Hostname: page-component-6766d58669-kn6lq Total loading time: 0 Render date: 2026-05-18T21:04:54.843Z Has data issue: false hasContentIssue false

The electromagnetic radiation whose decay violates the inverse-square law: detailed mathematical treatment of an experimentally realized example

Published online by Cambridge University Press:  13 June 2019

Houshang Ardavan*
Affiliation:
Institute of Astronomy, University of Cambridge, Madingley Road, Cambridge CB3 0HA, UK
*
Email address for correspondence: ardavan@ast.cam.ac.uk
Rights & Permissions [Opens in a new window]

Abstract

I analyse and numerically evaluate the radiation field generated by an experimentally realized embodiment of an electric polarization current whose rotating distribution pattern moves with linear speeds exceeding the speed of light in vacuum. I find that the flux density of the resulting emission (i) has a dominant value and is linearly polarized within a sharply delineated radiation beam whose orientation and polar width are determined by the range of values of the linear speeds of the rotating source distribution, and (ii) decays with the distance $d$ from the source as $d^{-\unicode[STIX]{x1D6FC}}$ in which the value of $\unicode[STIX]{x1D6FC}$ lies between $1$ and $2$ (instead of being equal to $2$ as in a conventional radiation) across the beam. In that the rate at which boundaries of the retarded distribution of such a source change with time depends on its duration monotonically, this is an intrinsically transient emission process: temporal rate of change of the energy density of the radiation generated by it has a time-averaged value that is negative (instead of being zero as in a conventional radiation) at points where the envelopes of the wave fronts emanating from the constituent volume elements of the source distribution are cusped. The difference in the fluxes of power across any two spheres centred on the source is in this case balanced by the change with time of the energy contained inside the shell bounded by those spheres. These results are relevant not only to long-range transmitters in communications technology but also to astrophysical objects containing rapidly rotating neutron stars (such as pulsars) and to the interpretation of the energetics of the multi-wavelength emissions from sources that lie at cosmological distances (such as radio and gamma-ray bursts). The analysis presented in this paper is self-contained and supersedes my earlier works on this problem.

Information

Type
Research Article
Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted re-use, distribution, and reproduction in any medium, provided the original work is properly cited.
Copyright
© The Author 2019
Figure 0

Figure 1. Schematic representation of the distribution pattern of the electric polarization described by (2.1) at a given $(r,z)$. The circles designate the edges of the dielectric ring hosting the polarization and the sinusoidal curve designates the rigidly rotating wave train whose linear speed $r\unicode[STIX]{x1D714}$ (along the shown arrows) exceeds the speed of light in vacuum.

Figure 1

Figure 2. Schematic view of the experimental apparatus (a) from above and (b) from the side, showing the boundaries of the dielectric medium (in orange) and the electrode pairs (in blue).

Figure 2

Figure 3. The oscillating voltage $V$ on each electrode pair versus the $\unicode[STIX]{x1D711}$ coordinate ($\unicode[STIX]{x1D711}_{n}=2\unicode[STIX]{x03C0}n/N$ with $n=1,\ldots ,21$) of the centre of that electrode at four equally spaced consecutive times ($t_{1}). The electrodes oscillate with the same frequency but differing phases. It can be seen that the phase difference between the oscillations of the adjacent electrode pairs sets this discretized wave train in motion. The fundamental Fourier component of the resulting discretized polarization, here depicted by a solid sinusoidal curve, thus moves in the azimuthal direction with a speed that can exceed the speed of light in vacuum, even though the charges whose separation creates the polarization move in a different direction with a different speed.

