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What fluid property is responsible for the development of the velocity boundary layer? For what kinds of fluids will there be no velocity boundary layer in a pipe?

Short Answer

Expert verified
Answer: The fluid property responsible for the development of the velocity boundary layer is viscosity. The type of fluids that will not result in a velocity boundary layer are ideal or inviscid fluids, which have zero viscosity. However, these fluids are theoretical constructs and do not exist in reality.

Step by step solution

01

Identify the fluid property responsible for the development of the velocity boundary layer

The fluid property responsible for the development of the velocity boundary layer is viscosity. Viscosity is the measure of a fluid's resistance to flow and causes the fluid to stick to the walls of the pipe or any solid surface, leading to the development of the velocity boundary layer.
02

Determine the type of fluids without a velocity boundary layer

For a fluid to have no velocity boundary layer, its viscosity must be zero. Such fluids are called ideal or inviscid fluids, which have the property that their viscosity is equal to zero, and they do not form a boundary layer when flowing through a pipe. However, it's important to note that ideal fluids are theoretical constructs and do not exist in reality. All real fluids have some viscosity and will develop a boundary layer.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Viscosity
Viscosity is a fundamental property of fluids that describes their resistance to flow. It plays a crucial role in the behavior of fluids as they move over surfaces or through pipes. When a fluid flows, the molecules demonstrate internal friction, which is what we observe as viscosity. This friction is due to intermolecular forces that cause the fluid to resist shearing motion.

In simple terms, viscosity can be thought of as the thickness or "stickiness" of a fluid:
  • Fluids with high viscosity (e.g., honey, syrup) flow slowly because they have higher resistance to deformation.
  • Fluids with low viscosity (e.g., water, air) flow easily as they have less resistance.
Viscosity is measured in units such as pascal-seconds (Pa·s) or poise. Understanding viscosity is crucial as it influences many practical applications including lubrication, food processing, and transport of fluids through pipelines.
Velocity Boundary Layer
The velocity boundary layer is a key concept in fluid mechanics that describes a region of fluid flow where the velocity changes from zero at the surface to the uniform flow velocity away from the surface.

This layer forms due to the interaction between the fluid's viscosity and the solid boundary, such as a pipe wall:
  • At the very surface, due to viscosity, the velocity of the fluid is essentially zero.
  • As you move away from the boundary, the velocity increases until it matches the free stream velocity.
The development of a velocity boundary layer is critical in determining flow characteristics, such as drag and pressure loss in pipes or over surfaces. Thinner boundary layers imply less viscous effects, often leading to lower drag, whereas thicker boundary layers indicate significant viscous forces acting on the flow.
Inviscid Fluids
Inviscid fluids are an idealized concept in fluid mechanics where the fluid is assumed to have zero viscosity. Unlike real fluids, which always have some degree of viscosity, inviscid fluids do not exhibit internal resistance to flow. This means there is no development of a velocity boundary layer when inviscid fluids flow past solid boundaries.

This idealization simplifies many fluid dynamics problems and allows for easier calculations:
  • No boundary layer effects mean calculations don't need to account for viscosity-related complications.
  • Inviscid flow assumptions are often used in theoretical models, especially in areas like aerodynamics where they assume potential flow for simplification.
While inviscid fluids don't exist in reality, this concept is invaluable for providing insight into fluid flow dynamics before more complex, real-world effects are included in the analysis.

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Most popular questions from this chapter

A concentric annulus tube has inner and outer diameters of 1 in. and 4 in., respectively. Liquid water flows at a mass flow rate of \(396 \mathrm{lbm} / \mathrm{h}\) through the annulus with the inlet and outlet mean temperatures of \(68^{\circ} \mathrm{F}\) and \(172^{\circ} \mathrm{F}\), respectively. The inner tube wall is maintained with a constant surface temperature of \(250^{\circ} \mathrm{F}\), while the outer tube surface is insulated. Determine the length of the concentric annulus tube. Assume flow is fully developed.

Determine the convection heat transfer coefficient for the flow of \((a)\) air and \((b)\) water at a velocity of \(2 \mathrm{~m} / \mathrm{s}\) in an \(8-\mathrm{cm}\) diameter and 7-m-long tube when the tube is subjected to uniform heat flux from all surfaces. Use fluid properties at \(25^{\circ} \mathrm{C}\).

Consider the velocity and temperature profiles for a fluid flow in a tube with diameter of \(50 \mathrm{~mm}\) can be expressed as $$ \begin{aligned} &u(r)=0.05\left[\left(1-(r / R)^{2}\right]\right. \\ &T(r)=400+80(r / R)^{2}-30(r / R)^{3} \end{aligned} $$ with units in \(\mathrm{m} / \mathrm{s}\) and \(\mathrm{K}\), respectively. Determine the average velocity and the mean (average) temperature from the given velocity and temperature profiles.

Water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters a 12 -cm-diameter and \(8.5-\mathrm{m}\)-long tube at \(75^{\circ} \mathrm{C}\) at a rate of \(0.35 \mathrm{~kg} / \mathrm{s}\), and is cooled by a refrigerant evaporating outside at \(-10^{\circ} \mathrm{C}\). If the average heat transfer coefficient on the inner surface is \(500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), the exit temperature of water is (a) \(18.4^{\circ} \mathrm{C}\) (b) \(25.0^{\circ} \mathrm{C}\) (c) \(33.8^{\circ} \mathrm{C}\) (d) \(46.5^{\circ} \mathrm{C}\) (e) \(60.2^{\circ} \mathrm{C}\)

Water is flowing in fully developed conditions through a 3 -cm-diameter smooth tube with a mass flow rate of \(0.02 \mathrm{~kg} / \mathrm{s}\) at \(15^{\circ} \mathrm{C}\). Determine \((a)\) the maximum velocity of the flow in the tube and \((b)\) the pressure gradient for the flow.

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