2. The time-dependent spherical vortex family

2.1. Definition of the time-dependent velocity solution

In order to define the time-dependent velocity solution $\boldsymbol {u}(\boldsymbol {x},t)$, it is convenient to introduce first, in spherical coordinates $(r,\theta,\varphi )$ and time $t$, the oscillating, in both space and time, function

(2.1)$$\begin{gather} \boldsymbol{\mathcal{U}}(r,\theta,\varphi,t)\equiv u_1 \left[\ell(\ell+1)\,\frac{{\rm j}_{\ell}(kr)}{kr}\,\boldsymbol{Y}_{\ell}^{m}(\theta,\varphi) +\left( (\ell+1)\,\frac{ {\rm j}_{\ell}(kr)}{kr} - {\rm j}_{\ell+1}(kr) \right) \boldsymbol{\varPsi}_{\ell}^{m}(\theta,\varphi) \right.\nonumber\\ \left.{}+ {\rm j}_{\ell}(kr)\,\boldsymbol{\varPhi}_{\ell}^{m}(\theta,\varphi)\vphantom{\frac{{\rm j}_{\ell}(kr)}{kr}}\right] {\rm e}^{-{\rm i} m \mathfrak{w}t} , \end{gather}$$

where ${\rm j}_{\ell }(\,{\cdot}\, )$ is the spherical Bessel function of the first kind and degree $\ell$, and the vector set $\{ \boldsymbol {Y}_{\ell }^{m}(\theta,\varphi ), \boldsymbol {\varPsi }_{\ell }^{m}(\theta,\varphi ), \boldsymbol {\varPhi }_{\ell }^{m}(\theta,\varphi )\}$, with integers $\ell \ge 0$ and $m\in \{ -\ell,\ldots,\ell \}$, is the vector spherical harmonics basis (Barrera, Estevez & Giraldo Reference Barrera, Estevez and Giraldo1985). The remaining parameters are the radial wavenumber $k$, the oscillation velocity amplitude $u_1$, and the frequency, or angular speed, $\mathfrak {w}$. To simplify the notation, it is only shown explicitly in (2.1) the function in terms of the spherical Bessel functions of the first kind (hence the subscript 1 in the velocity amplitude $u_1$). This function assumes implicitly the addition of a similar function but whose radial dependence is given in terms of the spherical Bessel functions of the second kind ${\rm y}_{\ell }(\,{\cdot}\, )$ instead of ${\rm j}_{\ell }(\,{\cdot}\, )$, and with a new constant velocity amplitude, say $u_2$ instead of $u_1$. Also, the indices $\ell, m$ will generally be omitted from the symbols $\boldsymbol {\mathcal {U}}$, etc. The oscillating function (2.1) is divergence-free ($\boldsymbol {\nabla }\boldsymbol {\cdot }\boldsymbol {\mathcal {U}}=0$), and when $\mathfrak {w} \mapsto 0$, equals the steady multipolar vortex solutions given in Viúdez (Reference Viúdez2022). We notice that in the general time-dependent case ($m\mathfrak {w}\neq 0$), the time-dependent function (2.1) is not a solution of the vorticity equation (1.1).

Next, we define the rigid motion

(2.2)\begin{equation} \bar{\boldsymbol{u}}(r,\theta) \equiv{-}2\,\frac{\mathfrak{w}}{k} \left( \cos\theta\, \hat{\boldsymbol{r}} - \sin\theta\,\hat{\boldsymbol{\theta}} \right) + \mathfrak{w} r \sin\theta\, \hat{\boldsymbol{\varphi}} = \rho \mathfrak{w} \hat{\boldsymbol{\varphi}} - \frac{2\mathfrak{w}}{k}\,\hat{\boldsymbol{z}} , \end{equation}

where the last equality, which provides the cylindrical components in cylindrical coordinates $(\rho,\varphi,z)$, shows more clearly that (2.2) is a cylindrical axial motion with swirl, having azimuthal velocity $\rho \mathfrak {w}\hat {\boldsymbol {\varphi }}$ and axial velocity $(-2\mathfrak {w}/k)\hat {\boldsymbol {z}}$. Hence $\mathfrak {w}$ is the angular speed of the rigid motion. Finally, from (2.1) and (2.2), we define the time-dependent velocity field family

(2.3)\begin{equation} \boldsymbol{u}(r,\theta,\varphi,t) \equiv \boldsymbol{\mathcal{U}}(r,\theta,\varphi,t) + \bar{\boldsymbol{u}}(r,\theta), \end{equation}

which is a time-dependent multipolar solution of (1.1) in spherical geometry. Since the time-dependent velocity oscillations have a local frequency ($m\mathfrak {w}$) proportional to the angular speed of the background flow ($\mathfrak {w}$), the time oscillations in (2.3) may be interpreted as inertial oscillations in background flow. The next subsection proves that the family of flows (2.3) satisfies the vorticity equation (1.1).

2.2. Proof that the velocity (2.3) satisfies (1.1)

First, we notice that the vorticity fields of (2.1) and (2.2) are

(2.4a,b)\begin{equation} \boldsymbol{\mathcal{W}} \equiv \boldsymbol{\nabla} \times \boldsymbol{\mathcal{U}} ={-} k \boldsymbol{\mathcal{U}} \quad {\rm and} \quad \bar{\boldsymbol{\omega}} \equiv \boldsymbol{\nabla} \times \bar{\boldsymbol{u}} = 2 \mathfrak{w} \hat{\boldsymbol{z}} , \end{equation}

and therefore the vorticity $\boldsymbol {\omega }(\boldsymbol {x},t)$ of the total flow is

(2.5)\begin{equation} \boldsymbol{\omega} ={-}k \boldsymbol{\mathcal{U}} + 2 \mathfrak{w}\hat{\boldsymbol{z}}. \end{equation}

Thus $\boldsymbol {\mathcal {U}}$ is a Beltrami function (an eigenfunction of the curl operator), and $\bar {\boldsymbol {\omega }}$ is a constant vertical vorticity. Consequently,

(2.6a,b)\begin{equation} \boldsymbol{\mathcal{W}} \times \boldsymbol{\mathcal{U}}=\boldsymbol{0} \quad {\rm and} \quad \bar{\boldsymbol{l}} \equiv \bar{\boldsymbol{\omega}} \times \bar{\boldsymbol{u}} ={-}2 \rho \mathfrak{w}^2 \hat{\boldsymbol{\rho}} , \end{equation}

that is, the Lamb vector of the oscillating function vanishes, and the Lamb vector of the rigid motion is radial. Therefore, the Lamb vector of the total flow $\boldsymbol {l}$ simplifies to

(2.7)\begin{equation} \boldsymbol{l} \equiv \boldsymbol{\omega} \times \boldsymbol{u} = \mathfrak{w} k\rho \hat{\boldsymbol{\varphi}} \times \boldsymbol{\mathcal{U}} + \bar{\boldsymbol{l}}, \end{equation}

which is the sum of the Lamb vector of the rigid motion $\bar {\boldsymbol {l}}$ and a nonlinear contribution from the oscillating and rigid motions. We notice from (2.7) and (2.6b) the important property that the azimuthal component of the Lamb vector of this vortex family vanishes:

(2.8)\begin{equation} \boldsymbol{l} \boldsymbol{\cdot} \hat{\boldsymbol{\varphi}} =0 . \end{equation}

Property (2.8) implies that the azimuthal component of the acceleration equation simplifies to

(2.9)\begin{equation} \frac{\partial\mathcal{U}_{\varphi}}{\partial t} = \frac{1}{\rho}\,\frac{\partial}{\partial\varphi} \left( P - \frac{1}{2}\,\boldsymbol{u}\boldsymbol{\cdot}\boldsymbol{u} \right) , \end{equation}

where $\mathcal {U}_{\varphi }\equiv \boldsymbol {\mathcal {U}}\boldsymbol {\cdot }\boldsymbol {\varphi }$ is the azimuthal component of the oscillating function, and $P$ is the acceleration potential ($\boldsymbol {a}=\boldsymbol {\nabla } P$). Clearly, the curl of the Lamb vector of the rigid motion vanishes,

(2.10)\begin{equation} \boldsymbol{\nabla} \times \bar{\boldsymbol{l}} = \boldsymbol{0} , \end{equation}

and the curl of the Lamb vector of the total flow (see Appendix A) is

(2.11)\begin{equation} \boldsymbol{\nabla} \times \boldsymbol{l} ={-}{\rm i} m \mathfrak{w} k \boldsymbol{\mathcal{U}} . \end{equation}

This is a remarkably property. It states that for the family of vortex solutions (2.3), the curl of the Lamb vector $\boldsymbol {l}$, which is defined through the nonlinear relation $\boldsymbol {l}\equiv \boldsymbol {\omega }\times \boldsymbol {u}$, satisfies in fact a very simply linear relation with $\boldsymbol {\mathcal {U}}$. The curl of the Lamb vector of the total flow $\boldsymbol {l}$ is a rotation by an azimuthal angle increment $\Delta \varphi = {\rm \pi}/2$ of the oscillating velocity function $-\boldsymbol {\mathcal {U}}$ times $m\mathfrak {w}k$. Expression (2.11) is consistent with $\boldsymbol {\mathcal {U}}$ being solenoidal ($\boldsymbol {\nabla } \boldsymbol {\cdot } \boldsymbol {\mathcal {U}}=0$). Generalized Beltrami flows ($\boldsymbol {\nabla } \times \boldsymbol {l}=\boldsymbol {0}$) correspond to the steady states with $m=0$ (Beltrami flow and rigid flow), or $\mathfrak {w}=0$ (only Beltrami flow), or $k=0$ (Hill's spherical vortex).

