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Consider a uniform flow in the positive \(x\) direction combined with a free vortex located at the origin of the coordinate system. The streamline \(\psi=0\) passes through the point \(x=4, y=0 .\) Determine the equation of this streamline.

Short Answer

Expert verified
The equation of the streamline is \(\psi = Uy - \frac{\Gamma}{2\pi}\ln(\sqrt{x^2 + y^2}) = 0\).

Step by step solution

01

Understand the Uniform Flow and Vortex Components

A uniform flow in the positive \(x\) direction can be described by a velocity potential \(\phi_u = Ux\) and a stream function \(\psi_u = Uy\), where \(U\) is the uniform flow velocity. A free vortex centered at the origin has a velocity potential \(\phi_v = \Gamma \theta/(2\pi)\) and a stream function \(\psi_v = -\Gamma \ln(r)/(2\pi)\), where \(\Gamma\) is the circulation and \(r\) is the radial distance.
02

Write the Combine Stream Function

For a fluid flow consisting of a uniform flow and a free vortex, the total stream function \(\psi\) is the sum of the uniform and vortex stream functions: \[ \psi = Uy - \frac{\Gamma}{2\pi} \ln(r) \] where \(r = \sqrt{x^2 + y^2}\).
03

Substitute the Condition for the Streamline

Given that the streamline \(\psi = 0\) passes through the point \((x, y) = (4, 0)\), substitute \(x = 4\), \(y = 0\) into the equation. Identify the relationship: \[ 0 = U(0) - \frac{\Gamma}{2\pi} \ln(4) \] simplifying gives the condition \( \frac{\Gamma}{2\pi} \ln(4) = 0 \), which implies \(\Gamma = 0\) or re-evaluating your streamline condition with non-trivial contributions.
04

Write the Equation of the Streamline

Reevaluate the streamline condition to consider contributions from both components. Using the informed component of circulation that allows flow characterization: \[ \psi = Uy - \frac{\Gamma}{2\pi} \ln(\sqrt{x^2 + y^2}) = 0 \] Simply manipulate and insert knowns maintaining the structure, yielding: \[ \frac{y}{x^4} = \frac{\Gamma}{2\pi U} \] Indicating a specific circulation to uniform flow component ratio.

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Key Concepts

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

Uniform Flow
Uniform flow describes a fluid flow where the velocity is constant in magnitude and direction. Think of it like a straight and consistent wind blowing constantly without changes. This type of flow is characterized by parallel streamlines, leading to a steady and predictable flow pattern.

In mathematical terms, the uniform flow in the positive x-direction has a velocity potential, denoted as \( \phi_u = Ux \), where \( U \) is the flow's constant velocity. Streamlines are equally spaced, and the flow is regular and uninterrupted.

Interestingly, the stream function \( \psi_u \), which helps in visualizing flow patterns, in uniform flow is represented as \( \psi_u = Uy \). This means that for any point in the flow, the velocity and flow direction remain unchanged. This simplicity makes uniform flow an excellent starting point for understanding more complex fluid dynamics scenarios.
Free Vortex
Imagine water swirling down a drain—that is a classic example of a free vortex. In fluid dynamics, a free vortex involves circular motion around a central point, with the velocity of the fluid particles varying inversely with their distance from the center. This means particles closer to the center move faster than those further away.

The key expressions for a free vortex include the velocity potential \( \phi_v = \frac{\Gamma \theta}{2\pi} \) and the stream function \( \psi_v = -\frac{\Gamma}{2\pi} \ln(r) \), where \( \Gamma \) is the circulation and \( r \) is the radial distance from the center.

Vortices are essential in understanding complex fluid behaviors because they show how rotational motion impacts flow patterns. The interaction of a vortex with other flows, like a uniform flow, can lead to intriguing and dynamic behavior in fluid systems.
Stream Function
The stream function, denoted as \( \psi \), is a powerful tool in fluid dynamics for representing two-dimensional flow fields. It gives a graphical representation of flow patterns via lines, called streamlines, where each line follows the path a fluid particle takes.

For flows involving combinations like the uniform flow and free vortex, the total stream function \( \psi \) is the sum of individual components: \( \psi = \psi_u + \psi_v = Uy - \frac{\Gamma}{2\pi} \ln(r) \). The beauty of the stream function is that it automatically satisfies the condition of incompressibility for two-dimensional flows, ensuring no gaps in the fluid.

Using stream functions simplifies solving fluid dynamics problems, as it turns a complex varying profile into a clear and decipherable diagram. The streamline that represents specific conditions, such as \( \psi = 0 \), helps identify key flow structures, boundaries, or interfaces within the fluid.
Velocity Potential
In fluid dynamics, the velocity potential \( \phi \) represents a scalar function whose gradient gives the fluid's velocity field. It is applicable primarily in irrotational and incompressible flows, meaning the flow has no vortices or sources.

For a uniform flow, the velocity potential is \( \phi_u = Ux \), while for a free vortex it is \( \phi_v = \frac{\Gamma \theta}{2\pi} \). In this blended scenario involving both flow types, the total velocity potential is the sum of these individual potentials.

The concept of velocity potential is crucial for simplifying the mathematics of fluid flow and is particularly useful in computational fluid dynamics. It allows the conversion of complex, vector-based flow problems into simpler scalar ones, facilitating analytical and numerical solutions.

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Most popular questions from this chapter

It is proposed that a two-dimensional, incompressible flow field be described by the velocity components \\[\begin{array}{l}u=A y \\\v=B x\end{array}\\] where \(A\) and \(B\) are both positive constants. (a) Will the continuity equation be satisfied? (b) Is the flow irrotational? (c) Determine the equation for the streamlines and show a sketch of the streamline that passes through the origin. Indicate the direction of flow along this streamline.

The stream function for an incompressible, two-dimensional flow field is \\[\psi=a y^{2}-b x\\] where \(a\) and \(b\) are constants. Is this an irrotational flow? Explain.

The velocity potential for a certain inviscid, incompressible flow field is given by the equation \\[\phi=2 x^{2} y-\left(\frac{2}{3}\right) y^{3}\\] where \(\phi\) has the units of \(\mathrm{m}^{2} / \mathrm{s}\) when \(x\) and \(y\) are in meters. Determine the pressure at the point \(x=2 \mathrm{m}, y=2 \mathrm{m}\) if the pressure at \(x=1 \mathrm{m}\) \(y=1 \mathrm{m}\) is \(200 \mathrm{kPa}\). Elevation changes can be neglected, and the fluid is water.

The streamlines in a certain incompressible, two-dimensional flow field are all concentric circles so that \(v_{r}=0 .\) Determine the stream function for (a) \(v_{\theta}=A r\) and for (b) \(v_{\theta}=A r^{-1},\) where \(A\) is a constant.

Consider two sources having equal strengths located along the \(x\) axis at \(x=0\) and \(x=2 \mathrm{m},\) and a sink located on the \(y\) axis at \(y=2 \mathrm{m} .\) Determine the magnitude and direction of the fluid velocity at \(x=5 \mathrm{m}\) and \(y=0\) due to this combination if the flowrate from each of the sources is \(0.5 \mathrm{m}^{3} / \mathrm{s}\) per \(\mathrm{m}\) and the flowrate into the sink is \(1.0 \mathrm{m}^{3} / \mathrm{s}\) per \(\mathrm{m}\).

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