Industry-relevant training in Business, Technology, and Design to help professionals and graduates upskill for real-world careers.
Fun, engaging games to boost memory, math fluency, typing speed, and English skills—perfect for learners of all ages.
Enroll to start learning
You’ve not yet enrolled in this course. Please enroll for free to listen to audio lessons, classroom podcasts and take practice test.
Listen to a student-teacher conversation explaining the topic in a relatable way.
In turbulent flow, the velocity profile significantly differs from laminar flow. Can anyone tell me what shear stress is, particularly at the pipe wall?
Is it the stress that arises from the friction between the fluid and the wall?
Exactly! The shear stress at the wall is denoted as tau_naught and is considered a constant. Let's not forget that at small values of y, we can equate tau to tau_naught. This gives us some useful simplifications. Remember the acronym 'STAY'—Shear stress at wall = Tau_naught + y small!
What does y represent in this context?
Great question! 'y' refers to the distance from the wall. The smaller the distance, the more we can approximate these relationships.
Now let's analyze how turbulent velocity profiles are structured. Based on what you've learned, can anyone explain the difference between laminar and turbulent velocity profiles?
I think the laminar profile is smooth and parabolic, while turbulent flow has a fuller profile.
Spot on! In turbulent flow, the profile is much fuller, which significantly influences the average fluid velocity. We use logarithmic profiles to capture this behavior. Remember 'FLAT': Full Layered Average Turbulent flow!
How are these profiles derived?
Excellent! We derive them using principles like the Prandtl mixing length theory. Each layer has distinct characteristics as we approach the wall.
Can anyone describe the four layers observed in turbulent flow near a wall?
I remember there's the viscous sublayer where velocity changes linearly.
Then there's the buffer layer, overlap layer, and the turbulent layer!
Fantastic! These layers define how flow behaves near surfaces. Who remembers the defining feature of the viscous sublayer?
The viscous effects are dominant there!
Exactly! If we visualize these layers as 'V-BOT' - Viscous, Buffer, Overlap, Turbulent, it will help in recalling their order.
Now let's explore how to categorize boundaries. What differentiates smooth boundaries from rough ones?
I think it's based on the height of surface irregularities compared to the viscous sublayer.
Correct! When the dimensionless ratio is less than 0.25, we're dealing with a smooth boundary, while a ratio greater than 6 signifies a rough boundary. Let’s use the acronym 'RICH'—Roughness Indicator for Categorizing Heights!
So those in-between values indicate transitional boundaries?
Absolutely! Transitional boundaries occur when the ratio lies between 0.25 and 6. Excellent observations, class!
Read a summary of the section's main ideas. Choose from Basic, Medium, or Detailed.
The section covers the analysis of turbulent flow in pipes, including the shear stress at the wall, the different layers of turbulence, and how boundary conditions impact flow characteristics. It emphasizes the importance of identifying boundary types based on surface roughness.
In this section, we delve into turbulent flow characteristics, particularly focusing on the formation of velocity profiles based on the Prandtl mixing length theory. We explore the shear stress at the wall, considering various boundary conditions and how they influence the flow dynamics in pipes. The section describes the four layers of turbulent flow: the viscous sublayer, buffer layer, overlap layer, and turbulent layer. It distinguishes between smooth and rough boundaries, utilizing concepts like the height of surface irregularities and the viscous sublayer thickness to define boundary types. The section wraps up with boundary equations and practical problem-solving examples, showcasing how theoretical concepts apply in real-world scenarios.
Dive deep into the subject with an immersive audiobook experience.
Signup and Enroll to the course for listening the Audio Book
Turbulent flow along a wall consists of 4 regions: Viscous sublayer, buffer layer, overlap layer, and turbulent layer. The viscous sublayer is a thin layer next to the wall where viscous effects are dominant, and the velocity profile is almost linear. In the buffer layer, turbulent effects begin to significant, though viscous effects still dominate. The overlap layer sees turbulent effects being more significant but not dominant. Lastly, in the turbulent layer, the turbulent effects dominate over viscous effects.
In turbulent flow near a wall, the flow is categorized into distinct regions:
1. Viscous Sublayer: Closest to the wall; here, the flow velocity changes linearly because of significant viscous forces. The flow behaves somewhat like a laminar flow within this layer.
2. Buffer Layer: This layer begins to involve turbulence but is still influenced by viscosity. The flow starts to show fluctuations here.
3. Overlap Layer: In this region, turbulent effects become predominant, yet they are still not fully established.
4. Turbulent Layer: This is where the turbulent characteristics dominate the flow, and velocity fluctuations are prominent. Each of these regions plays a crucial role in understanding the complete behavior of turbulent flow.