The local rate of change of (2.3) is

(2.12)\begin{equation} \frac{\partial \boldsymbol{u}}{\partial t} =\frac{\partial \boldsymbol{\mathcal{U}}}{\partial t} ={-}{\rm i}m\mathfrak{w} \boldsymbol{\mathcal{U}} , \end{equation}

and the local rate of change of the total vorticity $\boldsymbol {\omega }$ is, using (2.4a),

(2.13)\begin{equation} \frac{\partial \boldsymbol{\omega}}{\partial t} =\frac{\partial \boldsymbol{\mathcal{W}}}{\partial t} ={-}k\,\frac{\partial \boldsymbol{\mathcal{U}}}{\partial t} = {\rm i}m\mathfrak{w}k \boldsymbol{\mathcal{U}} , \end{equation}

which cancels with (2.11) and therefore proves that ${\boldsymbol {u}}$ from (2.3) satisfies (1.1).

2.3. Streamfunctions

Here, we provide the streamfunction $\boldsymbol {\psi }(\boldsymbol {x},t)$ of the total flow $\boldsymbol {u}$. First, we notice that for the oscillating function $\boldsymbol {\mathcal {U}}$, there exists a function

(2.14a–c)\begin{equation} \boldsymbol{\mathcal{F}} \equiv{-}\frac{1}{k}\,\boldsymbol{\mathcal{U}}, \quad \text{such that} \quad \boldsymbol{\nabla} \times \boldsymbol{\mathcal{F}} = \boldsymbol{\mathcal{U}} \quad \text{and} \quad \boldsymbol{\nabla} \boldsymbol{\cdot} \boldsymbol{\mathcal{F}} = 0 , \end{equation}

while for the streamfunction $\bar {\boldsymbol {\psi }}(\rho )$ of the rigid motion, we have

(2.15a–c)\begin{equation} \bar{\boldsymbol{\psi}}(\rho) \equiv{-}\frac{\mathfrak{w}}{k}\,\rho \, \hat{\boldsymbol{\varphi}} -\frac{\mathfrak{w}}{2}\,\rho^2 \, \hat{\boldsymbol{z}} , \quad \text{with} \quad \boldsymbol{\nabla} \times \bar{\boldsymbol{\psi}} = \bar{\boldsymbol{u}} \quad \text{and} \quad \boldsymbol{\nabla} \boldsymbol{\cdot} \bar{\boldsymbol{\psi}} = 0 . \end{equation}

From (2.14) and (2.15), we obtain the streamfunction $\boldsymbol {\psi }$ of the total flow:

(2.16a–c)\begin{equation} \boldsymbol{\psi} \equiv \boldsymbol{\mathcal{F}} + \bar{\boldsymbol{\psi}} , \quad \text{with} \quad \boldsymbol{\nabla} \times \boldsymbol{\psi} = \boldsymbol{u} \quad \text{and} \quad \boldsymbol{\nabla} \boldsymbol{\cdot} \boldsymbol{\psi} = 0 . \end{equation}

Using the mathematical identity

(2.17)\begin{equation} \boldsymbol{\nabla} \times \left( \boldsymbol{\nabla} \times \boldsymbol{X} \right) = \boldsymbol{\nabla}\left( \boldsymbol{\nabla} \boldsymbol{\cdot} \boldsymbol{X} \right) - \boldsymbol{\nabla}^2\boldsymbol{X} \end{equation}

applied to $\boldsymbol {\psi }$, we obtain readily the relation between vorticity and the Laplacian of the streamfunction:

(2.18)\begin{equation} \boldsymbol{\omega} ={-} \boldsymbol{\nabla}^2 \boldsymbol{\psi} . \end{equation}

2.4. Frequencies and phase speed

The angular phase of $\boldsymbol {u}$ from (2.3) is the phase of $\boldsymbol {\mathcal {U}}$ from (2.1) and is given by

(2.19)\begin{equation} \varTheta(\varphi,t)\equiv m(\varphi - \mathfrak{w}t) . \end{equation}

The local frequency $\omega _l$ of the oscillating motion is

(2.20)\begin{equation} \omega_l \equiv{-}\frac{\partial\varTheta}{\partial t} = m \mathfrak{w} , \end{equation}

while the physical $\boldsymbol {\nabla }\varTheta$ wavenumber is only azimuthal:

(2.21)\begin{equation} \boldsymbol{\nabla}\varTheta = \frac{m}{r \sin\theta}\,\hat{\boldsymbol{\varphi}} = \frac{m}{\rho}\,\hat{\boldsymbol{\varphi}} . \end{equation}

The intrinsic frequency $\omega _i$, defined as the rate of change of the phase $\varTheta$ from (2.19) for an observer moving with the background rigid flow $\bar {\boldsymbol {u}}$ vanishes since

(2.22)\begin{equation} \omega_i \equiv{-}\left( \frac{\partial\varTheta}{\partial t} + \bar{\boldsymbol{u}} \boldsymbol{\cdot} \boldsymbol{\nabla}\varTheta \right) = 0 . \end{equation}

The phase velocity $\boldsymbol {\sigma }$ is the velocity satisfying

(2.23a–c)\begin{equation} \frac{\partial\varTheta}{\partial t} + {\boldsymbol{\sigma}} \boldsymbol{\cdot} \boldsymbol{\nabla}\varTheta = 0 \quad \text{and} \quad {\boldsymbol{\sigma}} \times \boldsymbol{\nabla}\varTheta = \boldsymbol{0} \quad \Rightarrow \quad {\boldsymbol{\sigma}} = \rho \mathfrak{w} \, \hat{\boldsymbol{\varphi}}, \end{equation}

and therefore the phases of the oscillating motion $\boldsymbol {\mathcal {U}}(\boldsymbol {x},t)$ move with the constant azimuthal flow $\rho \mathfrak {w}\hat {\boldsymbol {\varphi }}$, while the angular phase velocity is $\mathfrak {w}\hat {\boldsymbol {\varphi }}$.

2.5. Divergence of the Lamb vector

Besides the curl of the Lamb vector given in (2.11), the divergence of the Lamb vector $\boldsymbol {\nabla } \boldsymbol {\cdot } \boldsymbol {l}$ is also relevant (Hamman, Klewicki & Kirby Reference Hamman, Klewicki and Kirby2008) because for isochoric flows, it equals the Laplacian of the acceleration potential. Introducing the potential $\chi (\boldsymbol {x},t)$ given by

(2.24)\begin{equation} \chi \equiv P - \frac{1}{2}\,\boldsymbol{u}\boldsymbol{\cdot}\boldsymbol{u} \end{equation}

in Lagrange's expression for the acceleration field $\boldsymbol {a}(\boldsymbol {x},t)$,

(2.25)\begin{equation} \boldsymbol{a} \equiv \frac{\partial\boldsymbol{u}}{\partial t} + \boldsymbol{l} + \frac{1}{2}\,\boldsymbol{\nabla}\left( \boldsymbol{u}\boldsymbol{\cdot}\boldsymbol{u} \right) = \boldsymbol{\nabla} P , \end{equation}

we may write Euler's equation of motion as

(2.26)\begin{equation} \frac{\partial\boldsymbol{u}}{\partial t} + \boldsymbol{l} = \boldsymbol{\nabla} \chi , \end{equation}

and therefore the divergence of the Lamb vector

(2.27)\begin{equation} \boldsymbol{\nabla} \boldsymbol{\cdot} \boldsymbol{l} = \nabla^2 \chi \end{equation}

equals the Laplacian of the potential $\chi$. If $\boldsymbol {l}(\boldsymbol {x},t)$ is known, then the potential $\chi (\boldsymbol {x},t)$ can be obtained by solving the Poisson equation (2.27). Noticing that the divergence of the Lamb vector of the rigid motion is

(2.28)\begin{equation} \boldsymbol{\nabla} \boldsymbol{\cdot} \bar{\boldsymbol{l}} ={-}4 \mathfrak{w}^2 , \end{equation}

that $\boldsymbol {\nabla } \times (\rho \hat {\boldsymbol {\varphi }}) = 2 \hat {\boldsymbol {z}}$, and using the mathematical identity

(2.29)\begin{equation} \boldsymbol{\nabla} \boldsymbol{\cdot} \left( \boldsymbol{{X}} \times \boldsymbol{{Y}} \right) = \boldsymbol{{Y}} \boldsymbol{\cdot} \left( \boldsymbol{\nabla} \times \boldsymbol{{X}} \right) - \boldsymbol{{X}} \boldsymbol{\cdot} \left( \boldsymbol{\nabla} \times \boldsymbol{{Y}} \right) , \end{equation}

which implies that

(2.30)\begin{equation} \boldsymbol{\nabla} \boldsymbol{\cdot} \boldsymbol{l} = \boldsymbol{u}\boldsymbol{\cdot} \boldsymbol{\nabla} \times \boldsymbol{\omega} - \boldsymbol{\omega} \boldsymbol{\cdot} \boldsymbol{\omega} , \end{equation}

we finally obtain

(2.31)\begin{equation} \boldsymbol{\nabla} \boldsymbol{\cdot} \boldsymbol{l} = \mathfrak{w} k \left( k \rho \boldsymbol{\mathcal{U}} \boldsymbol{\cdot} \hat{\boldsymbol{\varphi}} + 2 \boldsymbol{\mathcal{U}} \boldsymbol{\cdot} \hat{\boldsymbol{z}} \right) - 4 \mathfrak{w}^2 . \end{equation}

Thus the divergence of the Lamb vector is the sum of a constant term ($-4\mathfrak {w}^2$) associated with the rigid flow and a term that depends only on the axial and azimuthal components of the oscillating flow $\boldsymbol {\mathcal {U}}$. The divergence of $\boldsymbol {l}$ is therefore independent of the $\rho$-component of the oscillating flow $\boldsymbol {\mathcal {U}}\boldsymbol {\cdot }\hat {\boldsymbol {\rho }}$.