Figure 3

Figure 4. Generic forms of the function $g(\unicode[STIX]{x1D711})$ for source points whose $(\hat{r},\hat{z})$ coordinates lie across the boundary $\unicode[STIX]{x1D6E5}=0$ delineating the projection of the cusp curve of the bifurcation surface onto the $(\hat{r},\hat{z})$ plane (see figure 11). Depending on whether $\unicode[STIX]{x1D719}$ lies outside or inside the interval $(\unicode[STIX]{x1D719}_{-},\unicode[STIX]{x1D719}_{+})$, contributions are made toward the observed field (i.e. the argument $g(\unicode[STIX]{x1D711})-\unicode[STIX]{x1D719}$ of the Dirac delta function in (4.5) vanishes) at either one or three retarded positions of the source. For a horizontal line $g=\unicode[STIX]{x1D719}$ that either approaches an extremum of $g(\unicode[STIX]{x1D711})$ from inside the interval $(\unicode[STIX]{x1D719}_{-},\unicode[STIX]{x1D719}_{+})$ or passes through an inflection point of $g(\unicode[STIX]{x1D711})$, two or all three of the retarded positions in question coalesce and so their contributions interfere constructively to form caustics. This figure is for $\hat{r}=3$ and only shows two rotation periods. At higher speeds, the difference between the values of $\unicode[STIX]{x1D719}_{+}$ and $\unicode[STIX]{x1D719}_{-}$ can be large enough for a horizontal line $g=\unicode[STIX]{x1D719}$ to intersect $g(\unicode[STIX]{x1D711})$ over more than one rotation period (see figure 36). Contributions toward the observed field can thus arise, not only from one or three, but from any odd number of retarded positions of the source. There are contributions from more than three retarded times whenever the rotation period of the source is shorter than the time taken by the collapsing sphere $|\boldsymbol{x}-\boldsymbol{x}_{P}|=c(t-t_{P})$, centred on the observation point $P$, to cross the orbit of the source.

Figure 4

Figure 5. Cross-sections with the plane $\hat{z}_{P}=\hat{z}$ of the spherical wave fronts emanating from a rotating source point. This source has an angular frequency of rotation, $\unicode[STIX]{x1D714}$, that is constant and a speed, $r\unicode[STIX]{x1D714}$, that exceeds the speed of light $c$ in vacuum. The larger circle depicts the orbit of the source and the smaller circle the light cylinder $r=c/\unicode[STIX]{x1D714}$. The heavier (red) curves show the intersection of the envelope of these wave fronts (see figure 6) with the plane of rotation.

Figure 5

Figure 6. Three-dimensional view (in the space $(\hat{r}_{P},\hat{\unicode[STIX]{x1D711}}_{P},\hat{z}_{P})$ of observation points) of the envelope of wave fronts emanating from the rotating source point $(\hat{r},\hat{\unicode[STIX]{x1D711}},\hat{z})$. This envelope consists of two sheets that tangentially meet along a cusp (see figure 7). The singular sheet, i.e. the sheet that issues from the source point with an initial conical shape, is that described by $\hat{\unicode[STIX]{x1D711}}_{P}=\hat{\unicode[STIX]{x1D711}}-\unicode[STIX]{x1D719}_{-}(\hat{r}_{P},\hat{z}_{P};\hat{r},\hat{z})$.

Figure 6

Figure 7. The cusp along which the two sheets of the envelope of wave fronts meet and are tangent to one another. This cusp touches and is tangent to the light cylinder $\hat{r}_{P}=1$ on the plane $\hat{z}_{P}=\hat{z}$ and spirals outward into the far field on the hyperbolic surface of revolution $\unicode[STIX]{x1D6E5}(\hat{r}_{P},\hat{z}_{P};\hat{r},\hat{z})=0$ (see figure 12).

Figure 7

Figure 8. The two sheets $\unicode[STIX]{x1D719}=\unicode[STIX]{x1D719}_{\pm }$ of the bifurcation surface issuing from the observation point $P$, the cusp $C$ of this surface and the light cylinder $\hat{r}=1$. In contrast to the envelope of wave fronts which resides in the space of observation points, the surface shown here resides in the space $(r,\hat{\unicode[STIX]{x1D711}},z)$ of source points: it is the locus of source points that approach $P$, along the radiation direction, with the speed of light at the retarded time. The two sheets of this surface meet along a cusp that tangentially touches the light cylinder at $\hat{z}=\hat{z}_{P}$ and moves outward spiralling around the rotation axis on the hyperbolic surface of revolution $\unicode[STIX]{x1D6E5}(\hat{r},\hat{z};\hat{r}_{P},\hat{z}_{P})=0$ (see figure 11). The source points on this cusp approach the observer along the radiation direction not only with the speed of light but also with zero acceleration at the retarded time. The source would normally be distributed over a finite volume close to the light cylinder. If the position of the observation point is such that the cusp shown here intersects the source distribution, there will be wave fronts with differing emission times that are received simultaneously: while the source points outside the bifurcation surface make their contributions toward the value of the observed field at a single instant of retarded time, the source points inside this surface make their contributions at $3$ (or $5,7,\ldots$) distinct instants of retarded time.

