/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 49 Consider the steady flow of SAE ... [FREE SOLUTION] | 91Ó°ÊÓ

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Consider the steady flow of SAE 10 oil at \(20^{\circ} \mathrm{C}\) between two horizontal flat plates spaced \(20 \mathrm{~mm}\) apart. The average pressure between the plates is on the order of \(100 \mathrm{kPa}\), and the average velocity is on the order of \(0.08 \mathrm{~m} / \mathrm{s}\). What simplified form of the Navier-Stokes equation would be applicable in this situation?

Short Answer

Expert verified
The simplified Navier-Stokes equation is \( \frac{d^2 u}{dy^2} = \frac{1}{\mu} \frac{dp}{dx} \), applicable for laminar flow between plates.

Step by step solution

01

Understanding the Navier-Stokes Equation

The full Navier-Stokes equation for incompressible flow is given by: \[ \rho \left(\frac{\partial \mathbf{u}}{\partial t} + \mathbf{u} \cdot abla \mathbf{u} \right) = -abla p + \mu abla^2 \mathbf{u} + \mathbf{f} \] where \(\rho\) is the fluid density, \(\mathbf{u}\) is the velocity field, \(p\) is the pressure, \(\mu\) is the dynamic viscosity, and \(\mathbf{f}\) represents body forces. We will simplify this for our specific flow situation.
02

Assessing Assumptions for Simplification

For flow between narrow plates, several assumptions can be made: 1) The flow is steady, so \(\frac{\partial \mathbf{u}}{\partial t} = 0\). 2) The flow is fully developed, meaning \(\mathbf{u} \cdot abla \mathbf{u} = 0\). 3) The only pressure variation is in the direction of the flow. 4) There are no body forces acting in the flow direction.
03

Applying Assumptions to Navier-Stokes Equation

With the assumptions, the Navier-Stokes equation simplifies. The unsteady term \(\rho \frac{\partial \mathbf{u}}{\partial t}\) vanishes. The inertial term \(\mathbf{u} \cdot abla \mathbf{u}\) also disappears. Therefore, the simplified equation becomes: \[ 0 = -abla p + \mu abla^2 \mathbf{u} \] focusing on the balance between pressure gradient and viscous forces.
04

Recognizing the Type of Flow

Given the flow is between two plates, it corresponds to a "plane Poiseuille flow" or "laminar flow between parallel plates." This further confirms that the primary forces are viscous and pressure-driven.
05

Final Simplified Equation for this Flow

Considering the above, the simplified form of the Navier-Stokes equation for this situation, representing balance of pressure and viscous forces, is: \[ \frac{d^2 u}{dy^2} = \frac{1}{\mu} \frac{dp}{dx} \] where \(u\) is the velocity in the direction of the flow and \(y\) is the direction perpendicular to the plates.

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Key Concepts

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

Plane Poiseuille Flow
Plane Poiseuille Flow refers to the steady, viscous flow of a fluid between two infinitely large, parallel plates under a constant pressure gradient. Imagine two pieces of flat material, such as two slices of glass, held parallel to each other with some space between them. When a fluid, like oil, flows between these plates, it moves in a steady motion. This flow setup is a classic example used in studies of viscous fluid dynamics.

Deriving from the Navier-Stokes equations, the Plane Poiseuille Flow assumes that the velocity of the fluid changes across the space between the plates. The velocity is zero at the plates due to no-slip conditions and maximum at the mid-plane between them. The flow is smooth and layered, described by parallel streamlines.
  • Steady: The flow doesn’t change over time.
  • Viscous: The fluid’s internal friction is significant.
  • Newtonian: The fluid’s viscosity remains constant regardless of the flow conditions.
This type of flow is especially relevant in engineering applications like pipeline transports and lubrication systems.
Laminar Flow
Laminar Flow characterizes a type of fluid motion where the fluid travels smoothly or in regular paths, in contrast to turbulent flow, where the motion appears chaotic. In laminar flow, as evident in Plane Poiseuille Flow, each layer of fluid slides past adjacent layers smoothly, with minimal mixing and disturbance.