2.6. Acceleration potential

It is possible to obtain the acceleration potential $P$ for the velocity flow solutions $\boldsymbol {u}$ in the general case. We introduce the spherical velocity components

(2.32)\begin{equation} \boldsymbol{\mathcal{U}}(r,\theta,\varphi,t) = \left( \mathcal{U}_s(r,\theta)\,\hat{\boldsymbol{r}} + \mathcal{V}_s(r,\theta)\,\hat{\boldsymbol{\theta}} + \mathcal{W}_s(r,\theta)\, \hat{\boldsymbol{\varphi}} \right) \exp({{\rm i} m (\varphi - \mathfrak{w}t)}) . \end{equation}

From the azimuthal component of (2.26), using the properties (2.8) and (2.12), we obtain

(2.33)\begin{equation} -{\rm i} m \mathfrak{w} \rho \boldsymbol{\mathcal{U}} \boldsymbol{\cdot} \hat{\boldsymbol{\varphi}} ={-}{\rm i} m \mathfrak{w} \rho\,\mathcal{W}_s (r,\theta) \exp({{\rm i} m (\varphi - \mathfrak{w}t)}) = \frac{\partial \chi}{\partial \varphi} , \end{equation}

where $\mathcal {W}_s(r,\theta ) \exp ({{\rm i} m (\varphi - \mathfrak {w}t)})$ is the azimuthal component of $\boldsymbol {\mathcal {U}}$. Since the acceleration potential of the rigid motion satisfies

(2.34a,b)\begin{equation} \boldsymbol{\nabla} \boldsymbol{\cdot} \bar{\boldsymbol{l}} ={-} 4 \mathfrak{w}^2 = \boldsymbol{\nabla}^2 \bar{\chi}, \quad \text{then} \quad \bar{\chi} ={-} \mathfrak{w}^2 \rho^2 . \end{equation}

Integration of (2.33) leads to

(2.35)\begin{equation} \chi ={-} \mathfrak{w}\rho \boldsymbol{\mathcal{U}} \boldsymbol{\cdot} \hat{\boldsymbol{\varphi}} - \mathfrak{w}^2 \rho^2 ={-} \left( \boldsymbol{\mathcal{U}} \boldsymbol{\cdot} \hat{\boldsymbol{\varphi}} + \mathfrak{w} \rho \right)\mathfrak{w}\rho ={-} \mathfrak{w}\rho \, \boldsymbol{u} \boldsymbol{\cdot} \hat{\boldsymbol{\varphi}}, \end{equation}

and therefore the acceleration potential $P(\boldsymbol {x},t)$ is simply

(2.36a,b)\begin{equation} P = e - \mathfrak{w}\rho \, \boldsymbol{u} \boldsymbol{\cdot} \hat{\boldsymbol{\varphi}} , \quad \text{where} \ e \equiv \frac{1}{2}\,\boldsymbol{u} \boldsymbol{\cdot} \boldsymbol{u} \end{equation}

is the kinetic energy density of the total flow.

3. Solutions satisfying the Navier–Stokes equation

The family of vortex solutions $\hat {\boldsymbol {u}}(\boldsymbol {x},t)$ defined from $\boldsymbol {\mathcal {U}}(\boldsymbol {x},t)$ in (2.1) and $\bar {\boldsymbol {u}}(\boldsymbol {x})$ in (2.2) as

(3.1)\begin{equation} \hat{\boldsymbol{u}}(\boldsymbol{x},t) \equiv \boldsymbol{\mathcal{U}}(\boldsymbol{x},t)\,{\rm e}^{-\nu k^2 t} + \bar{\boldsymbol{u}}(\boldsymbol{x}) \end{equation}

satisfies the Navier–Stokes equation

(3.2)\begin{equation} \frac{\partial \boldsymbol{\hat{\omega}}}{\partial t} + \boldsymbol{\nabla} \times \left( \hat{\boldsymbol{\omega}} \times \hat{\boldsymbol{u}} \right) = \nu\,\nabla^2 \hat{\boldsymbol{\omega}}, \end{equation}

where $\nu$ is a constant, assumed complex-valued, momentum diffusivity. We notice that in (3.1), the diffusivity affects the oscillating motion and not the rigid motion $\bar {\boldsymbol {u}}$ in (2.2), whose Laplacian vanishes. In order to prove that (3.1) satisfies (3.2), we define the new velocity $\hat {\boldsymbol {\mathcal {U}}}(\boldsymbol {x},t)$ and vorticity $\hat {\boldsymbol {\mathcal {W}}}(\boldsymbol {x},t)$ fields of the oscillating motion as

(3.3a,b)\begin{equation} \hat{\boldsymbol{\mathcal{U}}}(\boldsymbol{x},t) \equiv \boldsymbol{\mathcal{U}}(\boldsymbol{x},t)\, {\rm e}^{-\nu k^2 t}\quad \text{and} \quad \hat{\boldsymbol{\mathcal{W}}}(\boldsymbol{x},t) \equiv \boldsymbol{\nabla} \times \hat{\boldsymbol{\mathcal{U}}} ={-} k \hat{\boldsymbol{\mathcal{U}}} , \end{equation}

which imply that

(3.4a,b)\begin{equation} \hat{\boldsymbol{u}}(\boldsymbol{x},t) = \hat{\boldsymbol{\mathcal{U}}} + \bar{\boldsymbol{u}} \quad \text{and} \quad \hat{\boldsymbol{\omega}}(\boldsymbol{x},t) \equiv \boldsymbol{\nabla}\times\hat{\boldsymbol{u}} = \hat{\boldsymbol{\mathcal{W}}} + \bar{\boldsymbol{\omega}} = \boldsymbol{\mathcal{W}}\,{\rm e}^{-\nu k^2 t} + \bar{\boldsymbol{\omega}} . \end{equation}

Therefore, the local rate of change of vorticity is

(3.5)\begin{equation} \frac{\partial \hat{\boldsymbol{\omega}}}{\partial t} ={-}{\rm i} m \mathfrak{w} \hat{\boldsymbol{\mathcal{W}}} - \nu k^2 \hat{\boldsymbol{\mathcal{W}}} , \end{equation}

while the curl of the Lamb vector and the Laplacian of the vorticity are

(3.6a,b)\begin{equation} \boldsymbol{\nabla} \times \hat{\boldsymbol{l}} = {\rm i} m \mathfrak{w} \hat{\boldsymbol{\mathcal{W}}} \quad \text{and} \quad \boldsymbol{\nabla}^2 \hat{\boldsymbol{\omega}} ={-} k^2 \hat{\boldsymbol{\mathcal{W}}} , \end{equation}

which immediately prove (3.2). For complex-valued $\nu =\nu _r + {\rm i}\nu _i$, where $\nu _r,\nu _i \in \mathbb {R}$, the imaginary part $\nu _i$ represents oscillations of frequency

(3.7)\begin{equation} \hat{\mathfrak{w}}(k) \equiv \nu_i k^2 \end{equation}

in the flow $\hat {\boldsymbol {u}}(\boldsymbol {x},t)$, which may take place even in the particular case where the oscillations correspond to the zonal spherical harmonics solution ($m=0$).

