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A plane polar coordinate velocity potential is defined by \\[ \phi=\frac{K \cos \theta}{r} \quad K=\mathrm{const} \\] Find the stream function for this flow, sketch some streamlines and potential lines, and interpret the flow pattern.

Short Answer

Expert verified
The stream function is \( \psi = \frac{K \sin \theta}{r} \). Streamlines and potential lines are orthogonal hyperbolas, indicating irrotational flow.

Step by step solution

01

Understand the Relationship between Velocity Potential and Stream Function

In plane polar coordinates, the velocity potential \( \phi \) and the stream function \( \psi \) are related by the following equations: \( u_r = \frac{\partial \phi}{\partial r} \) and \( u_\theta = \frac{1}{r} \frac{\partial \phi}{\partial \theta} \). The corresponding stream function relations are \( u_r = \frac{1}{r} \frac{\partial \psi}{\partial \theta} \) and \( u_\theta = -\frac{\partial \psi}{\partial r} \). Our goal is to find \( \psi \).
02

Calculate the Radial and Angular Components of Velocity

Given \( \phi = \frac{K \cos \theta}{r} \), differentiate with respect to \( r \): \( u_r = \frac{\partial \phi}{\partial r} = -\frac{K \cos \theta}{r^2} \). Differentiate with respect to \( \theta \): \( u_\theta = \frac{1}{r} \frac{\partial \phi}{\partial \theta} = -\frac{K \sin \theta}{r} \).
03

Determine the Stream Function \( \psi \)

Use the velocity relationships: \( u_r = \frac{1}{r} \frac{\partial \psi}{\partial \theta} \) implies that \( \frac{1}{r} \frac{\partial \psi}{\partial \theta} = -\frac{K \cos \theta}{r^2} \). Integrate with respect to \( \theta \) to find \( \psi = K \sin \theta / r + f(r) \), where \( f(r) \) is a function of \( r \) only.
04

Use the Angular Component to Determine \( f(r) \)

From \( u_\theta = -\frac{\partial \psi}{\partial r} \), we have \( -\frac{K \sin \theta}{r} = -\frac{\partial}{\partial r} \left( \frac{K \sin \theta}{r} + f(r) \right) \). Evaluating, we see that \( f'(r) = 0 \), so \( f(r) \) is a constant, which can be set to zero for simplicity.
05

Write the Complete Stream Function

Substitute \( f(r) = 0 \) back into the expression for \( \psi \), giving \( \psi = \frac{K \sin \theta}{r} \).
06

Sketch Streamlines and Potential Lines

Streamlines are obtained from constant \( \psi \), i.e., \( \frac{K \sin \theta}{r} = \text{constant} \), representing hyperbolas. Potential lines are obtained from constant \( \phi = \frac{K \cos \theta}{r} = \text{constant} \), also representing hyperbolas. These patterns intersect each other orthogonally, detailing the flow around an object with uniform circulation.
07

Interpretation of Flow Pattern

The flow described by this velocity potential represents a source or sink of strength proportional to \( \cos \theta \), causing radial and angular flow components. The hyperbolic nature of streamlines and potential lines suggests irrotational flow towards and away from the origin, with induced motion around the coordinate axes.

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Key Concepts

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

Velocity Potential
In fluid dynamics, the velocity potential is a scalar function that helps in understanding irrotational flow. Specifically, in plane polar coordinates, it represents the potential energy of the flow. The equations connecting velocity potential \(\phi\) and the flow components are:
  • Radial component \(u_r = \frac{\partial \phi}{\partial r}\)
  • Angular component \(u_\theta = \frac{1}{r} \frac{\partial \phi}{\partial \theta}\)
For the given velocity potential \(\phi = \frac{K \cos \theta}{r}\), these components help determine how the flow moves in radial and angular directions. Understanding these components is crucial for transforming the velocity potential into a stream function, which helps visualize the streamlines in the fluid.
Stream Function
The stream function \(\psi\) is a crucial concept for visualizing flow patterns in an irrotational fluid. It is particularly useful as it represents lines where the flow velocity is constant, known as streamlines. In polar coordinates, the relationships between \(\psi\) and flow velocities are:
  • \(u_r = \frac{1}{r} \frac{\partial \psi}{\partial \theta}\)
  • \(u_\theta = -\frac{\partial \psi}{\partial r}\)
To find \(\psi\) from a given velocity potential \(\phi\), we integrate under the condition that \(\frac{1}{r} \frac{\partial \psi}{\partial \theta} = -\frac{K \cos \theta}{r^2}\). Upon integrating, we obtain \(\psi = \frac{K \sin \theta}{r}\), assuming \(f(r) = 0\) for simplicity. This stream function indicates hyperbolic streamlines, displaying how the fluid circulates around objects.
Irrotational Flow
Irrotational flow is a type of flow where the fluid has no rotation at any point. This concept is of particular interest, as it simplifies the analysis of fluid dynamics by using velocity potential and stream functions. Notably, in an irrotational flow, relationships such as \(u_r = \frac{\partial \phi}{\partial r}\) and \(u_\theta = \frac{1}{r}\frac{\partial \phi}{\partial \theta}\) hold true. Irrotational flow in polar coordinates often results in patterns where streamlines and potential lines intersect orthogonally. This orthogonality signifies a flow pattern with harmonic characteristics, making it easier to predict how the fluid will behave around boundaries or inside various domains. The specific hyperbolic nature of streamlines in this case study demonstrates how irrotational flows tend to behave in ideal conditions, assisting students in understanding complex flow problems.

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Most popular questions from this chapter

A two-dimensional incompressible velocity field has \(u=K\left(1-e^{-\alpha y}\right),\) for \(x \leq L\) and \(0 \leq y \leq \infty .\) What is the most general form of \(v(x, y)\) for which continuity is satisfied and \(v=v_{0}\) at \(y=0 ?\) What are the proper dimensions for constants \(K\) and \(a ?\)

A stream function for a plane, irrotational, polar coordinate flow is \\[ \psi=C \theta-K \ln r \quad C \text { and } K=\mathrm{const} \\] Find the velocity potential for this flow. Sketch some streamlines and potential lines, and interpret the flow pattern.

Show that the incompressible flow distribution, in cylindrical coordinates, \\[ v_{r}=0 \quad v_{\theta}=C r^{n} \quad v_{z}=0 \\] where \(C\) is a constant, \((a)\) satisfies the Navier-Stokes equation for only two values of \(n\). Neglect gravity. \((b)\) Knowing that \(p=p(r)\) only, find the pressure distribution for each case, assuming that the pressure at \(r=R\) is \(p_{0} .\) What might these two cases represent?

A steady, two-dimensional flow has the following polarcoordinate velocity potential: \\[ \phi=C r \cos \theta+K \ln r \\] where \(C\) and \(K\) are constants. Determine the stream function \(\psi(r, \theta)\) for this flow. For extra credit, let \(C\) be a velocity scale \(U\) and let \(K=U L,\) sketch what the flow might represent.

Consider the plane polar coordinate velocity distribution \\[ v_{r}=\frac{C}{r} \quad v_{\theta}=\frac{K}{r} \quad v_{z}=0 \\] where \(C\) and \(K\) are constants. ( \(a\) ) Determine if the equation of continuity is satisfied. (b) By sketching some velocity vector directions, plot a single streamline for \(C=K .\) What might this flow field simulate?

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