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Today, we're going to talk about mass flux through an elemental strip. Can anyone tell me what mass flux actually means?
I think mass flux is how much mass passes through a certain area per unit time.
Exactly! It's quantified as mass flow rate per unit area, typically expressed as ρu, where ρ is the density and u is the velocity.
So how does this relate to fluid flow over a plate?
Great question! When fluid flows over a flat plate, we need to account for how much mass crosses an elemental strip of the plate. Let's define our elemental strip's area first.
The area of the elemental strip is given by width multiplied by thickness, right?
So, if 'b' is the width and 'dy' is the thickness, the area is b times dy?
Exactly! This setup will help us calculate the mass flux across that strip.
Let’s summarize: mass flux is defined as mass per unit area, and in our case, it’s related to the elemental strip’s area.
Now let's define displacement thickness. Who can explain what it means?
Isn't it the distance a streamline is displaced away from the wall due to viscosity?
Correct! Specifically, it's the distance that a streamline, which is outside the boundary layer, is pushed away from the wall due to the influence of viscous effects.
How do we calculate it?
We calculate it by integrating the velocity profile across the boundary layer. The formula integrates the difference between outer velocity U and the velocity u within the boundary layer.
What does the integral look like?
It’s written as ∫(1 - u/U) dy from 0 to delta. This helps us capture the flow behavior across the thickness.
In short, displacement thickness accounts for how flow is affected near the boundary, essential for predicting fluid behavior.
Next, let's discuss momentum thickness. Who remembers what that term represents?
I think it relates to the loss of momentum in the boundary layer due to viscosity?
Exactly! Momentum thickness is a measure of how much momentum flux is reduced in the boundary layer compared to the potential flow.
How is it calculated differently from displacement thickness?
Good question! While displacement thickness focuses on mass flow, momentum thickness involves integrating a term which includes velocity 'u' itself: ∫(u/U)(1 - u/U) dy.
So, we consider the velocity's effect on momentum?
Yes! This helps us understand energy losses in flow due to viscosity, which is crucial for engineering calculations.
Hence, momentum thickness provides insights into momentum losses in fluid dynamics.
Let’s talk about why knowing displacement and momentum thickness is essential in engineering.
Is it to design better systems that handle fluid flows efficiently?
Precisely! These thicknesses help in optimizing designs, predicting energy losses, and ensuring efficient fluid handling.
Could you give us an example?
Imagine designing an aircraft wing; understanding the boundary layer and these thicknesses helps improve lift and drag characteristics, leading to more fuel-efficient designs.
So, it also relates to performance in real-world applications!
Exactly! Engineers use these principles regularly in various fields such as aerospace, mechanical, and civil engineering.
Today, we covered displacement and momentum thicknesses and their applications in engineering.
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In this section, the concept of mass flux through an elemental strip in boundary layer theory is discussed. Key definitions such as displacement thickness and momentum thickness are introduced, along with their significance in understanding fluid dynamics over a flat plate.
This section focuses on the calculation of mass flux through an elemental strip in fluid flow, particularly in the context of boundary layer theory. It begins with the examination of flow over a smooth flat plate, where various thicknesses like displacement thickness and momentum thickness are derived and explained.
Key points discussed include:
- Displacement Thickness: Defined as the distance by which a streamline outside the boundary layer is shifted due to viscous effects on the plate; mathematically expressed as the integral of velocity deficit across the boundary layer.
- Momentum Thickness: Reflects the reduction in momentum flux due to the presence of viscosity, calculated in a similar manner as displacement thickness, where momentum rather than mass flux is considered.
The derivation of these terms involves consideration of mass flux through an elemental strip defined by its width and thickness, resulting in equations crucial for understanding fluid behavior in engineering applications. The relationship between the displacement and momentum thicknesses is critically analyzed, emphasizing their roles in boundary layer theory.
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Now, we consider the flow over a smooth flat plate, like this. So, there is a flow which is coming with a speed U, there is a flat plate and at any distance x, there is a section 1 - 1. I will remove this, but just to mark, this is the section 1 – 1 and, that is, located at a distance x, from the leading edge. So, this is the leading edge. The orientation is clear to you, I hope. Now, at section 1 - 1, we consider an elemental strip of thickness dy. Now, this dy so, this is the elemental thickness dy and it is located at a distance y from the plate.
In this chunk, we are setting the scenario for our analysis. We are looking at a flat plate with fluid flowing over it at a speed U. The important aspect here is understanding that at a certain distance (x) from the leading edge of the plate, we can analyze a small section (1 - 1). This section contains an 'elemental strip' of thickness denoted as dy. Essentially, dy represents an infinitesimally small vertical slice of the flow right next to the plate. Knowing these characteristics allows us to examine properties of the flow at a specific point.
Imagine you are observing a smooth river flowing over a flat rock. If you were to take a tiny slice of the water that flows directly against the rock’s surface, that slice would be akin to our 'elemental strip.' Just as we can look at how the water behaves in that small section, we can analyze the behavior of fluid in our elemental strip next to the plate.
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Suppose, if b is the width of the plate, that is, the width, then the area of the strip can be given by, b into dy. The strip will have the height dy and the width is b. Therefore, the area is simply bdy, here. Now, the mass flux through the elemental strip is given by, ρ u into dA. ρ u is the sort of a momentum, ρ into u, mass into velocity. Of course, we have not considered the volume, right now, but we multiply it with dA, to have the mass flux. So, dA if you put dy, this becomes ρ U b into dy.