4. Transformation under a change of frame translating with constant axial velocity

The velocity solution $\boldsymbol {u}$ in (2.3) includes the rigid motion $\bar {\boldsymbol {u}}(\rho )$ in (2.2), which includes a constant vertical velocity $(-2\mathfrak {w}/k)\hat {\boldsymbol {z}}$, and an azimuthal velocity $\mathfrak {w}\rho \hat {\boldsymbol {\varphi }}$. It therefore becomes interesting to generalize the solution $\boldsymbol {u}$ so as to make it valid in a reference frame translating with an arbitrary constant axial velocity (addressed in this section) and rotating with an arbitrary constant angular velocity (addressed in the next section). The mathematical expressions involving changes of frame moving with constant axial velocity become simpler in cylindrical coordinates. We introduce the cylindrical velocity components of the steady multipolar solution $\boldsymbol {\mathcal {U}}_0(\boldsymbol {x})\equiv \boldsymbol {\mathcal {U}}(\boldsymbol {x},t;\mathfrak {w}\mapsto 0)$ from (2.1) as

(4.1)\begin{equation} \boldsymbol{\mathcal{U}}_0(\rho,\varphi,z) \equiv \left( \mathcal{U}_c(\rho,z)\, \hat{\boldsymbol{\rho}} + \mathcal{V}_c(\rho,z)\,\hat{\boldsymbol{\varphi}} + \mathcal{W}_c(\rho,z)\, \hat{\boldsymbol{z}} \right) {\rm e}^{{\rm i} m \varphi} . \end{equation}

In a reference frame translating with constant axial velocity $-w \hat {\boldsymbol {z}}$, the time-dependent solution (2.3), now written using (4.1) as

(4.2)\begin{equation} \boldsymbol{u}(\rho,\varphi,z,t) =\boldsymbol{\mathcal{U}}_0(\rho,\varphi-\mathfrak{w}t,z) + \mathfrak{w}\rho\hat{\boldsymbol{\varphi}}-(2\mathfrak{w}/k)\hat{\boldsymbol{z}}, \end{equation}

is

(4.3)\begin{equation} \tilde{\boldsymbol{u}}(\rho,\varphi,z,t) \equiv \boldsymbol{\mathcal{U}}_0(\rho,\varphi-\mathfrak{w}t,z-wt) + \rho \mathfrak{w} \hat{\boldsymbol{\varphi}} + \left( w - 2\mathfrak{w}/k \right) \hat{\boldsymbol{z}}. \end{equation}

Since this is a Galilean transformation of $\boldsymbol {u}(\boldsymbol {x},t)$, the acceleration $\boldsymbol {a}(\boldsymbol {x},t)$ of the flow remains invariant, which can be verified by noticing that the local and advective rates of change of velocity transform as

(4.4a,b)\begin{equation} \frac{\partial\tilde{\boldsymbol{u}}}{\partial t} = \frac{\partial\boldsymbol{u}}{\partial t} - w\, \frac{\partial\boldsymbol{\mathcal{U}}_0}{\partial z} \quad \text{and} \quad \tilde{\boldsymbol{u}} \boldsymbol{\cdot} \boldsymbol{\nabla}\tilde{\boldsymbol{u}} = \boldsymbol{u} \boldsymbol{\cdot} \boldsymbol{\nabla} \boldsymbol{u} + w\,\frac{\partial\boldsymbol{\mathcal{U}}_0}{\partial z} , \end{equation}

where functions $\boldsymbol {\mathcal {U}}_{0}$ are evaluated at $(\rho,\varphi,z-wt)$, so that the acceleration $\tilde {\boldsymbol {a}}(\boldsymbol {x},t)$ remains unchanged,

(4.5)\begin{equation} \tilde{\boldsymbol{a}} \equiv \frac{\partial\tilde{\boldsymbol{u}}}{\partial t} +\tilde{\boldsymbol{u}} \boldsymbol{\cdot} \boldsymbol{\nabla} \tilde{\boldsymbol{u}} = \boldsymbol{a}, \end{equation}

and, since $\boldsymbol {u}$ is a flow solution ($\boldsymbol {\nabla } \times {\boldsymbol {a}} = \boldsymbol {0}$), $\tilde {\boldsymbol {u}}$ is a flow solution as well ($\boldsymbol {\nabla } \times \tilde {\boldsymbol {a}} = \boldsymbol {0}$). We notice also that the phase of this solution,

(4.6)\begin{equation} \tilde{\varTheta}(\varphi,t) = m(\varphi - \mathfrak{w}t) = \varTheta(\varphi,t), \end{equation}

is invariant as well. The velocity solution $\tilde {\boldsymbol {u}}(\boldsymbol {x},t)$ in (4.3) has a new free parameter $w$, which may be interpreted as the (minus) axial velocity of an axially translating reference frame relative to which the velocity solution $\boldsymbol {u}(\boldsymbol {x},t)$ in (2.3) becomes $\tilde {\boldsymbol {u}}(\boldsymbol {x},t)$ in (4.3). Alternatively, $w\hat {\boldsymbol {z}}$ in $\tilde {\boldsymbol {u}}(\boldsymbol {x},t)$ from (4.3) may be interpreted as the velocity of displacement of $\boldsymbol {u}(\boldsymbol {x},t)$ from (2.3). Regardless of the interpretation, the particular case where

(4.7)\begin{equation} k w = 2\mathfrak{w} \end{equation}

is characterized by a velocity $\tilde {\boldsymbol {u}}(\boldsymbol {x},t)$ from (4.3) without rigid, or background, axial velocity.

5. Transformation under a change of frame translating and rotating with constant axial and angular velocities

In this section, we extend the results in the previous section to a reference frame that is both translating and rotating with constant axial and angular velocities. Using the cylindrical velocity components of the steady spatially oscillating vortex solution (4.1), we define the time-dependent velocity field

(5.1)\begin{equation} \hat{\boldsymbol{u}}(\rho,\varphi,z,t) \equiv \boldsymbol{\mathcal{U}}_0(\rho,\varphi-\mathfrak{w} t,z-w t) + \rho \mathfrak{w} \hat{\boldsymbol{\varphi}} + (w+w_0) \hat{\boldsymbol{z}}, \end{equation}

where $w_0$ is a new vertical velocity parameter. We define, in the usual way, the vorticity $\hat {\boldsymbol {\omega }} \equiv \boldsymbol {\nabla } \times \hat {\boldsymbol {u}}$ and Lamb vector $\hat {\boldsymbol {l}} \equiv \hat {\boldsymbol {\omega }} \times \hat {\boldsymbol {u}}$. From these definitions and applying the chain rule to (5.1), we obtain

(5.2)\begin{equation} \frac{\partial\hat{\boldsymbol{\omega}}}{\partial t} = \mathfrak{w} k\, \frac{\partial{\boldsymbol{\mathcal{U}}_0}}{\partial\varphi} + w k\, \frac{\partial{\boldsymbol{\mathcal{U}}_0}}{\partial z} \end{equation}

and

(5.3)\begin{equation} \boldsymbol{\nabla} \times \hat{\boldsymbol{l}} ={-}\mathfrak{w} k\, \frac{\partial\boldsymbol{\mathcal{U}}_0}{\partial\varphi} - (2\mathfrak{w} +(w+w_0) k )\,\frac{\partial\boldsymbol{\mathcal{U}}_0}{\partial z} , \end{equation}

where $\boldsymbol {\mathcal {U}}_0$ in the right-hand side of these and following equations is always evaluated at $(\rho,\varphi -\mathfrak {w}t,z-wt)$, whereas those in the left-hand side are evaluated at $(\rho,\varphi,z,t)$. Since the curl of the centripetal acceleration vanishes ($\boldsymbol {\nabla } \times (-\varOmega ^2\rho \hat {\boldsymbol {\rho }})=\boldsymbol {0}$), we need only to add to the vorticity equation the curl $\boldsymbol {\mathcal {C}}$ of the Coriolis acceleration $2 \varOmega \hat {\boldsymbol {z}} \times \hat {\boldsymbol {u}}$,

(5.4)\begin{equation} \boldsymbol{\mathcal{C}} \equiv \boldsymbol{\nabla} \times \left( 2 \varOmega \hat{\boldsymbol{z}} \times \hat{\boldsymbol{u}} \right) ={-} 2 \varOmega\,\frac{\partial\boldsymbol{\mathcal{U}}_0}{\partial z} , \end{equation}

to obtain the vorticity equation in the rotating non-inertial frame

(5.5)\begin{equation} \frac{\partial\hat{\boldsymbol{\omega}}}{\partial t} + \boldsymbol{\nabla} \times \hat{\boldsymbol{l}} + \boldsymbol{\nabla} \times \left( 2 \varOmega \hat{\boldsymbol{z}} \times \hat{\boldsymbol{u}} \right) = \boldsymbol{0} , \end{equation}

which implies

(5.6)\begin{equation} -\left[ w_0 k + 2(\mathfrak{w}+\varOmega) \right] \frac{\partial\boldsymbol{\mathcal{U}}_0}{\partial z} = \boldsymbol{0} . \end{equation}

Therefore, the velocity $\hat {\boldsymbol {u}}$ in (5.1) is a solution of the vorticity equation in a frame of reference rotating with constant angular velocity $\varOmega \hat {\boldsymbol {z}}$ relative to the inertial reference frame when

(5.7)\begin{equation} w_0 k ={-}2(\mathfrak{w}+\varOmega) . \end{equation}

Thus $\hat {\boldsymbol {u}}$ in (5.1) is a flow solution in an inertial reference frame ($\varOmega =0$) when $w_0 = -2\mathfrak {w}/k$, which corresponds to the time-dependent oscillating vortex solution $\boldsymbol {u}(\boldsymbol {x},t)$ in (2.3). Replacing $w_0$ from (5.7) in (5.1), we finally write the solution

(5.8)\begin{equation} \hat{\boldsymbol{u}}(\rho,\varphi,z,t) \equiv \boldsymbol{\mathcal{U}}_0(\rho,\varphi-\mathfrak{w} t,z-w t) + \rho \mathfrak{w} \hat{\boldsymbol{\varphi}} + \left( w - \frac{2(\mathfrak{w}+\varOmega)}{k} \right) \hat{\boldsymbol{z}} . \end{equation}

Thus $\hat {\boldsymbol {u}}$ in (5.8), with the free parameters $u_1,k,l,m,\mathfrak {w} , w , \varOmega$, is a flow solution of the vorticity equation in a reference frame (which is non-inertial when $\varOmega \neq 0$) moving with velocity $\rho \varOmega \hat {\boldsymbol {\varphi }}$ relative to the inertial one. We notice that now all the terms in the solution $\hat {\boldsymbol {u}}$ in (5.8) are relative to the rotating reference frame; for example, $\mathfrak {w}$ in (5.8) is the relative angular speed of the background flow. Solution (5.8) is relevant to geophysical flows as it describes inertial oscillations in vortices relative to a rotating sphere.

