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

In summary: I'm not so sure what you are after. First of all velocities are vectors (for you first equation) or vector fields.
  • #1
I_laff
41
2
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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  • #2
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".
 
  • #3
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).
 
  • #4
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.
 

1. What is a free vortex?

A free vortex is a type of flow in a fluid where the particles rotate around a central axis without any external forces acting on them. This type of flow is often seen in tornadoes and whirlpools.

2. What is the equation for the velocity of a free vortex?

The equation for the velocity of a free vortex is v = (g/2π)ln(r/r0), where v is the tangential velocity, g is the strength of the vortex, r is the distance from the center of the vortex, and r0 is a reference radius.

3. Where does this equation come from?

The equation for the velocity of a free vortex is derived from the conservation of angular momentum in a fluid. It takes into account the circular motion of the fluid particles and the balance between the centrifugal force and the pressure gradient force.

4. What are the assumptions made in this equation?

The equation for the velocity of a free vortex assumes that the fluid is inviscid (has no internal friction), incompressible, and irrotational (no net rotation). It also assumes that the vortex is axisymmetric (has a circular cross-section) and that the flow is steady.

5. Can this equation be applied to all types of vortices?

No, this equation is specifically for a free vortex, where there are no external forces acting on the fluid particles. Other types of vortices, such as forced vortices or line vortices, have different equations for their velocity profiles.

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