Velocity Profile For Turbulent Boundary Layer (2.2) - Boundary Layer Theory (Contd..)
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Velocity Profile for Turbulent Boundary Layer

Velocity Profile for Turbulent Boundary Layer

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Interactive Audio Lesson

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Introduction to Turbulent Boundary Layer and Velocity Profiles

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Teacher
Teacher Instructor

Today, we will explore the turbulent boundary layer's behavior, specifically focusing on its velocity profile, which is determined by the one-seventh power law. Who can tell me what this law states?

Student 1
Student 1

Is it something like u/U = (y/δ)^(1/7)?

Teacher
Teacher Instructor

Exactly! Well done! This equation describes how fluid velocity changes with the distance from the surface. Can anyone explain what u and δ represent?

Student 2
Student 2

u is the fluid velocity at a certain height y, and δ is the boundary layer thickness.

Teacher
Teacher Instructor

Correct! This understanding is vital as it sets the stage for deriving important concepts like drag force. Can anyone recall what we mean by drag force?

Student 3
Student 3

It's the force exerted by the fluid on a surface due to friction.

Teacher
Teacher Instructor

That's right! Let’s remember the acronym ‘Friction – Forces Exerted’ to keep it in mind. At the end of this session, we’ll derive drag force critical for applications.

Deriving Drag Force and Coefficient of Drag

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Teacher
Teacher Instructor

Now that we know the velocity profile, let's move to calculating the drag force. What is the relationship between τ₀ and drag force?

Student 4
Student 4

Drag force F_D is calculated using the shear stress τ₀ over the area.

Teacher
Teacher Instructor

Correct! The formula F_D = ∫_0^L τ₀ * b dx will help us get the total drag force. We can substitute τ₀ from our previous equations. What does τ₀ depend on?

Student 1
Student 1

It depends on fluid density and velocity squared, among other factors.

Teacher
Teacher Instructor

Precisely! The density is vital while calculating the average drag coefficient, C_D. What is its formula?

Student 2
Student 2

C_D = F_D / (1/2 * ρ * A * U²).

Teacher
Teacher Instructor

Excellent! Remember, ‘Drag / Area’ gives us coefficients of efficiency in design.

Boundary Layer Separation and Its Effects

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Teacher
Teacher Instructor

Before we end, let’s talk about boundary layer separation. Who can explain what it is?

Student 3
Student 3

It's when the flow detaches from the surface due to adverse pressure gradients.

Teacher
Teacher Instructor

Right! This separation leads to increased drag and loss of lift in aerodynamic systems. Can you describe the conditions that favor flow separation?

Student 4
Student 4

When the pressure gradient is adverse, such as when dP/dx > 0.

Teacher
Teacher Instructor

Very well put! Now, let's memoroize with ‘Pressure Peaks Need Support’ to recall how pressure affects these layers.

Student 1
Student 1

Got it! So it's vital to manage separation in designs.

Teacher
Teacher Instructor

Exactly! Mitigating separation can be achieved by streamlining shapes or using suction. Understanding this is crucial for engineers!

Introduction & Overview

Read summaries of the section's main ideas at different levels of detail.

Quick Overview

This section discusses the velocity profile of turbulent boundary layers using the one-seventh power law and its implications on drag force and coefficient calculations.

Standard

The section explores the turbulent boundary layer's velocity profile, notably the one-seventh power law, and derives expressions for drag force and average drag coefficient in terms of Reynolds number. It emphasizes the importance of these calculations in hydraulic engineering applications.

Detailed

In this section, we delve into the turbulent boundary layer's velocity profile characterized by the one-seventh power law, defined mathematically as u/U = (y/δ)^(1/7), where U is the free stream velocity and δ is the boundary layer thickness. We begin with the derivation of drag force, τ₀, and then move on to how it relates to the Reynolds number. The boundary layer thickness for turbulent flow can be expressed as δ = 0.376 * x * Reₓ^(-0.2), leading to results for τ₀ in terms of these parameters. Furthermore, we investigate the coefficients of drag (C_D), culminating in the expression C_D = 0.072/Re^L^(1/5) as we evaluate how boundary layer properties affect drag forces. The section concludes with practical examples and problem-solving related to boundary layer separations and control methods, underpinning the theories with numerical interpretations.

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Introduction to Turbulent Boundary Layer

Chapter 1 of 4

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Chapter Content

The velocity profile for turbulent boundary layer is given by one by seventh power law.

