge, the width of the river (x) is much larger than that slow-moving water strip near the bank (delta). Just like in this scenario, in fluid mechanics, we assume the flow (x) is much wider and faster than the thickness of the boundary layer.
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So, we are going to solve some problems that will demonstrate this momentum thickness, displacement thickness and energy thickness. So, the question is, find the displacement thickness, the momentum thickness and the energy thickness for the velocity distribution in the boundary layer which is given by, u / U y / delta.
Here, the instructor presents a practical problem where they will calculate displacement thickness, momentum thickness, and energy thickness based on a specific velocity distribution profile given by the equation 'u / U = y / delta'. This serves as a foundation for applying theoretical concepts to calculable scenarios, encouraging students to connect theory and practice.
Think of an artist painting a landscape. Just as the artist must consider the details of the foreground (the boundary layer) compared to the larger image of the background (the overall flow of water in our example), engineers must look closely at small sections of flow to understand how it behaves before drawing larger conclusions about how the entire flow system operates.
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By definition, displacement thickness, delta dash is given as, 0 to delta 1 minus u / U and into dy. Using this term here, we can use, we can write, delta dash again as, integral 0 to delta 1 minus, so, this is bracket, 1 - y / delta dy. Delta dash can be written as, after integration, 0 to delta - 1 / delta because this an integration with respect to y, this will become y square / 2 0 to delta.
The displacement thickness (delta dash) is defined mathematically by integrating from 0 to delta, using the equation considering the difference in velocities at different points within the boundary layer. The integration simplifies to a specific expression depicting the effective thickness of the boundary layer, directly influencing the flow characteristics above the plate. This thickness accounts for the difference between actual flow and the hypothetical flow without viscosity effects.
Consider the thinning of a pancake. If you pour batter onto a hot surface, the outer part (the edge) cooks faster—this can be visualized similarly to flow velocities near a plate. The displacement thickness represents how far 'the pancake' has thinned out in comparison to a theoretical perfect spread, where batter flows uniformly.
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Now, proceeding, what is the momentum thickness theta? So, momentum thickness theta is the loss of momentum flux in the boundary layer, as compared to that of the potential flow. Therefore, this is the loss of the momentum flux. Now, the deficit in the momentum flux for the boundary layer flow is written as, the same fundamental.
Momentum thickness (theta) represents the loss of momentum compared to an idealized scenario where velocity profiles are uniform. This section outlines the calculation, explaining that the difference in momentum flux must be analyzed to understand how much momentum is 'lost' in the boundary layer due to viscosity. An equation summarizes this concept, identifying what happens in a fluid when shear stress affects the flow velocities.
Think about a not-so-smooth highway versus a smooth racetrack. When cars drive on the racetrack (representing ideal flow), they maintain high speeds with minimal loss of momentum. However, on a bumpy highway (representing the boundary layer with friction), cars experience losses—much like momentum thickness shows us how real-life friction impacts ideal velocity in fluid flow.
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Key Concepts
Boundary Layer: The thin region near a boundary where viscous forces dominate.
Displacement Thickness: Distance that a streamline shifts due to viscous effects.
Momentum Thickness: Represents loss of momentum flux due to viscosity.
Energy Thickness: Represents the reduction in kinetic energy due to velocity deficits.
See how the concepts apply in real-world scenarios to understand their practical implications.
Calculating the displacement thickness for a flat plate with a known boundary layer velocity profile.
Determining momentum and energy thickness for flow around a cylindrical vessel.
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To know the flow, displacement's the key, a streamline shifted, that's the decree.
Imagine water flowing across a sleek plate. As it nears the plate, it slows down due to sticky forces, creating layers. Those layers cause a shift, displacing the main flow and changing its behavior.
DME - Displacement, Momentum, Energy: Remember the three thicknesses we must measure.
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Review the Definitions for terms.
Term: Displacement Thickness
Definition:
The distance by which a streamline outside the boundary layer is displaced due to viscous effects.
Term: Momentum Thickness
Definition:
A measure of the loss of momentum flux in the boundary layer relative to that of non-viscous flow.
Term: Energy Thickness
Definition:
A thickness based on the reduction of kinetic energy in fluid flow due to the velocity deficit within the boundary layer.
Term: Boundary Layer
Definition:
A thin region adjacent to a solid boundary where viscous forces are significant compared to inertial forces.