Though inertial oscillations are frequently associated with flows observed in a rotating non-inertial reference frame, we have seen here that this is not the case, since the waves exist in an inertial reference frame as long as there is a background rotation $\mathfrak {w}\ne 0$ and the oscillating function has a wavenumber $m \ne 0$. When the flow is steady in the inertial reference frame (and in the general case the oscillating flow has any wavenumber $m$), we have that $\mathfrak {w}=-\varOmega$ in the rotating frame (we notice that this is consistent with $\mathfrak {w}=0$ in the inertial reference frame characterized by $\varOmega =0$), and $w=0$, so solution (5.8) reduces to

(5.9)\begin{equation} \hat{\boldsymbol{u}}(\rho,\varphi,z,t) \equiv \boldsymbol{\mathcal{U}}_0(\rho,\varphi+\varOmega t,z) - \rho \varOmega \hat{\boldsymbol{\varphi}} , \end{equation}

which clearly differs from the solution $\boldsymbol {u}$ in (2.3) after the substitution $\mathfrak {w} \rightarrow -\varOmega$. The fact that (5.9) represents steady motion in the inertial reference frame is immediately proven by setting $\varOmega =0$.

Clearly, for zonal spherical harmonics ($m=0$) the flow has no azimuthal dependence, so we may write $\boldsymbol {\mathcal {U}}(\rho,\varphi -\mathfrak {w}t,z-wt)=\boldsymbol {\mathcal {U}}(\rho,\cdot,z-wt)$ in (5.8), and the relative angular speed $\mathfrak {w}$ has no effect in $\boldsymbol {\mathcal {U}}$, so the vortex remains steady in a reference frame translating with velocity $w\hat {\boldsymbol {z}}$. This fact, and the resulting exterior inertial waves associated with the axial translation of the vortex $w$ and with the angular speed of the rotating frame $\varOmega$, was addressed by Scase & Terry (Reference Scase and Terry2018) in the particular case $\ell =1$ for the spherical vortex of Hill ($k=0$) and the swirling spherical vortex of Hicks–Moffatt ($k\ne 0$).

Let us now consider a solution $\hat {\boldsymbol {u}}$ from (5.1) in an inertial reference frame ($\varOmega =0$). The flow with

(5.10)\begin{equation} w = 2\mathfrak{w}/k \end{equation}

is a velocity solution with vanishing background axial flow. The velocity $\check {\boldsymbol {u}}(\boldsymbol {x},t)$ of this particular solution is

(5.11)\begin{equation} \check{\boldsymbol{u}}(\rho,\varphi,z,t) \equiv \boldsymbol{\mathcal{U}}_0(\rho,\varphi-\mathfrak{w} t,z - (2 \mathfrak{w}/k) t) + \rho \mathfrak{w} \hat{\boldsymbol{\varphi}}. \end{equation}

Applying the chain rule to the solution with no background axial flow $\check {\boldsymbol {u}}(\boldsymbol {x},t)$ in (5.11), we find that the displacement velocity $\check {\boldsymbol {v}}$ of the velocity field $\check {\boldsymbol {u}}$, that is, satisfying the equation

(5.12a,b)\begin{equation} \frac{\partial\check{\boldsymbol{u}}}{\partial t} + \check{\boldsymbol{v}} \boldsymbol{\cdot} \boldsymbol{\nabla} \check{\boldsymbol{u}} = \boldsymbol{0} , \quad \text{is} \quad \check{\boldsymbol{v}} = \rho \mathfrak{w} \hat{\boldsymbol{\varphi}} + \frac{2\mathfrak{w}}{k}\,\hat{\boldsymbol{z}}. \end{equation}

Thus an observer moving with velocity $\check {\boldsymbol {v}}$ from (5.12b) will see no rate of change of velocity, as is also inferred directly from (5.11). The phase velocity $\boldsymbol {\sigma }=\rho \mathfrak {w}\hat {\boldsymbol {\varphi }}$ in (2.23) is azimuthal, therefore transverse to the axial direction, and it remains invariant to any inertial observer moving with an arbitrary axial velocity.

The velocity fields found here – $\boldsymbol {u}$ in (2.3), and its generalization to a translating and rotating reference frame $\hat {\boldsymbol {u}}$ in (5.8) – are solutions to the nonlinear vorticity equation (1.1). However, since the nonlinear term $\boldsymbol {\nabla }\times \boldsymbol {l}=-{\rm i}m\mathfrak {w}k\boldsymbol {\mathcal {U}}$ in (2.11) becomes a linear function of the velocity oscillation $\boldsymbol {\mathcal {U}}$, these solutions satisfy different linear wave equations as well. These wave equations are considered in the next section.

6. Wave equations

In order to obtain the wave equations for $\boldsymbol {u}$ and $\boldsymbol {\omega }$ (as well as for all their higher-degree curl fields), we notice that since $\boldsymbol {\nabla }\times \boldsymbol {\mathcal {U}}=-k\boldsymbol {\mathcal {U}}$ from (2.4a), and $\boldsymbol {\nabla }\boldsymbol {\cdot }\boldsymbol {\mathcal {U}}=0$, the velocity oscillations $\boldsymbol {\mathcal {U}}$, $\boldsymbol {\mathcal {W}}$, and all successive curls, satisfy the Helmholtz equations

(6.1a,b)\begin{equation} \nabla^2 \boldsymbol{u} = \nabla^2 \boldsymbol{\mathcal{U}} ={-}k^2 \boldsymbol{\mathcal{U}} \quad \text{and} \quad \nabla^2 \boldsymbol{w} = \nabla^2 \boldsymbol{\mathcal{W}} ={-}k^2 \boldsymbol{\mathcal{W}}. \end{equation}

Using the local rate of change of $\boldsymbol {u}$ from (2.12) and $\boldsymbol {\omega }$ from (2.13), we see that $\boldsymbol {\mathcal {U}}$, and hence $\boldsymbol {u}$, $\boldsymbol {\omega }$, and all successive curls, satisfy

(6.2a,b)\begin{equation} {\rm i}\,\frac{\partial \boldsymbol{u}}{\partial t} ={-} \frac{m \mathfrak{w}}{k^2}\, \boldsymbol{\nabla}^{2}\boldsymbol{u} \quad \text{and} \quad {\rm i}\,\frac{\partial \boldsymbol{\omega}}{\partial t} ={-} \frac{m \mathfrak{w}}{k^2}\,\boldsymbol{\nabla}^{2}\boldsymbol{\omega} . \end{equation}

These equations are similar to the time-dependent Schrödinger equations for a massive free particle. The similarity of these equations to the Schrödinger and Klein–Gordon equations is addressed in Appendix B. The second partial time derivatives of (6.2) imply that

(6.3a,b)\begin{equation} \frac{\partial^2 \boldsymbol{u}}{\partial t^2} =\frac{\partial^2 \boldsymbol{\mathcal{U}}}{\partial t^2} ={-} m^2 \mathfrak{w}^2 \boldsymbol{\mathcal{U}} \quad \text{and} \quad \frac{\partial^2 \boldsymbol{\omega}}{\partial t^2} = \frac{\partial^2 \boldsymbol{\mathcal{W}}}{\partial t^2} ={-} m^2 \mathfrak{w}^2 \boldsymbol{\mathcal{W}}, \end{equation}

and therefore $\boldsymbol {u}$ and $\boldsymbol {\omega }$ satisfy the classical wave equations

(6.4a,b)\begin{equation} \frac{1}{c^2}\,\frac{\partial^2 \boldsymbol{u}}{\partial t^2} -\boldsymbol{\nabla}^2 \boldsymbol{u} = \boldsymbol{0} \quad \text{and} \quad \frac{1}{c^2}\,\frac{\partial^2 \boldsymbol{\omega}}{\partial t^2} -\boldsymbol{\nabla}^2 \boldsymbol{\omega} = \boldsymbol{0}, \end{equation}

where the squared wave speed is

(6.5)\begin{equation} c^2 \equiv \frac{m^2 \mathfrak{w}^2}{k^2} . \end{equation}

The fact that both velocity $\boldsymbol {u}$ and vorticity $\boldsymbol {\omega }$ satisfy the wave equations (6.4a,b) makes it appealing to investigate the analogy between the propagation of these vortex oscillations and the propagation of electromagnetic waves in vacuum (see § 7). This analogy is interesting also because the angular phase velocity $\mathfrak {w}\hat {\boldsymbol {\varphi }}$ is transverse to the axial velocity and therefore is independent of the inertial reference frame translating with constant axial velocity addressed in § 4.