Imagine a river flowing past a riverbank. Right next to the bank, the water flows slowly, similar to the viscous sublayer where viscosity dominates. As you move further into the river, the same water begins to swirl and create waves, resembling the more turbulent flow in the turbulent layer. The variations in speed and movement show how different regions affect the overall flow.
Signup and Enroll to the course for listening the Audio Book
When it comes to bed types in turbulent flow, important terms are hydrodynamically rough and smooth boundaries. The mean height of surface irregularities is denoted as 'k'. If k is much larger than the thickness of the viscous sublayer (delta dash), the irregularities interact with eddies, leading to rough boundaries. If k is much smaller than delta dash, it leads to smooth boundaries. Nikuradse’s experiments classify these boundaries based on ratios of k to delta dash.
In turbulent flow, the texture of the boundary affects how the flow behaves:
- Smooth Boundaries: Occur when the surface irregularities are much smaller than the thickness of the viscous sublayer. Here, the eddies cannot significantly affect the flow, leading to smoother conditions.
- Rough Boundaries: Arise when the height of surface irregularities is greater than the viscous sublayer thickness. This situation causes turbulent eddies to interact with the surface, increasing friction and affecting flow velocities.
Nikuradse established metrics to help categorize these conditions, particularly focusing on the ratio of surface roughness to the viscous layer thickness.
Consider a slide at a playground. If the slide is smooth (like a smooth boundary), kids can go down faster without much friction. However, if the slide is rough with bumps (like a rough boundary), they will slow down due to increased friction and turbulence created by those bumps.
Signup and Enroll to the course for listening the Audio Book
To categorize boundaries, Nikuradse provided a threshold for k/delta dash:
- If k/delta dash < 0.25 → Smooth Boundary
- If k/delta dash > 6 → Rough Boundary
- If 0.25 < k/delta dash < 6 → Transitional Boundary. The roughness Reynolds number is used for evaluation as well: Re < 4 (Smooth), Re > 100 (Rough), 4 < Re* < 100 (Transitional).
The classification of a boundary type can often be determined mathematically using the height of irregularities (k) compared to the thickness of the viscous sublayer (delta dash):
- If the ratio of k to delta dash is less than 0.25, the boundary is considered smooth, indicating gentle effects on the flow by surface irregularities.
- Conversely, if the ratio exceeds 6, the boundary becomes rough, suggesting that the irregularities significantly impact flow dynamics.
- If the ratio falls in between these two values, the boundary is termed transitional. Similarly, the roughness Reynolds number helps to quantify this further and establish clear boundaries of smooth, rough, and transitional.
Think of a skincare routine where certain products can treat different types of skin textures. For delicate skin (smooth), you would use gentle exfoliants (smooth boundary), while for rough skin, you might need stronger scrubs (rough boundary). If your skin is a bit of both, you would choose hybrid treatments for transitional skin. The approach you take depends on the texture similar to how we assess boundary types in flow.
Learn essential terms and foundational ideas that form the basis of the topic.
Key Concepts
Prandtl Mixing Length Theory: A model used to describe the velocity profile in turbulent flow.
Shear Velocity: A parameter that represents frictional forces in turbulent flow, derived from wall shear stress.
Logarithmic Velocity Profile: A model that captures the behavior of velocity in turbulent flow near the wall.
See how the concepts apply in real-world scenarios to understand their practical implications.
An analysis of how the velocity profile changes from laminar to turbulent flow as the flow rate increases in a pipe.
Calculating the six conditions necessary to define a smooth boundary based on the height of surface irregularities.
Use mnemonics, acronyms, or visual cues to help remember key information more easily.
Turbulent flow isn't slow, it swirls and sways to and fro.
Imagine a fast river filled with rocks that creates whirlpools; that chaos is like turbulent flow.
Use 'FLAT' - Full Layered Average Turbulent to remember the structure of turbulent velocity profiles.
Review key concepts with flashcards.
Review the Definitions for terms.
Term: Turbulent Flow
Definition:
A type of fluid flow characterized by chaotic property changes, typically occurring at high velocities.
Term: Shear Stress
Definition:
The stress component parallel to a given surface, responsible for the deformation of materials.
Term: Viscous Sublayer
Definition:
The layer in turbulent flow adjacent to the wall where viscous effects are dominant and the velocity profile is nearly linear.
Term: Buffer Layer
Definition:
The layer in turbulent flow where both viscous and turbulent effects are significant.
Term: Rough Boundary
Definition:
A boundary where surface irregularities significantly interact with eddies in turbulent flow.