Theoretical Fluid Mechanics - Ideal Fluid Flow

AI Thread Summary
The discussion centers on deriving the complex potential for two sources of strength m located at z=ih and z=-ih, and demonstrating that the real axis acts as a streamline in the resulting flow field. The complex potential is expressed as F(z)=m/(2π) log(z+h) + m/(2π) log(z-h), with the goal of isolating the imaginary part to show that ψ=0 along y=0. Participants clarify that Bernoulli's equation can be simplified for ideal, irrotational flow, allowing for the calculation of pressure on the plate's upper surface. The conversation also addresses the necessity of evaluating φ at specific y values for practical applications, particularly for the pressure calculations on the flat plate. Understanding these concepts is crucial for solving the homework problem effectively.
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Homework Statement


Write down the complex potential for a source of strength m located at z=ih and a source of strength m located at z=-ih. Show that the real axis is a streamline in the resulting flow field, and so deduce that the complex potential for the two sources is also the complex potential for a flat plate located along the line y=0 with a source of strength m located a distance h above it.

Obtain the pressure on the upper surface of the plate mentioned above from Bernoulli's equation. Integrate the pressure difference over the entire surface of the plate, and so show that the force acting on the plate due to the presence of the source is pm^2/(4\pi h). Take the pressure along the lower surface of the plate to be equal to the stagnation pressure in the fluid.

Homework Equations


z=x+iy
Complex potential general form: F(z)=\phi +i\psi
Complex potential for a source of strength m : F(z)=\frac{m}{2\pi}\log(z-z_0)
Bernoulli's equation for ideal irrotational flow: \frac{\partial\phi}{\partial t}+\frac{p}{\rho}+\frac{1}{2}\nabla\phi\cdot\nabla\phi-G=F(t) where F(t) is the unsteady Bernoulli constant

The Attempt at a Solution


I have set up the problem in ({x,iy}) space with two sources along the iy axis of strength m, one at +h and one at -h. I then came up with the complex potential of the flow due to these two sources as F(z)=\frac{m}{2\pi}\log(z+h)+\frac{m}{2\pi}\log(z-h). This is about as far as I get before starting to become lost.

The next step is that I need to show that y=0 is a streamline in the flow field. To do so, I believe I need to separate real and imaginary parts of the complex potential so that I can isolate \psi and show that \psi=0 at y=0. When I attempt to tease out \psi from the complex potential I show that \phi + i\psi=\frac{m}{2\pi}\log(z^2-h^2), I can take the exponential of each side to get rid of the log function, but then my i\psi term is tied up in an exponential e^{\phi+i\psi} =e^{\frac{m}{2\pi}}(z^2-h^2). I have tried using Euler's formula, however, I still end up with a mess in which I can't seem to get equations for \phi and \psi in terms of x and y.

I am also somewhat uncomfortable with the form of Bernoulli's equation the book gives. I assume that since this flow is ideal, irrotational, and steady that Bernoulii's equation would simplify down to \frac{p}{\rho}+\frac{1}{2}\nabla\phi\cdot\nabla\phi-G=0, is this correct?Thank you all in advance for your time and guidance. I'm way out of my comfort zone in this course.

Also, would this topic be better of in one of the other subforums?
 
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Hello Bio, and welcome to PF :)

This is not my expertise, but if you want to write a complex potential in this way, don't you want something like ##{\bf F}({\bf z}) =\frac{m}{2\pi}\log({\bf z}+ih)+\frac{m}{2\pi}\log({\bf z}-ih)## (bold face F and z are complex, but h is a real number), which indeed also is a little healthier at z=h ? And then you rewrite it to ## {\bf F}({\bf z}) = \phi + i\psi=\frac{m}{\pi}\log({\bf z}^2+h^2)## to easily see ##\psi = 0## if z is real.
 
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Thank you for your input BvU. You are correct that it is easy to see that \psi=0 when y=0 (i.e. when z is real), however, I still need to isolate \phi for use in Bernoulli's equation. I believe I need to do this for all arbitrary y values, and not just for y=0...
 
for all arbitrary y values
to answer which question ?
Otherwise, I would simplify the Bernoulli eqn (no time dependence, no gravity) and see if I can find ##\nabla \phi## for y = 0 ...
 
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BvU said:
to answer which question ?
Otherwise, I would simplify the Bernoulli eqn (no time dependence, no gravity) and see if I can find ##\nabla \phi## for y = 0 ...
For whatever reason I was hesitant to find \phi for y=0 and felt as though it needed to be a general equation for \phi applicable to any value of y. Why is it okay to use \phi at a specific value of y for Bernoulli's equation? Is it because it's asking for the pressure on the upper surface of a flat plate, therefore y=+0? ... how obvious!
 
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