7. Maxwell equations for the propagation of electromagnetic waves in vacuum

We define the time-dependent fields $\boldsymbol {E}$ and $\boldsymbol {B}$ from the velocity $\boldsymbol {u}(\rho,\varphi,z,t)$ as

(7.1a,b)\begin{equation} {\mathrm{c}}\boldsymbol{E}\equiv \frac{\partial\boldsymbol{u}}{\partial t} \quad {\rm and} \quad \boldsymbol{B} \equiv{-}\boldsymbol{\nabla}\times\boldsymbol{u} ={-}\boldsymbol{\omega} , \end{equation}

where ${\mathrm{c}}$ is a constant identified with the speed of the electromagnetic waves in vacuum, but in principle independent of $c$. Fields $\boldsymbol {E}$ and $\boldsymbol {B}$ are solenoidal and therefore satisfy Gauss's laws for the magnetic ($\boldsymbol {\nabla }\boldsymbol {\cdot }\boldsymbol {B}=0$) and electric ($\boldsymbol {\nabla }\boldsymbol {\cdot }\boldsymbol {E}=0$) fields in the absence of electric charges. Fields (7.1), in the Gaussian units convention, satisfy also Faraday's law of induction

(7.2)\begin{equation} \boldsymbol{\nabla} \times \boldsymbol{E} + \frac{1}{\mathrm{c}}\,\frac{\partial\boldsymbol{B}}{\partial t} = \boldsymbol{0}, \end{equation}

for any $\boldsymbol {u}(\boldsymbol {x},t)$. We note that

(7.3a,b)\begin{equation}\frac{1}{\mathrm{c}}\,\frac{\partial\boldsymbol{E}}{\partial t} ={-}\frac{m^2\mathfrak{w}^2}{{\mathrm{c}}^2}\,\boldsymbol{\mathcal{U}}\quad \text{and} \quad \boldsymbol{\nabla}\times\boldsymbol{B} ={-} k^2 \boldsymbol{\mathcal{U}} . \end{equation}

If the density current $\boldsymbol {J}$ is defined as

(7.4)\begin{equation} \frac{4{\rm \pi}}{\mathrm{c}}\,\boldsymbol{J} \equiv \left(\frac{m^2\mathfrak{w}^2}{{\mathrm{c}}^2} - k^2 \right) \boldsymbol{\mathcal{U}}, \end{equation}

then Ampère's law,

(7.5)\begin{equation} \boldsymbol{\nabla}\times \boldsymbol{B} - \frac{1}{\mathrm{c}} \left( 4 {\rm \pi}\boldsymbol{J} + \frac{\partial \boldsymbol{E}}{\partial t} \right) = \boldsymbol{0}, \end{equation}

is also satisfied. Though the current density is $\boldsymbol {J} \neq \boldsymbol {0}$, there is no charge density since $\boldsymbol {\nabla } \boldsymbol {\cdot } \boldsymbol {J}=0$. The fulfilment of the Maxwell equations in the absence of charge density, using the definitions (7.1), does not suffice to obtain wave equations for $\boldsymbol {E}$ and $\boldsymbol {B}$. The additional constraint that the density current vanishes, $\boldsymbol {J}=\boldsymbol {0}$, must be assumed in (7.4), or equivalently set the wave speed

(7.6)\begin{equation} {\mathrm{c}} = c = \frac{m \mathfrak{w}}{k} , \end{equation}

then Ampère's law in the absence of charge density,

(7.7)\begin{equation} \boldsymbol{\nabla}\times \boldsymbol{B} - \frac{1}{c}\,\frac{\partial \boldsymbol{E}}{\partial t} = \boldsymbol{0}, \end{equation}

is also satisfied. In this case, both $\boldsymbol {E}$ and $\boldsymbol {B}$, as defined by (7.1), satisfy wave equations with phase velocity $c$,

(7.8a,b)\begin{equation} \frac{1}{c^2}\,\frac{\partial^2 \boldsymbol{E}}{\partial t^2} - \nabla^2\boldsymbol{E} =\boldsymbol{0} , \quad \frac{1}{c^2}\,\frac{\partial^2 \boldsymbol{B}}{\partial t^2} - \nabla^2\boldsymbol{B} =\boldsymbol{0} , \end{equation}

which are the Maxwell equations for electromagnetic waves in vacuum. The phase speed $c$ in (7.6) does not depend on the $w$ reference frame, but depends on the radial $k$ and azimuthal $m$ wavenumbers. This is so because the velocity solution $\boldsymbol {u}(r,\theta,\varphi,t)$ in (2.3), with free parameters $u_1, \mathfrak {w}, k , \ell , m$, is still too general to be applied directly to any particular physical process. In order to apply the hydrodynamical flow solution (2.3) as a model for the propagation of electromagnetic waves in ‘vacuum’, which is experimentally known to have a constant – and independent of the inertial reference frame – wave speed $c$, we establish an additional condition, namely, that frequency $\mathfrak {w}$ and wavenumbers $k,m$ are related through a dispersion relation

(7.9)\begin{equation} \mathfrak{w}^2=\tilde{\mathfrak{w}}^2(k,m) = c_0^2\,\frac{k^2}{m^2} , \end{equation}

where $c_0$ is a constant wave speed. Constraint (7.9) is independent of the $w$ reference frame. This condition immediately gives $\mathfrak {w} = \pm c_0 k/m$ and therefore $c=c_0$ in (7.6) is a constant independent of the $w$ reference frame. The constant

(7.10)\begin{equation} c_0 = \frac{m\mathfrak{w}}{k} \end{equation}

(positive relation assumed) is identified with the speed of the electromagnetic waves in ‘vacuum’. Once $c_0$ is given a universal value, say $c_0=1$, the remaining free parameters of the hydrodynamical model $\boldsymbol {u}(r,\theta,\varphi,t)$ from (2.3) are the amplitude velocity of the oscillating term $u_1$, the frequency $\mathfrak {w}$ (or the radial wavenumber $k = m\mathfrak {w}/c_0$), and the degree $\ell$ (or number of nodal lines). Interestingly, in the particular case of azimuthal wavenumber $m=2$, the wave speed in (7.10), $c_0=2\mathfrak {w}/k$, equals the axial velocity of displacement $w$ in (5.10) for the velocity solution with vanishing background axial flow (vanishing axial flow at infinity). For such a velocity solution, the wave speed and axial speed of displacement coincide. Another interesting property of these hydrodynamical models is that they admit piecewise solutions, as explained in § 10, making it possible to assign to these flows both continuous field and discrete particle-like properties.

8. Superposition

This section addresses the relevant question of whether the superposition of two members of the vortex family $\boldsymbol {u}(\boldsymbol {x},t)$ in (2.3) is a flow solution as well. First, we denote a particular member $\boldsymbol {u}_{i}(\boldsymbol {x},t)$ of this vortex family with the index $i$ as

(8.1)\begin{equation} \boldsymbol{u}_{i}(r,\theta,\varphi,t) \equiv \boldsymbol{u}(k_{i},\ell_{i},m_{i},u_{1,i},\mathfrak{w}_{i};r,\theta,\varphi,t), \end{equation}

and we want to know whether the superposition

(8.2)\begin{equation} \boldsymbol{u}_{1,2} \equiv \boldsymbol{u}_{1} + \boldsymbol{u}_{2} \end{equation}

satisfies the vorticity equation (1.1). We define in the usual way $\boldsymbol {u}_{i} \equiv \boldsymbol {\mathcal {U}}_i + \bar {\boldsymbol {u}}_{i}$, the vorticity $\boldsymbol {\omega }_{i} \equiv \boldsymbol {\nabla } \times \boldsymbol {u}_{i} = \boldsymbol {\mathcal {W}}_i + \bar {\boldsymbol {\omega }}_{i}$, and the Lamb vector $\boldsymbol {l}_{i} \equiv \boldsymbol {\omega }_{i} \times \boldsymbol {u}_{i}$. Since the particular solutions satisfy the relations

(8.3a–c)\begin{equation} \frac{\partial\boldsymbol{\omega}_{i}}{\partial t} + \boldsymbol{\nabla} \times \boldsymbol{l}_{i} = \boldsymbol{0} \,, \quad \boldsymbol{\mathcal{W}}_{i} \times \boldsymbol{\mathcal{U}}_{i} = \boldsymbol{0} \,, \quad \boldsymbol{\nabla} \times \left( \bar{\boldsymbol{\omega}}_{i} \times \bar{\boldsymbol{u}}_{i} \right) = \boldsymbol{0} , \end{equation}

All that remains from the vorticity equation for (8.2) is the curl of the crossing terms

