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An incompressible and irrotational flow field has a potential function, \(\phi\), that can be described by the relation $$ \phi=r \cos \theta+\ln r $$ Determine the corresponding expression for the stream function in polar coordinates.

Short Answer

Expert verified
\( \psi = r \sin \theta + \theta + C \).

Step by step solution

01

Understand the Relationship Between Potential and Stream Function

In a flow field, the potential function \( \phi \) and the stream function \( \psi \) satisfy the Cauchy–Riemann equations. For polar coordinates \((r, \theta)\), these equations are: \( \frac{\partial \phi}{\partial r} = \frac{1}{r} \frac{\partial \psi}{\partial \theta} \) and \( \frac{1}{r} \frac{\partial \phi}{\partial \theta} = -\frac{\partial \psi}{\partial r} \). We will use these relations to find \( \psi \).
02

Differentiate \( \phi \) with Respect to \( r \)

Given \( \phi = r \cos \theta + \ln r \), differentiate \( \phi \) with respect to \( r \):\[ \frac{\partial \phi}{\partial r} = \cos \theta + \frac{1}{r}. \]
03

Differentiate \( \phi \) with Respect to \( \theta \)

Differentiate \( \phi \) with respect to \( \theta \):\[ \frac{\partial \phi}{\partial \theta} = -r \sin \theta. \]
04

Solve for \( \frac{1}{r} \frac{\partial \psi}{\partial \theta} \)

Using the equation \( \frac{\partial \phi}{\partial r} = \frac{1}{r} \frac{\partial \psi}{\partial \theta} \), substitute \( \frac{\partial \phi}{\partial r} = \cos \theta + \frac{1}{r} \):\[\frac{1}{r} \frac{\partial \psi}{\partial \theta} = \cos \theta + \frac{1}{r}.\]Multiply both sides by \( r \) to obtain:\[\frac{\partial \psi}{\partial \theta} = r \cos \theta + 1.\]
05

Integrate with Respect to \( \theta \) to Find \( \psi \)

Integrate \( \frac{\partial \psi}{\partial \theta} = r \cos \theta + 1 \) with respect to \( \theta \):\[\psi = r \sin \theta + \theta + f(r),\]where \( f(r) \) is an arbitrary function of \( r \).
06

Solve for \( -\frac{\partial \psi}{\partial r} \)

Using the equation \( \frac{1}{r} \frac{\partial \phi}{\partial \theta} = -\frac{\partial \psi}{\partial r} \), where \( \frac{\partial \phi}{\partial \theta} = -r \sin \theta \), we have \[-\frac{\partial \psi}{\partial r} = -\sin \theta.\]Thus, \[\frac{\partial \psi}{\partial r} = \sin \theta.\]
07

Confirm \( f(r) \) from \( \frac{\partial \psi}{\partial r} \)

From \( \frac{\partial \psi}{\partial r} = \sin \theta \), it implies that \( f'(r) = 0 \). Therefore, \( f(r) = C \), where \( C \) is a constant. The stream function thus becomes: \[\psi = r \sin \theta + \theta + C.\]
08

Final Expression for Stream Function

The final expression for the stream function \( \psi \) is \[\psi = r \sin \theta + \theta + C,\]where \( C \) is any constant, often chosen as zero for simplicity unless specified otherwise.

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Key Concepts

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

Irrotational Flow
Irrotational flow is a crucial concept in fluid dynamics. It describes a situation where the flow has no rotation or vorticity. That means as you travel along a flow path, you don't experience any spinning motion. This is typical for potential flows where the fluid moves in a stream without any vortices forming.

In mathematics, irrotational flow is represented by a velocity field whose curl is zero. If you imagine the flow like a smooth river, no whirlpools or swirling occur in irrotational flows. This condition simplifies the equations governing the flow significantly, allowing engineers and scientists to make accurate predictions about the behavior of the flow.

Irrotational behavior is often assumed in incompressible flows, especially at a steady state where the velocity doesn't change over time. This assumption makes it possible to use potential functions, as the flow can be described entirely through a scalar potential, giving the fluid field a highly ordered and predictable nature. So, understanding irrotational flows helps in solving complex real-world problems using simplified concepts.
Stream Function
In fluid dynamics, the stream function is a mathematical tool used to simplify the analysis of two-dimensional incompressible flows. It complements the potential function, which is often used for irrotational flows. The beauty of the stream function lies in its ability to represent the flow lines or streamlines in a fluid movement.

