Where does the equation of the velocity of a free vortex come from?

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The equation for the velocity of a free vortex, given by v = c/r, arises from the characteristics of a curl-free vector field, which is singular along the z-axis. This equation reflects the irrotational nature of the free vortex, contrasting with the forced vortex where velocity is proportional to the radius (v = rω). The discussion highlights the significance of the circulation constant 'c' and the line integral around the z-axis, which yields a non-zero value, indicating the presence of circulation. Additionally, the potential function associated with this velocity field is defined in regions excluding the z-axis, emphasizing the non-simply connected nature of the domain. Understanding these concepts is crucial for grasping the behavior of fluid dynamics in vortex systems.
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I am aware of the equation of the velocity of a forced vortex, which is simply ## v = r\omega ##. However, the velocity for a free vortex is ## v = \frac{c}{r} ## (## c ## is the 'circulation constant', ## r ## is the radius, ## v ## is the velocity and ## \omega ## is the angular velocity). I understand why you should expect to see a difference in the equations for both the vortices since the free vortex doesn't have a radial velocity, but where does the equation come from?
 
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I'm not so sure what you are after. First of all velocities are vectors (for you first equation) or vector fields.

Your first equation describes the velocity of a point particle rotating around an axis. The full equation is $$\vec{v}=\vec{\omega} \times \vec{r},$$
where ##\vec{\omega}## is the angular velocity and ##\vec{r}## the position vector of the particle (with the origin of the reference frame on the axis of rotation).

Proof: Take the rotation axis to be the ##z##-axis of a Cartesian coordinate system and the particle being in the ##xy## plane. For a constant angular velocity you have
$$\vec{r}(t)=a \begin{pmatrix} \cos(\omega t) \\ \sin \omega t \\ 0 \end{pmatrix},$$
and the velocity is
$$\vec{v}(t)=\dot{\vec{r}}(t)=a \omega \begin{pmatrix} -\sin \omega t \\ \cos \omega \\ 0 \end{pmatrix}.$$
Now ##\vec{\omega}=(0,0,\omega)^{\text{T}}## and thus indeed
$$\vec{v}=\vec{\omega} \times \vec{r}.$$

The second equation describes the velocity field of a fluid. In Cartesian coordinates the correct equation is
$$\vec{v}(\vec{r})=\frac{c}{x^2+y^2} \begin{pmatrix} -y \\ x \\0 \end{pmatrix}.$$
Note that this is a curl-free vector field everywhere except along the ##z##-axis, where it is singular. Nevertheless the line integral along any closed curve going once around the ##z##-axis gives the value ##2 \pi c##. It's an example for a potential field in a non simply connected domain. It's thus called the "potential vortex".
 
vanhees71 said:
I'm not so sure what you are after. First of all velocities are vectors (for you first equation) or vector fields.

Your first equation describes the velocity of a point particle rotating around an axis. The full equation is $$\vec{v}=\vec{\omega} \times \vec{r},$$
where ##\vec{\omega}## is the angular velocity and ##\vec{r}## the position vector of the particle (with the origin of the reference frame on the axis of rotation).

Proof: Take the rotation axis to be the ##z##-axis of a Cartesian coordinate system and the particle being in the ##xy## plane. For a constant angular velocity you have
$$\vec{r}(t)=a \begin{pmatrix} \cos(\omega t) \\ \sin \omega t \\ 0 \end{pmatrix},$$
and the velocity is
$$\vec{v}(t)=\dot{\vec{r}}(t)=a \omega \begin{pmatrix} -\sin \omega t \\ \cos \omega \\ 0 \end{pmatrix}.$$
Now ##\vec{\omega}=(0,0,\omega)^{\text{T}}## and thus indeed
$$\vec{v}=\vec{\omega} \times \vec{r}.$$

The second equation describes the velocity field of a fluid. In Cartesian coordinates the correct equation is
$$\vec{v}(\vec{r})=\frac{c}{x^2+y^2} \begin{pmatrix} -y \\ x \\0 \end{pmatrix}.$$
Note that this is a curl-free vector field everywhere except along the ##z##-axis, where it is singular. Nevertheless the line integral along any closed curve going once around the ##z##-axis gives the value ##2 \pi c##. It's an example for a potential field in a non simply connected domain. It's thus called the "potential vortex".
Thanks for the reply, my question better put is, where does the second equation,
$$\vec{v}(\vec{r})=\frac{c}{x^2+y^2} \begin{pmatrix} -y \\ x \\0 \end{pmatrix}.$$
come from. Is it simply that equation because the velocity field of that equation matches the description of a free vortex (i.e. irrotational).
 
Yes, it's simply used as an example for a curl- and source-free vector field (except along the ##z##-axis, where it's singular!), for which
$$\int_C \mathrm{d} \vec{r} \cdot \vec{v}(\vec{r}) = 2 \pi c \neq 0$$
for any closed curve that encircles the ##z##-axis.

It emphasizes the importance that form ##\vec{\nabla} \times \vec{v}## you can only conclude ##\vec{v}=-\vec{\nabla} \phi## locally, i.e., in simply-connected regions around a regular point.

Now globally, the Euclidean ##\mathbb{R}^3## with the ##z##-axis taken out is not simply connected.

To see that ##\vec{v}## has a unique potential only in a region with an entire half-plane with the ##z##-axis as boundary taken out, rewrite it in terms of the usual cylinder coordinates ##(\rho,\varphi,z)##. It's easy to see that it can be written as
$$\vec{v}(\vec{r})=\frac{c}{\rho} \vec{e}_{\varphi}.$$
Obviously it has a local potential in every simply-connected neighborhood of any point not on the ##z##-axis. Since it's only in direction of ##\vec{e}_{\varphi}##, it's suggestive to assume that the potential is a function of ##\varphi## only. Indeed the gradient in cylinder coordinates gives
$$\vec{\nabla} \phi(\varphi)=\frac{1}{\rho} \vec{e}_{\varphi} \partial_\varphi \phi \stackrel{!}{=}-\vec{v}=-\frac{c}{\rho} \vec{e}_{\varphi} \; \rightarrow \; \phi(\varphi)=-c \varphi.$$
Now to get the potential unique, you have to take out some half-plane with the ##z##-axis as boundary. You can, e.g., choose the ##(x,z)##-half-plane with ##x<0##. Then you can choose ##\varphi \in ]-\pi,\pi]##. Then the potential makes a jump at any point on this half-plane by a value of ##2 \pi c##, and indeed that's the value you get for the integral along a closed loop around the ##z##-axis.
 
This has been discussed many times on PF, and will likely come up again, so the video might come handy. Previous threads: https://www.physicsforums.com/threads/is-a-treadmill-incline-just-a-marketing-gimmick.937725/ https://www.physicsforums.com/threads/work-done-running-on-an-inclined-treadmill.927825/ https://www.physicsforums.com/threads/how-do-we-calculate-the-energy-we-used-to-do-something.1052162/
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