(8.4)\begin{align} & \boldsymbol{\nabla} \times \left( \boldsymbol{\omega}_1 \times \boldsymbol{u}_2 +\boldsymbol{\omega}_2 \times \boldsymbol{u}_1 \right) \nonumber\\ &\quad = \boldsymbol{\nabla} \times \left[ \left( \boldsymbol{\mathcal{W}}_1 + \bar{\boldsymbol{\omega}}_1 \right) \times \left( \boldsymbol{\mathcal{U}}_2 + \bar{\boldsymbol{u}}_2 \right) + \left( \boldsymbol{\mathcal{W}}_2 + \bar{\boldsymbol{\omega}}_2 \right) \times \left( \boldsymbol{\mathcal{U}}_1 + \bar{\boldsymbol{u}}_1 \right) \right] \nonumber\\ &\quad = \boldsymbol{\nabla} \times \left[ \left( k_2 - k_1 \right) \left( \boldsymbol{\mathcal{U}}_1 \times \boldsymbol{\mathcal{U}}_2 \right) + \left( \bar{\boldsymbol{\omega}}_1 \times \bar{\boldsymbol{u}}_2 + \bar{\boldsymbol{\omega}}_2 \times \bar{\boldsymbol{u}}_1 \right) \right. \nonumber\\ &\left.\qquad {}- \boldsymbol{\mathcal{U}}_1 \times \left( k_1 \bar{\boldsymbol{u}}_2 + \bar{\boldsymbol{\omega}}_2 \right) - \boldsymbol{\mathcal{U}}_2 \times \left( k_2 \bar{\boldsymbol{u}}_1 + \bar{\boldsymbol{\omega}}_1 \right) \right] . \end{align}

Clearly, the curl of the terms

(8.5)\begin{equation} \bar{\boldsymbol{\omega}}_{1} \times \bar{\boldsymbol{u}}_2 ={-}2 \mathfrak{w}_1 \mathfrak{w}_2\rho \hat{\boldsymbol{\rho}} \end{equation}

vanishes, and also we can express

(8.6)\begin{equation} k_1 \bar{\boldsymbol{u}}_{2} + \bar{\boldsymbol{\omega}}_2 = k_1 \mathfrak{w}_2 \rho \hat{\boldsymbol{\varphi}} - 2 \mathfrak{w}_2 \left( \frac{k_1 - k_2}{k_2}\right) \hat{\boldsymbol{z}}. \end{equation}

Thus for identical radial wavenumbers $k_1 = k_2 = k$, the curl of the crossing terms (8.4) reduces to the simple expression

(8.7)\begin{align} \boldsymbol{\nabla} \times \left( \boldsymbol{\omega}_1 \times \boldsymbol{u}_2 +\boldsymbol{\omega}_2 \times \boldsymbol{u}_1 \right) &={-}k \boldsymbol{\nabla} \times \left[ \rho \left( \mathfrak{w}_2 \boldsymbol{\mathcal{U}}_1 + \mathfrak{w}_1 \boldsymbol{\mathcal{U}}_2 \right)\times \hat{\boldsymbol{\varphi}} \right] \nonumber\\ &={-} {\rm i} k \left( m_1 \mathfrak{w}_2 \boldsymbol{\mathcal{U}}_1 + m_2 \mathfrak{w}_1 \boldsymbol{\mathcal{U}}_2 \right) . \end{align}

Term (8.7) vanishes, and therefore $\boldsymbol {u}_1$ and $\boldsymbol {u}_2$ are superposable, in different cases. (i) The steady oscillating flows vanish ($u_{1,1} = u_{1,2} = 0$), leaving only the steady rigid flows ($\mathfrak {w}_1 \ne 0$ and/or $\mathfrak {w}_2 \ne 0$). (ii) The trivial case in which the steady oscillating flows cancel, $\boldsymbol {\mathcal {U}}_{1}=-\boldsymbol {\mathcal {U}}_{2}$ ($u_{1,1} = -u_{1,2}$, $m_1 = m_2$ and $\mathfrak {w}_1=\mathfrak {w}_2$). (iii) Both flows are steady because $m_1=m_2=0$ and there is rigid flow ($\mathfrak {w}_1 \ne 0$ and/or $\mathfrak {w}_2 \ne 0$). (iv) Both flows are steady because $\mathfrak {w}_1 = \mathfrak {w}_2 = 0$ and therefore there is no rigid flow (this case corresponds to the superposition of solutions $\boldsymbol {\mathcal {U}}(\boldsymbol {x},0)$). (v) One of the flows is steady with no rigid motion (say $\mathfrak {w}_1=0$ and $m_1 \ne 0$), and the other one is steady with rigid motion ($m_2=0$ and $\mathfrak {w}_2\ne 0$).

9. Stability of the steady vortices with $m=0$

The time-dependent vortex solution $\boldsymbol {u}(\boldsymbol {x},t)$ in (2.3) is very useful to investigate the stability of spherical vortices and in particular the stability of the steady Hicks–Moffatt vortex. The Hicks–Moffatt vortex is a three-dimensional piecewise vortex whose interior vortical velocity is given by $\boldsymbol {u}$ in (2.3) for the particular case of degree $\ell =1$ (one nodal line) and order $m=0$ (zonal spherical harmonics solution). Thus the stationarity of this vortex is due not to the absence of background rotation $\mathfrak {w}\rho$, but to the fact that since $m=0$, the velocity field does not depend on the azimuthal angle $\varphi$. If the vortex boundary $r_n$ is taken at any zero $j_{5/2,n}$ of ${\rm j}_2(\,{\cdot}\, )$ – that is, if $k r_n = j_{5/2,n}$, and the ratio $\mathfrak {w}/u_1 = \sqrt {3/{\rm \pi} }\,{\rm j}_0(k r_n)/6$ (employing the parameter $u_1$ in (2.3)) – then these spherical vortex boundary surfaces are stagnation surfaces, and the exterior irrotational flow vanishes. The stability of these zonal vortices is investigated next.

Let us consider the oscillating function $\bar {\boldsymbol {\mathcal {U}}}(r,\theta )$ defined from $\boldsymbol {\mathcal {U}}(\boldsymbol {x},t)$ in (2.1) by

(9.1)\begin{equation} \bar{\boldsymbol{\mathcal{U}}}_{\ell}(r,\theta) \equiv \boldsymbol{\mathcal{U}}(r,\theta,\varphi\mapsto0,t;u_1\mapsto 1, \mathfrak{w}\mapsto 0) , \end{equation}

where the degree $\ell$ is shown for clarity. In such a flow, having an amplitude term $u_1(t)$,

(9.2)\begin{equation} \boldsymbol{u}_1 (r,\theta,\varphi,t) = u_1(t)\,\bar{\boldsymbol{\mathcal{U}}}_{\ell}(r,\theta) \exp({{\rm i}m_1(\varphi-\mathfrak{w}_1 t)}) + \mathfrak{w}_1\rho \, \hat{\boldsymbol{\varphi}} - \frac{2\mathfrak{w}_1}{k} \, \hat{\boldsymbol{z}} , \end{equation}

is in the form (2.3), and therefore (9.2) is a velocity solution when $u_1(t)=\hat {u}_1$ is a constant. We notice that since the spherical harmonics basis vectors are not normalized, the weight $u_1(t)$ is not the total velocity amplitude of the oscillation. We then force $\boldsymbol {u}_{1}$ to be steady by setting $m_1=0$, but keep the background flow $\mathfrak {w}_1 \ne 0$. We then add to the steady velocity $\boldsymbol {u}_1$ a perturbation velocity with time-dependent amplitude $u_2(t)$, azimuthal wavenumber $m_2\ne 0$, and local frequency $m_2\mathfrak {w}_2\ne 0$:

(9.3)\begin{equation} u_2(t)\,\bar{\boldsymbol{\mathcal{U}}}_{\ell}(r,\theta) \exp({{\rm i}m_2(\varphi-\mathfrak{w}_2 t)}) . \end{equation}

Adding (9.3) to (9.2), we obtain the total velocity

(9.4)\begin{equation} \boldsymbol{u} = \left( u_1(t) \exp({-{\rm i}m_2(\varphi-\mathfrak{w}_2 t)}) + u_2(t) \right) \bar{\boldsymbol{\mathcal{U}}}_{\ell}(r,\theta) \exp({{\rm i}m_2(\varphi-\mathfrak{w}_2 t)}) + \mathfrak{w}_1\rho \, \hat{\boldsymbol{\varphi}} - \frac{2\mathfrak{w}_1}{k} \, \hat{\boldsymbol{z}} , \end{equation}

and we want to know when this velocity $\boldsymbol {u}(\boldsymbol {x},t)$ is a flow solution of the vorticity equation. It turns out that $\boldsymbol {u}(\boldsymbol {x},t)$ in (9.4) is already in the form (2.3), and therefore (9.4) is a velocity solution when $m_2\in \{ -\ell,\ldots,-1,1,\ldots,\ell \}$, the angular frequency $\mathfrak {w}_2$ of the oscillation equals the angular speed of the background flow $\mathfrak {w}_1$,

(9.5)\begin{equation} \mathfrak{w}_2 = \mathfrak{w}_1 \equiv \mathfrak{w} , \end{equation}

and the velocity amplitude is constant,

(9.6)\begin{equation} \frac{\partial}{\partial t} \left( u_1(t) \exp({-{\rm i} m_2(\varphi-\mathfrak{w} t)}) + u_2(t) \right) = 0. \end{equation}

Condition (9.6) is satisfied when

(9.7a,b)\begin{equation} u_1(t) = \hat{u}_1 \exp({-{\rm i}m_2\mathfrak{w}t}) \quad \text{and} \quad {u}_2(t) = \hat{u}_2, \end{equation}

where $\hat {u}_1$ and $\hat {u}_2$ are constant amplitudes, in such a way that $\boldsymbol {u}(\boldsymbol {x},t)$ in (9.4) may be written as

(9.8)\begin{equation} \boldsymbol{u} = \left( \hat{u}_1 + \hat{u}_2\,{\rm e}^{{\rm i}m_2\varphi} \right) \exp({-{\rm i} m_2 \mathfrak{w} t})\,\bar{\boldsymbol{\mathcal{U}}}_{\ell}(r,\theta) + \mathfrak{w}\rho \, \hat{\boldsymbol{\varphi}} - \frac{2\mathfrak{w}}{k} \, \hat{\boldsymbol{z}} , \end{equation}

which means that the addition of any perturbation with constant amplitude $\hat {u}_2$, no matter how small and with any permissible azimuthal wavenumber $m_2\neq 0$, to the steady velocity $\boldsymbol {u}_1$ that has a background flow characterized by the angular speed $\mathfrak {w}$, will cause inertial oscillations of amplitude $\|\hat {u}_1\bar {\boldsymbol {\mathcal {U}}}_{\ell }\|$ and local frequency $m_2\mathfrak {w}$.

