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The stream function for an incompressible, two dimensional flow field is $$\psi=2 r^{3} \sin 3 \theta$$ For this flow field, plot several streamlines for \(0 \leq \theta \leq \pi / 3\).

Short Answer

Expert verified
Plot streamlines for \( \theta \) between 0 and \( \pi/3 \) using different \( C \) values in the expression \( r = \left(\frac{C}{2\sin 3\theta} \right)^{1/3} \).

Step by step solution

01

Understand Stream Function Equation

The given stream function is \( \psi = 2r^3 \sin 3\theta \). A stream function describes the flow lines of a fluid such that the flow speed in a two-dimensional incompressible flow can be determined by its spatial derivatives.
02

What is Streamline?

A streamline is a line that is everywhere tangent to the velocity vector of the flow. For the stream function \( \psi \), the streamlines are given by setting \( \psi = C \), where \( C \) is a constant, resulting in the equivalent expression \( 2r^3 \sin 3\theta = C \).
03

Express Equation for Streamlines

To find streamlines, rearrange the expression to find \( r \) in terms of \( \theta \): \( r = \left(\frac{C}{2\sin 3\theta} \right)^{1/3} \). This form allows us to draw different streamlines by varying \( C \) and plotting \( r \) versus \( \theta \).
04

Define Range for Plotting

The problem restricts \( \theta \) to the range \( 0 \leq \theta \leq \frac{\pi}{3} \). Within this range, we will plot multiple streamlines by selecting different values of \( C \) and plotting the corresponding \( r \) values.
05

Plot Several Streamlines

For streamline plotting: Choose several constant values for \( C \), such as \( C = 1, 2, 3\). For each chosen \( C \), compute \( r \) over the specified range of \( \theta \). Plot \( r \) against \( \theta \) to show the streamlines within the \( \theta \) range. Each curve represents a streamline with a particular constant \( C \).

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Key Concepts

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

Streamlines
A streamline is a path traced by a fluid parcel in a steady flow, where the tangent at any point gives the fluid direction. In simpler terms, these are curves that show the flow direction of a fluid at every point. These lines are crucial in fluid dynamics as they help visualize flow patterns.
Each streamline's equation is derived from the stream function, given by setting the stream function \( \psi \) equal to a constant, such as \( C \). For the provided function \( \psi = 2r^3 \sin 3\theta \), streamlines can be expressed as \( 2r^3 \sin 3\theta = C \). This states that for specific values of \( C \), we can determine specific paths that particles in the fluid flow follow.
Regardless of how the flow may be affected by different pressures or obstacles, the shape and form of streamlines remain consistent in a steady flow field. This concept is usually tested by plotting these lines in different scenarios, helping us visualize and understand the flow of incompressible fluids. Each streamline is unique to its constant \( C \) value, representing different flow lines within the field.
Incompressible Flow
In fluid dynamics, when we talk about an incompressible flow, we are referring to a flow where the fluid's density remains constant. This means that the fluid does not undergo any change in its volume when pressure is applied. Imagine water flowing through a pipe; no matter how fast it's flowing, its density stays the same.
This property is crucial in simplifying calculations related to flow patterns and helps in binding equations like the stream function to solve real-world problems. Incompressible flow is often assumed for liquids since gases typically compress under pressure changes.
An important characteristic of incompressible flow is the constancy of mass flow rate across the flow. Any increase in speed due to narrowing of the channel must correspond to a decrease in the cross-sectional area, ensuring continuity. This continuity simplifies many fluid mechanics problems, making incompressible flow an essential concept in understanding the dynamics presented in stream function exercises.
Two-Dimensional Flow
Two-dimensional flow occurs when fluid flow is restricted to two dimensions, effectively assuming that nothing occurs out of the plane of interest. It's like taking a slice of cake and ignoring what happens above or below the slice. This kind of flow simplifies problems by reducing the number of variables affecting the system.
When a flow is considered two-dimensional, it means that the velocity of the fluid has only components along two axes, typically within a specified plane, like the xy-plane. This assumption significantly reduces the complexity of analyzing fluid behavior, making calculations much more manageable.
The two-dimensional assumption is often valid when the flow's length and width dimensions are significantly larger compared to its out-of-plane dimension. In such cases, studying the flow patterns using the stream function approach within these two dimensions can yield accurate insights. The streamlines obtained give a precise representation of the two-dimensional flow field, helping visualize how the fluid navigates through the designated area.

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Most popular questions from this chapter

It is known that the velocity distribution for twodimensional flow of a viscous fluid between wide parallel plates (Fig. \(P 6.31)\) is parabolic; that is, $$u=U_{c}\left[1-\left(\frac{y}{h}\right)^{2}\right]$$ with \(v=0 .\) Determine, if possible, the corresponding stream function and velocity potential.

A layer of viscous liquid of constant thickness (no velocity perpendicular to plate) flows steadily down an infinite, inclined plane. Determine, by means of the Navier-Stokes equations, the relationship between the thickness of the layer and the discharge per unit width. The flow is laminar, and assume air resistance is negligible so that the shearing stress at the free surface is zero.

The stream function for an incompressible, two-dimensional flow field is $$\psi=a y-b y^{3}$$ where \(a\) and \(b\) are constants. Is this an irrotational flow? Explain.

A certain flow field is described by the stream function $$\psi=A \theta+B r \sin \theta$$ where \(A\) and \(B\) are positive constants. Determine the correspond. ing velocity potential and locate any stagnation points in this flow field.

The streamlines for an incompressible, inviscid, twodimensional flow field are all concentric circles, and the velocity varies directly with the distance from the common center of the streamlines; that is $$v_{\theta}=K r$$ where \(K\) is a constant. (a) For this rotational flow, determine, if possible, the stream function. (b) Can the pressure difference between the origin and any other point be determined from the Bernoulli equation? Explain.

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