In this segment, we calculate the mass flux through our elemental strip. The mass flux (mass flow per unit area) through this strip is found by multiplying the density (ρ) of the fluid with its velocity (u) and the area of the strip (dA = bdy). The width of the strip is b, and since we’re working with an infinitesimally small thickness dy, the area of our strip becomes bdy. Therefore, the mass flux expression simplifies to ρ U b dy, where U is the velocity of the flow.
Think of this in terms of water flowing through a hose. The hose is a uniform tube (like our plate), and when you look at a small segment of this hose, the amount of water flowing through it per second can be thought of as mass flux. If the water has a certain density and flows at a certain speed, you can calculate how much mass of water passes through that small section of hose in a given time.
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Therefore, the reduction in the mass flux through the elemental strip, compared to the, you know, uniform velocity profile will be the difference of the mass fluxes. This is due to uniform, that is, in the boundary layer, or if we take ρ outside, b and dy outside, it becomes ρ into U minus u into bdy.
This chunk discusses how we determine the difference in mass flux between the ideal uniform flow scenario and the actual flow within the boundary layer. The resulting reduction in mass flux can be calculated by comparing the mass flux in a region where the flow is fully developed (U) vs. the boundary layer flow (u). By factoring out constants such as ρ, b, and dy, we find that the reduction simplifies to ρ (U - u) b dy, indicating how much the velocity defect reduces the mass flow.
Imagine a river flowing smoothly (uniform flow). If you drop a stick into it, the stick will float and move with the river’s speed. Now think about the surface of the river near the bank where the water slows down due to friction with the riverbed (boundary layer). The stick would appear to lag behind this slower-moving water; the difference in speed represents the reduction in mass flux, as the slower water has less influence on moving objects.
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Now, the total reduction in mass flux through BC, will be, we have considered and its thickness of dy. So, what we are going to do? We are going to simply integrate over this length. And let us say, this is so, let me, so, this distance is delta. So, the integration goes from 0 to delta and ρ U - u b dy, that is, the total reduction in mass flux through BC. I hope, this is clear, this is equation number 1.
Here, we're discussing how to quantify the total reduction in mass flux across the entire boundary layer by performing an integration. We set up to integrate our earlier expression of mass flux reduction from the point where the flow first touches the plate (y=0) to the boundary layer's outer edge (y=delta). This provides us with a complete picture of how mass flux changes as we move through the boundary layer.
Think of counting how many apples fall from a tree. Instead of just counting one apple at a time, you can gather apples from all the branches at once. By summing them all up—that's essentially what integration does for our problem. You're tallying the total effect (in this case, total mass flux reduction) across a range, rather than just at a single point.
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Now, when the plate is displaced by delta dash, such that, the velocity at delta dash is equal to U, then the reduction in mass flux through the distance delta dash is going to be, very simple. It is going to be ρ U because the velocity there is, U delta dash into b. So, we have assumed, that the place, I mean, the plate is displaced by delta dash, such that, the velocity at delta dash is equal to the uniform velocity U, that was, outside the boundary layer, then the reduction in the mass flux through that distance is going to be ρ U delta dash b, because at the plate it was 0.
In this part, we are deriving the formula for displacement thickness. We assume the plate has been shifted such that at this new position (delta dash), the fluid velocity equals U. The mass flux reduction can then be represented as ρ U delta dash b. Notably, at the plate itself, the fluid velocity is 0. Thus, this simplification provides us with an essential relationship that helps us later quantify the effects of the boundary layer.
Think about pushing a board through water. As you push the board faster, the water beneath it gets displaced. If you displaced the board by a certain length and measured the speed of water flowing at that new point, that’s akin to our concept of displacement thickness—it quantifies the impact of moving the board on the surrounding water flow.
Learn essential terms and foundational ideas that form the basis of the topic.
Key Concepts
Mass Flux: A measure of the quantity of mass flowing per unit area per unit time.
Displacement Thickness: The distance a streamline is displaced from the wall due to viscous effects.
Momentum Thickness: The loss of momentum flux in the boundary layer compared to the potential flow.
Boundary Layer: A thin region near a boundary where viscous effects are significant.
See how the concepts apply in real-world scenarios to understand their practical implications.
In laminar flow over a flat plate, the mass flux can be calculated using the density and velocity profile.
In designing aircraft wings, knowledge of displacement and momentum thickness are used to optimize lift and drag characteristics.
Use mnemonics, acronyms, or visual cues to help remember key information more easily.
In fluid lore, mass flux takes flight, Through strips of space, it flows so right.
Imagine a river flowing over a flat rock. The water edge hugs closely, while the center flows smoothly, creating layers. The distance from the rock’s edge to the main flow is like displacement thickness; it pushes the flow away, creating a calming effect.
To remember the three thicknesses: Displace, Measure, Momentum — DMM for Displacement, Momentum, and manipulation of mass.
Review key concepts with flashcards.
Review the Definitions for terms.
Term: Mass Flux
Definition:
The amount of mass passing through a unit area per unit time, typically expressed as ρu.
Term: Displacement Thickness
Definition:
The thickness 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 compared to potential flow.
Term: Boundary Layer
Definition:
The thin region near a surface where the effects of viscosity are significant.