How Can Newton's Laws Derive the Plateau Equation for Soap Films?

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Homework Help Overview

The discussion centers around deriving the Plateau equation, which describes the minimal surface of a soap film, using Newton's laws. The original poster attempts to connect the variational principle approach with a force balance approach based on Newtonian mechanics.

Discussion Character

  • Exploratory, Assumption checking, Mathematical reasoning

Approaches and Questions Raised

  • Participants explore the relationship between surface tension and forces acting on a small element of the soap film. The original poster initially presents a force balance approach but questions the correctness of their assumptions regarding the forces involved.

Discussion Status

The discussion has evolved with the original poster revising their approach based on feedback. They have acknowledged an earlier assumption that led to incorrect conclusions and are now working towards a more accurate formulation of the forces involved. Some participants have provided insights that challenge the original poster's reasoning, prompting further reflection and refinement of the derivation.

Contextual Notes

There is an ongoing examination of the assumptions made regarding the components of the forces acting on the soap film, particularly in relation to the tangential and normal forces. The discussion reflects a learning process with no definitive resolution yet.

Sasha86
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Homework Statement


The Plateau equation (minimal surface of a soap film) can easily be derived from variational principle. We want to minimize the area of the soap film,
<br /> S = \int \sqrt{1 + z_x^2 + z_y^2} \, \mathrm{d}x \, \mathrm{d}y<br />,
and through Euler-Lagrange equation we get the Plateau equation,
<br /> \frac{\partial}{\partial x} \left( <br /> \frac{z_x}{\sqrt{1 + z_x^2 + z_y^2}}<br /> \right) +<br /> \frac{\partial}{\partial y} \left( <br /> \frac{z_y}{\sqrt{1 + z_x^2 + z_y^2}}<br /> \right) = 0.<br />
I'd like to derive this equation from Newtons law.


Homework Equations


<br /> z_x = \frac{\partial z}{\partial x} \\<br /> z_y = \frac{\partial z}{\partial y} \\<br /> z_{xx} = \frac{\partial^2 z}{\partial x^2} \\<br /> z_{yy} = \frac{\partial^2 z}{\partial y^2}<br />
\gamma - surface tension


The Attempt at a Solution


I'll write the forces for a small element of the film, whose projection to plane z = 0 is a square \mathrm{d}x \, \mathrm{d}y. Sum of the forces on each element must by Newton be 0. Area of the element is \mathrm{d}S = \mathrm{d}x \, \mathrm{d}y \sqrt{1 + z_x^2 + z_y^2} = \sqrt{\mathrm{d}x^2 + \mathrm{d}z^2} \sqrt{\mathrm{d}y^2 + \mathrm{d}z^2} \frac{\sqrt{1 + z_x^2 + z_y^2}}{\sqrt{1 + z_x^2} \sqrt{1 + z_y^2}}.

The work needed to increase a surface is \mathrm{d}W = \gamma \mathrm{d}A (F \, \mathrm{d}x = y \, \mathrm{d}x for a simple square). Imagine I want to stretch the element in the x direction. Then the element stretches by \mathrm{d} \left( \sqrt{\mathrm{d}x^2 + \mathrm{d}y^2} \right) and the force needed to overcome the tension is \gamma \, \mathrm{d}y \, \sqrt{\frac{1 + z_x^2 + z_y^2}{1 + z_x^2}}. I'll only be interested in z component of the force so I need to multiply it by \frac{\mathrm{d}z}{\sqrt{\mathrm{d}x^2 + \mathrm{d}z^2}}.
Similarly for stretching in y direction.