The stream function, denoted by \( \psi \), is crucial for visualizing fluid flow since contours of \( \psi \) correspond to streamlines. These are lines tangent to the velocity vector at every point, which means that fluid elements never cross these lines. This property makes it easier to study how a fluid evolves over time.

Using stream functions offers several advantages:
  • They inherently satisfy the continuity equation for incompressible flow.
  • They reduce the problem of finding flow fields to solving simpler gradient equations.
  • They are helpful in visualizing complex flow scenarios without solving the full Navier-Stokes equations.
The relationship between stream functions and potential functions is often governed by the Cauchy-Riemann equations. This complementary aspect helps determine flow characteristics in problems involving irrotational and incompressible flows.
Potential Function
A potential function, denoted by \( \phi \), is a scalar function used in fluid dynamics to describe velocity fields in irrotational and incompressible flows. It greatly simplifies the mathematics involved in analyzing these types of flows. Essentially, the gradient of the potential function gives the velocity field of the fluid.

For incompressible and irrotational flows, the potential function provides a powerful tool for understanding the movement without directly calculating complex movement equations. This occurs because any derivative of the potential function can correspond to a velocity component.

The potential function offers various benefits:
  • It simplifies the equations needed to describe the flow.
  • It helps in representing three-dimensional flows with a two-dimensional function in cases of axial symmetry.
  • It provides a more efficient way to solve fluid dynamics problems with fewer computations.
Whether you are dealing with engineering applications or theoretical fluid dynamics, employing a potential function makes the problem-solving process straightforward without unnecessary computational burdens.
Polar Coordinates
Polar coordinates are a two-dimensional coordinate system where each point on a plane is determined by a distance from a reference point and an angle from a reference direction. In fluid dynamics, this coordinate system is especially beneficial for describing problems with rotational symmetry or those involving circular paths.

In polar coordinates, a point is described by two values:
  • \( r \): the radial distance from the origin, often considered the center of rotation.
  • \( \theta \): the angular displacement measured in radians from the reference direction.
Using polar coordinates simplifies equations when there is symmetry in the radial direction or when the geometry aligns with circular shapes. This makes them ideal for applications like analyzing flow patterns around cylindrical objects or within circular pipes.

When dealing with potential functions and stream functions in polar coordinates, it ensures that the mathematics of these functions aligns with the physical reality of the flow, leading to more manageable and meaningful solutions.

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Most popular questions from this chapter

Observations of a fluid flow indicate that a velocity field can be represented by the velocity components \(u=8 z, v=6 x,\) and \(w=2 x,\) where gravity has a magnitude \(g\) and acts in the negative \(z\) -direction. Within the flow field, the viscosity is presumed constant. Assess whether this given velocity field satisfies the Navier-Stokes equation. If not, speculate on what may be the reason. If so, find an expression for the pressure distribution.

A two-dimensional velocity field in the \(x y\) plane is described by the following velocity components: $$ u=\frac{10 x}{x^{2}+y^{2}}, \quad v=\frac{10 y}{x^{2}+y^{2}} $$ Does the velocity field represent a possible incompressible flow? If so, find the pressure gradient \(\nabla p\) assuming a frictionless flow with negligible body forces.

A viscous liquid flows down an inclined plane as shown in Figure \(5.62 .\) The flow is two-dimensional in the \(x y\) plane, and the \(x\) -axis is oriented in the flow direction. Apply the Navier-Stokes equation to this problem and write the components of the Navier-Stokes equation in their most simplified forms.

In a two-dimensional incompressible flow field, the \(y\) component of the velocity, \(v\), is given by \(v=5 x^{2}\). The \(x\) component of the velocity, \(u(x, y)\), is unknown, but it is known that \(u(x, y)\) must satisfy the boundary condition that \(u(0, y)=0\). Determine \(u(x, y)\)

A viscous fluid is contained between two parallel plates spaced \(30 \mathrm{~mm}\) apart as shown in Figure \(5.52 .\) The bottom plate remains stationary, the top plate moves at \(2 \mathrm{~m} / \mathrm{s},\) and the velocity of the fluid varies linearly between the bottom and top plate. (a) Determine the rate of angular rotation and the vorticity of a fluid element contained between the plates and (b) determine the rate of angular deformation of the fluid element.

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