10. Piecewise solutions

The spatial domain of the rotational flows described in the previous sections is an unbounded region. It is often convenient, however, to work with spatially bounded velocity solutions by assuming that the rotational flow is confined within a spherical region – usually a sphere, but a spherical shell is also possible – while outside this vortical region the flow is potential. The natural choice for selecting the radius of any spherical boundary surface to the velocity $\boldsymbol {\mathcal {U}}$ in (2.1) is at the zeros of ${\rm j}_{\ell }(\,{\cdot}\, )$, i.e. $k r_p = \jmath _{\ell,p} \equiv j_{\ell +1/2,p}$, because at these radial distances the velocity oscillation has only $\boldsymbol {\varPsi }$-component,

(10.1)\begin{equation} \boldsymbol{\mathcal{U}}(\jmath_{\ell,p}/k,\theta,\varphi,t) ={-} u_1\,{\rm j}_{\ell+1}(\jmath_{\ell,p})\,\boldsymbol{\varPsi}_{\ell}^{m}(\theta,\varphi) \exp({-{\rm i} m \mathfrak{w}t}) , \end{equation}

and vanishing exterior flow conditions are consistent because there is no velocity jump in the radial direction, so there are no shock waves, which would not be permissible for isochoric flows. The vortex boundary, regarding the discontinuity in the azimuthal component of the background flow $\rho \mathfrak {w}\hat {\boldsymbol {\varphi }}$, is a vortex sheet (first-order singular surface where the velocity jump is only tangential). The axial component of the background flow $w=-2\mathfrak {w}/k$ is not problematic since it vanishes in the steadily translating solutions $\check {\boldsymbol {u}}(\boldsymbol {x},t)$ of (5.11).

Nevertheless, it is possible to provide the exterior irrotational velocity $\tilde {\boldsymbol {\mathcal {U}}}_p(r,\theta,\varphi,t)$ for the oscillating component, which is given by

(10.2)$$\begin{gather} \tilde{\boldsymbol{\mathcal{U}}}_p(r,\theta,\varphi,t) = u_1\,\frac{ {\rm j}_{\ell+1}(\jmath_{\ell,p})}{2\ell+1} \left[ \ell(\ell+1) \left( \left( \frac{kr}{\jmath_{\ell,p}} \right)^{ \ell -1} -\left( \frac{kr}{\jmath_{\ell,p}} \right)^{-\ell -2} \right) \boldsymbol{Y}_{\ell}^{m}(\theta,\varphi) \right. \nonumber\\ \left.{}+\left( (\ell+1) \left( \frac{kr}{\jmath_{\ell,p}} \right)^{ \ell -1} + \ell \left( \frac{kr}{\jmath_{\ell,p}} \right)^{-\ell -2} \right) \boldsymbol{\varPsi}_{\ell}^{m}(\theta,\varphi) \right] {\rm e}^{-{\rm i} m \mathfrak{w}t} . \end{gather}$$

Solution $\tilde {\boldsymbol {\mathcal {U}}}_p(r,\theta,\varphi,t)$ is irrotational ($\boldsymbol {\nabla }\times \tilde {\boldsymbol {\mathcal {U}}}_p=\boldsymbol {0}$) and satisfies continuity at the spherical boundaries, i.e. $\tilde {\boldsymbol {\mathcal {U}}}(\jmath _{\ell,p}/k,\theta,\varphi,t) =\boldsymbol {\mathcal {U}}(\jmath _{\ell,p}/k,\theta,\varphi,t)$.

In this case, and regarding only the oscillating velocity, the vortex boundary is a second-order singular surface (the velocity field is continuous), and when it propagates, it is an acceleration wave.

When a momentum diffusivity $\nu \neq 0$ is considered in the Navier–Stokes equation (3.2), the oscillating motion in the interior and exterior domains decays according to (3.3a) but the effect in the vortex boundary may be problematic since the vortex boundary radius may change due to the lateral diffusivity (e.g. Kloosterziel Reference Kloosterziel1990).

As an example, the velocity field and streamlines of a piecewise vortex are shown in figures 1 and 2. This example is the vortex $\boldsymbol {u}(\boldsymbol {x},t)$ with parameters $\ell =2$, $m=-2$, $\mathfrak {w}=0$, $k=1$ and vorticity boundary at $k r_b = \jmath _{2,1}$. The streamlines set shown in these figures bifurcates twice. The first bifurcation occurs on $z>0$ on two descending streamline branches, the left and right branches (mostly in blue and red colours, respectively), which descend and cross the plane $z=0$ close to the regions of minimum axial speed (blue arrows in the north-west and south-east poles). The right branch (mostly in red) bifurcates again on $z<0$ on two ascending branches (see figure 2); the first branch (red) comes back to the initial location at $z=0$ (south-west pole), while the second branch (red-blue) crosses the plane at the location of maximum axial speed in the north-east pole. Obviously, as it happens with similar piecewise multipolar vortices in two-dimensional flows for azimuthal wavenumbers larger than $1$, this flow structure is not steady and breaks into four spherical dipoles, moving apart.

Figure 1. Top view of the piecewise velocity field $\boldsymbol {u}(\boldsymbol {x},t_0)$ (arrows) at $z=0$ and $t_0=0$ for parameters $\ell =2$, $m=-2$, $\mathfrak {w}=0$, $k=1$ and vorticity boundary at $k r_b = \jmath _{2,1}$. Colour in the arrows corresponds to the axial $z$-component of the velocity $\boldsymbol {u}\boldsymbol {\cdot }\hat {\boldsymbol {z}}$ (blue and red colours mean negative and positive $z$-components, respectively). The coloured ribbon is a set of streamlines initiated on the plane $z=0$ on the region of maximum positive axial velocity (red arrows) in the south-west pole (the initial location of the streamline ribbon is shown more clearly in a side view in figure 2).

Figure 2. Side (from the south) view of the streamlines ribbon shown in figure 1. The initial location of the streamlines ribbon is seen on the left-hand side.

11. Concluding remarks

In this paper, we have provided a new family of exact solutions of multipolar vortical flows $\boldsymbol {u}(\boldsymbol {x},t)$ satisfying the time-dependent vorticity equation. These solutions may be interpreted as time and space oscillations, with spherical geometry, embedded in a cylindrical constant flow with swirl, and are characterized as inertial oscillations in background flow. These time-dependent azimuthal oscillating velocity solutions are a generalization of the steady three-dimensional multipolar vortex solutions given in Viúdez (Reference Viúdez2022), which are recovered in the case of vanishing time dependence ($m\mathfrak{w}=0$). The necessary and sufficient condition for the existence of the inertial waves is a double condition: the flows experience inertial waves as long as they have a non-vanishing azimuthal wavenumber $(m \ne 0)$ in the presence of a background rotation (angular speed $\mathfrak {w}\ne 0$). In the case of vanishing azimuthal wavenumber $m=0$, the background rotation causes no effect in the local flow, which becomes a steady solution $\boldsymbol {\mathcal {U}}(\boldsymbol {x})$ even in the presence of background rotational flow. In this case, however, small perturbations to the local flow would cause inertial oscillations. The vortex solutions also satisfy a superposable property, which is relevant to investigate the stability of simple, not composed, vortices. Furthermore, the more general time-dependent flow solution $\boldsymbol {u}(\boldsymbol {x},t)\,{\rm exp}(-\nu k^2 t)$ is a solution of the Navier–Stokes equation with constant diffusivity $\nu$. Since the curl of the Lamb vector of the total flow $\boldsymbol {\nabla } \times (\boldsymbol {\omega }\times \boldsymbol {u})$ is proportional to the oscillating term $\boldsymbol {\mathcal {U}}(\boldsymbol {x},t)$, these nonlinear solutions also satisfy several well-known linear wave equations. An important problem to address now concerns the stability of these time-dependent solutions. Though piecewise vortices of individual modes seem to be unstable, it might be possible to find stable solutions in terms of a superposition of time-dependent modes, as has been done already with neutral vortices (vortices with vanishing amount of vertical vorticity) in two-dimensional Euler flows. This research is left for future work.