This can be observed in the stable, straight, and parallel streamlines. When you think of laminar flow, imagine a river flowing slowly without much disturbance or a stream moving calmly across a floor. Factors affecting laminar flow include:
  • Reynolds Number: Low Reynolds number (<2300) indicates laminar flow.
  • Fluid Viscosity: Higher viscosity encourages laminar flow.
  • Channel geometry: Smooth, narrow channels favor laminar movement.
Understanding laminar flow is crucial in fields like aerospace and chemical engineering, where controlled and predictable fluid movement is necessary.
Dynamic Viscosity
Dynamic Viscosity is a measure of a fluid's resistance to flow. In simpler terms, it is the "thickness" or "internal friction" of a fluid. Imagine trying to stir honey versus water; honey is thicker and harder to stir, which means it has higher viscosity.

Expressed in units of \( ext{Pascal-second (Pa·s)} \), dynamic viscosity affects how fluids move under applied force. Higher viscosity fluids move more slowly and are more resistant to flow, impacting the motion depicted in the Navier-Stokes equations. Dynamic viscosity plays a significant role in problems involving:
  • Flow resistance: It determines how much force is needed to move the fluid.
  • Energy loss: Higher viscosity leads to more heat generated due to friction.
  • Shear rates: It affects the rate at which layers of fluid slide past one another.
Knowledge of dynamic viscosity is essential for designing systems involving fluid transport like car engines and pipelines.
Pressure Gradient
A Pressure Gradient is the rate of pressure change occurring within a fluid along a particular direction. In fluid dynamics, a constant pressure gradient forces the fluid to move from high pressure areas towards lower pressure zones.

You can think of this as a slope down which fluid naturally flows. When discussing Plane Poiseuille Flow or any system ruled by Navier-Stokes equations, a pressure gradient is crucial for driving the motion of fluids between plates or pipes. Key characteristics include:
  • Direction: Indicates the path along which fluid is driven to move.
  • Magnitude: The strength of the pressure gradient affects velocity and flow rate.
  • Source of Flow: In our context, it is the primary driver behind flow between parallel plates.
Understanding pressure gradients helps predict how changes in pressure will impact fluid movement, crucial for applications in weather systems and HVAC design.

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Most popular questions from this chapter

A velocity field can be represented by the velocity components \(u=8 z, v=0,\) and \(w=2 x,\) where gravity has a magnitude \(g\) and acts in the negative \(z\) direction. Within the flow field, the viscosity is constant, and the pressure and density are equal to \(p_{0}\) and \(\rho_{0}\), respectively, at the location \(\left(x_{0}, y_{0}, z_{0}\right)\). Use the Navier-Stokes equation to determine the pressure distribution in terms of the given parameters.

A two-dimensional velocity field has the velocity components \(u=-2 x\) and \(v=2 y\). (a) Verify that this flow field can be described by a potential function. (b) Determine the circulation, \(\Gamma,\) around a closed path of straight lines connecting the following points: \((1,1),(2,1),(2,4),(1,4),\) and \((1,1) .\) Explain the significance of your result.

Consider the velocity field, \(\mathbf{V},\) given by $$ \mathbf{V}=x z \mathbf{i}-2 y z \mathbf{j}+3 x y \mathbf{k} \mathbf{m} / \mathbf{s} $$ where \(x, y\), and \(z\), are the coordinate locations in meters. Find the dilatation rate of the fluid at \((x, y, z)=(2 \mathrm{~m}, 3 \mathrm{~m}, 1 \mathrm{~m})\) and assess whether the fluid is being compressed or expanded.

A flow field in which the radial component of the velocity is everywhere equal to zero and in which the tangential component of the velocity depends only on the radial distance, \(r\), from a center point is called a vortex. Consider the vortex illustrated in Figure \(5.69,\) where Point \(P\) is the center of the vortex, Point 1 is on one streamline, and Point 2 is on another streamline. For which of the following velocity fields can the Bernoulli equation be applied between Points 1 and \(2: v_{\theta}=a r\) or \(v_{\theta}=a / r\), where \(a\) is any constant?

The velocity components in a two-dimensional flow field are \(u=x+2\) and \(v=3-y\). (a) Is the flow irrotational throughout the flow field? (b) If the flow is irrotational, determine the potential function of the flow field.

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