Detailed Explanation

In turbulent flows, the velocity profile near a solid boundary can be described using a one-seventh power law. This means that the velocity of the fluid at any point in the boundary layer can be determined with respect to the velocity at the edge of the boundary layer. This law helps predict the behavior of turbulent flow near the surface.

Examples & Analogies

Imagine a wide river flowing rapidly. Near the banks, the water moves slower due to friction but accelerates as it moves toward the center. The one-seventh power law is like saying, 'the closer you are to the bank (the boundary), the slower your speed compared to the fast-moving center of the river.'

Expression for Drag Force

Chapter 2 of 4

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Chapter Content

Obtain an expression for the drag force and the average coefficient of drag, in terms of Reynolds number.

Detailed Explanation

The drag force experienced in a turbulent boundary layer can be expressed through the relationship involving the Reynolds number. The dimensionless Reynolds number is a key factor because it characterizes the flow regime. By integrating the shear stress over the area of the surface, we can derive the total drag force acting on the body immersed in the fluid.

Examples & Analogies

Think of swimming in a pool. If you swim quickly, you'll experience less drag compared to a slow swimmer. Similarly, the drag force can be reduced through higher speeds (represented by the Reynolds number), consequently affecting the swimmer's overall efficiency.

Wall Shear Stress

Chapter 3 of 4

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Chapter Content

The wall shear stress for turbulent shear boundary layer is given as, tau_0 is given.

Detailed Explanation

The wall shear stress, which acts at the boundary between the fluid and the surface, is crucial in analyzing fluid behavior. For turbulent flows, the shear stress can be calculated using empirical relationships that relate it to the density, velocity, and characteristics of the flow. This will assist in understanding how much force the fluid exerts over the surface.

Examples & Analogies

Imagine rubbing your hand against a fast-moving stream of water. The harder you push your hand against the water, the more resistance you feel. This resistance is analogous to wall shear stress; it quantifies how much force the water exerts against the surface of your hand.

Calculating Drag Force and Coefficient of Drag

Chapter 4 of 4

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Chapter Content

F_D is equal to integral 0 to L tau_0 b dx.

Detailed Explanation

Calculating the drag force starts with the wall shear stress and requires integrating over the length of the surface. This integration yields the total drag force, considering the shear stress distribution along that surface. The coefficient of drag then can be computed by comparing this force to the effective inertial force acting on the fluid.

Examples & Analogies

Think of a car moving through air. The drag it experiences can be thought of like the cumulative force that wind exerts all along its structure as it travels. By assessing how the wind pushes against various parts of the car, we can determine how 'draggy' the design is, just like we do in fluid dynamics.

Key Concepts

  • One-Seventh Power Law: The equation that relates fluid velocity distribution in a turbulent boundary layer.

  • Drag Force: The force acting against the motion of an object in the fluid.

  • Reynolds Number: A critical value for determining flow characteristics and regimes.

  • Boundary Layer Thickness: The measurement of how far the influence of viscosity extends into the fluid.

Examples & Applications

Example 1: Calculating the drag force for a flat plate in turbulent flow using the derived equations.

Example 2: Evaluating boundary layer thickness for a given Reynolds number under specific conditions.

Memory Aids

Interactive tools to help you remember key concepts

🎵

Rhymes

In the turbulent swirl, velocity takes a twirl, One-seventh's the rule, let maths be your tool!

📖

Stories

Imagine a river flowing over a rock, at first it's smooth, but as it gets crowded, it starts swirling and detaching. This is like our turbulent boundary layer, revealing how flows can separate as they encounter obstacles.

🧠

Memory Tools

Remember 'DRAG' - Drag, Reynolds, Area, Gradient, to keep terms related to fluid dynamics just in mind!

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Acronyms

Use 'BTTM' for Boundary, Thickness, Turbulence, and Motion in turbulent flow studies.

Flash Cards

Glossary

Turbulent Boundary Layer

The part of the flow near a boundary where viscous forces are significant and turbulence occurs.

Velocity Profile

The distribution of fluid velocity across the boundary layer.

Drag Force (F_D)

The force acting opposite to the relative motion of an object in a fluid.

Reynolds Number (Re)

A dimensionless number that predicts flow regimes in fluid dynamics.

Coefficient of Drag (C_D)

A dimensionless number that describes the drag force relative to the fluid density and speed.

Boundary Layer Separation

The phenomenon where the flow of fluid detaches from the boundary surface.

Reference links

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