A Why is circulation zero for irrotational vortices outside their axis?

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In irrotational vortices, the circulation is zero for any closed contour that does not enclose the vortex axis, while it has a fixed value for contours that do. This phenomenon is explained by the fact that the curl of the velocity field is zero everywhere except along the vortex axis, as shown through mathematical derivations involving Helmholtz's Second Theorem. Vortex tubes must either close on themselves or terminate at fluid boundaries due to the conservation of circulation in fluid dynamics. The discussion also touches on the singular nature of the vortex at its axis and the implications for the behavior of vortices, including the possibility of splitting. Understanding these principles is crucial for analyzing fluid mechanics and vortex dynamics.
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Hi PF!

For an irrotational vortex, the circulation is zero along any closed contour that does not enclose the vortex axis; and has a fixed value, ##\Gamma##, for any contour that does enclose the axis once. Why?

Secondly, why must vortex tubes close on themselves or begin/end at fluid boundaries?

Thanks so much!
 
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joshmccraney said:
Secondly, why must vortex tubes close on themselves or begin/end at fluid boundaries?

This is due to Helmholtz's Second Theorem
 
If you have an irrotational vortex you have a flow filed ##\vec{v}(\vec{x})## (it can of course also be time dependent, but that's not important for my answer here), that means you have
$$\vec{\nabla} \times \vec{v}=0$$
everywhere except along some line. As an example take
$$\vec{v}=\frac{\Gamma}{2 \pi (x^2+y^2)} \begin{pmatrix} -y \\ x \\ 0 \end{pmatrix}.$$
This is defined everywhere except along the ##z## axis, and there you have
$$\vec{\nabla} \times \vec{v}=0.$$
To see, what's going on along the ##z## axis, we regularize this field by introducing a parameter ##\epsilon>0##:
$$\vec{v}_{\epsilon}(\vec{x})=\frac{\Gamma}{2 \pi (x^2+y^2+\epsilon^2)} \begin{pmatrix} -y \\ x \\ 0 \end{pmatrix}.$$
Calculating now the curl leads to
$$\vec{\nabla} \times \vec{v}_{\epsilon}=\vec{e}_z \frac{\Gamma \epsilon^2}{\pi(\epsilon^2+x^2+y^2)^2}.$$
Now for ##x^2+y^2 \neq 0## you get of course ##0## in the limit ##\epsilon \rightarrow 0##. For ##x^2+y^2=0## (i.e., along the ##z## axis) the limit ##\epsilon \rightarrow 0## diverges.

On the other hand you can integrate over any plane parallel to the ##xy## plane, leading to (using polar coordinates)
$$\int_{\mathbb{R}^2} \mathrm{d} x \mathrm{d} y \vec{e}_z \cdot \vec{\nabla} \times \vec{v}_{\epsilon}=2 \pi \int_0^{\infty} \mathrm{d} \rho \frac{ \rho \Gamma \epsilon^2}{\pi(\epsilon^2+x^2+y^2)^2}=\Gamma.$$
This means that
$$\vec{\nabla} \times \vec{v}=\lim_{\epsilon \rightarrow 0} \vec{\nabla} \times \vec{v}_{\epsilon}=\Gamma \delta(x)\delta(y).$$
Now calculate the circulation along any curve winding (once!) around the ##z## axis. Because ##\vec{\nabla} \times \vec{v}=0## everywhere except along the ##z## axis you can see using Stokes's theorem that for any such curve you get the same result, because you can cut the area encircelt by the two curves with two arbitrary lines and calculating the line integral over the corresponding two closed curves (leading finally to the integral along the one curve minus the one along the other), which don't contain the ##z## axis. Then you use Stokes theorem there, and since ##\vec{\nabla} \times \vec{v}=0## there you get ##0##, i.e., the line integrals along the original two curves give the same.

Now use a circle parallel to the ##xy## plane, and you get
$$\int_C \mathrm{d} \vec{x} \cdot \vec{v}=\Gamma.$$
 
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vanhees71 said:
Because ##\vec{\nabla} \times \vec{v}=0## everywhere except along the ##z## axis you can see using Stokes's theorem that for any such curve you get the same result, because you can cut the area encircelt by the two curves with two arbitrary lines and calculating the line integral over the corresponding two closed curves (leading finally to the integral along the one curve minus the one along the other), which don't contain the ##z## axis. Then you use Stokes theorem there, and since ##\vec{\nabla} \times \vec{v}=0## there you get ##0##, i.e., the line integrals along the original two curves give the same.
So every irrotational vortex has zero curl everywhere except at some origin of the vortex, which is I guess singular?
 
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Alexandre Chorin Jerrold E. Marsden A Mathematical Introduction
to Fluid Mechanics. Here ##\boldsymbol \xi=\mathrm{rot}\,\boldsymbol v##
 
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zwierz said:
Here ##\boldsymbol \xi=\mathrm{rot}\,\boldsymbol v##
What is the ##\mathrm{rot}## operator; some sort of rotation?

I'm trying to understand the last statement in the first paragraph, but I don't know what ##\mathrm{rot} \boldsymbol v## is.

Also, I'm unsure if a vortex could split in two; could you explain why or why not, or guide me to the answer?

Thanks for being so helpful!
 
rot=curl
 
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