Now I'll mark with \mathrm{d}_x a small diference between x and x + \mathrm{d}x and similarly for y. I then write the sum (over four sides of the small element) of the forces in z direction on the small element,
<br /> \mathrm{d}_x \left(<br /> \gamma \, \mathrm{d}y \, \frac{\sqrt{1 + z_x^2 + z_y^2}}{1 + z_x^2} z_x \right) +<br /> \mathrm{d}_y \left(<br /> \gamma \, \mathrm{d}x \, \frac{\sqrt{1 + z_x^2 + z_y^2}}{1 + z_y^2} z_y \right) = 0.<br />
Divide the expression bx \gamma \, \mathrm{d}x \, \mathrm{d}y and get,
<br /> \frac{\partial}{\partial x} \left( z_x \frac{\sqrt{1 + z_x^2 + z_y^2}}{1 + z_x^2} \right) +<br /> \frac{\partial}{\partial y} \left( z_y \frac{\sqrt{1 + z_x^2 + z_y^2}}{1 + z_y^2} \right) = 0,<br />
which isn't the Plateau equation.

Also, if I write the forces in the x direction I get,
<br /> \mathrm{d}_x \left(<br /> \gamma \, \mathrm{d}y \, \frac{\sqrt{1 + z_x^2 + z_y^2}}{1 + z_x^2} \right) = 0,<br />
which suggests that the expression between the braces depends only on y. Take this into account in the upper equation and get,
<br /> \frac{\sqrt{1 + z_x^2 + z_y^2}}{1 + z_x^2} z_{xx} +<br /> \frac{\sqrt{1 + z_x^2 + z_y^2}}{1 + z_y^2} z_{yy} = 0.<br />
This is even worse. What am I missing?
 
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Hello, and welcome to PF!

A couple of things that I noticed that don't seem correct to me, but maybe I'm just not following your work.

First, you have the following expression for the force:
Sasha86 said:
...the force needed to overcome the tension is \gamma \, \mathrm{d}y \, \sqrt{\frac{1 + z_x^2 + z_y^2}{1 + z_x^2}}.

If this is the force on one edge of the surface element, then I would think the magnitude of the force would be ##\gamma## times the length of the edge, which doesn't seem to be what you have.

Second, I don't think your expression for getting the z-component of the force is correct:
I'll only be interested in z component of the force so I need to multiply it by \frac{\mathrm{d}z}{\sqrt{\mathrm{d}x^2 + \mathrm{d}z^2}}.

The force will point in a direction that is tangent to the surface and also perpendicular to the edge. In general, the force vector will have nonzero x, y, and z components. So, the factor for finding the z-component will be more complicated than your expression.

That's how I see it anyway.
 
Last edited:
Ah yes, I stupidly made an assumption that on x and x + \mathrm{d}x edges, where y = const., the forces don't have the y component. I then tailored my derivation around this assumption.

If I now try it again.
Force on x and x + \mathrm{d}x edges is \gamma \sqrt{\mathrm{d}y^2 + \mathrm{d}z^2}. This force is tangent to the surface and perpendicular to the edge. The normal to the surface is \mathbf{n} = \left( -z_x, -z_y, 1 \right) (I'm not normalizing the vectors here) and the edge has the direction \mathbf{s} = \left( 0, 1, z_y \right). The force then must be perpendicular to both this vectors and has the direction, \mathbf{s} \times \mathbf{n} = \left( 1 + z_y^2, -z_x z_y, z_x \right). The z component of the force is then proportional to \frac{z_x}{\sqrt{\left( 1 + z_y^2 \right)^2 + z_x^2 z_y^2 + z_x^2}} = \frac{z_x}{\sqrt{1 + z_y^2} \sqrt{1 + z_x^2 + z_y^2}}.
Similarly for the other two edges.

Similarly as before I sum the forces over the edges and with \mathrm{d}_x mark a small difference between x - \mathrm{d}x (force of the left neighbouring element) and x + \mathrm{d}x (force of the right neighbouring element). The forces are then,
<br /> \mathrm{d}_x \left( \gamma \mathrm\, {d}y \, \frac{z_x}{\sqrt{1 + z_x^2 + z_y^2}} \right) + \mathrm{d}_y \left( \gamma \mathrm\, {d}x \, \frac{z_y}{\sqrt{1 + z_x^2 + z_y^2}} \right) = 0.<br />
Divide this by 2 \gamma \, \mathrm{d}x \, \mathrm{d}y and you get the Plateau equation.


Thank you for your input. It's been very helpful.
 
That all looks correct to me. Good.
 

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