Figure 8

Figure 9. Dependence of the Green’s function $G_{nj}$ on $\unicode[STIX]{x1D712}$ in cases where $q_{nj}$ is positive and appreciably greater than $|p_{nj}/c_{1}|$. The two sheets $\unicode[STIX]{x1D719}_{+}$ and $\unicode[STIX]{x1D719}_{-}$ of the bifurcation surface map onto the distinct values $\unicode[STIX]{x1D712}=1$ and $\unicode[STIX]{x1D712}=-1$ of $\unicode[STIX]{x1D712}$, respectively, even at the cusp locus of the bifurcation surface where the separation $\unicode[STIX]{x1D719}_{+}-\unicode[STIX]{x1D719}_{-}$ of these two sheets vanishes. The Green’s function thus diverges only for source points inside the bifurcation surface whose retarded positions coalesce when they approach this surface or its cusp from $|\unicode[STIX]{x1D712}|<1$.

Figure 9

Figure 10. Dependence of the Green’s function $G_{nj}$ on $\unicode[STIX]{x1D712}$ in cases where $p_{nj}$ is positive and appreciably greater than $|c_{1}q_{nj}|$ (see also figure 9).

Figure 10

Figure 11. The dash-dotted curve is the projection of the cusp locus of the bifurcation surface, $C$, onto the $(\hat{r},\hat{z})$ plane, i.e. the projection of the locus of source points that approach the observer along the radiation direction with the speed of light and zero acceleration at the retarded time (see (4.24)). The solid curve (in red) is the locus $S$ of the stationary points of the function $\unicode[STIX]{x1D719}_{-}$, i.e. the stationary points of the phase of the exponential factor that appears in the integrand of the expression for the field $[\boldsymbol{E}_{-}^{\text{b}}~~\boldsymbol{B}_{-}^{\text{b}}]$ (see (5.8) and (7.2)). The dotted rectangle represents the boundary of the support ${\mathcal{S}}^{\prime }$ of the source term $\boldsymbol{s}$ defined in (2.7), i.e. the boundary of the projection of the source distribution described in § 2 onto the $(\hat{r},\hat{z})$ plane. The part of the source distribution whose projection lies to the left of curve $C$, for which $\unicode[STIX]{x1D6E5}<0$, only generates a spherically decaying conventional field. Whether the cusp locus $C$ intersects the source distribution (as shown here) or lies to the left or right of the domain ${\mathcal{S}}^{\prime }$ is dictated by the polar coordinate $\unicode[STIX]{x1D703}_{P}$ of the observation point $P$ (see (5.12)). In plotting this figure, I have placed the observation point close to the source (at $\hat{r}_{P}=\hat{z}_{P}=3$) in order to render the separation between $C$ and $S$ visible. As $\hat{R}_{P}$ increases, these two curves overlap and tend toward the vertical. For $\hat{R}_{P}\gg 1$, the radial distance between $C$ and $S$ at an arbitrary $\hat{z}$ diminishes as $\hat{R}_{P}^{-2}$ (see (7.3)).

Figure 11

Figure 12. Counterpart of figure 11 in the $(\hat{r}_{P},\unicode[STIX]{x1D711}_{P},\hat{z}_{P})$-space of observation points. While the cusp locus $C$ in figure 11 is described by $\unicode[STIX]{x1D6E5}=0$ for fixed values of $(\hat{r}_{P},\hat{z}_{P})$, the hyperbolas shown here are described by $\unicode[STIX]{x1D6E5}=0$ for fixed values of the source coordinates $(\hat{r},\hat{z})$: the values $(\hat{r}_{U},\hat{z}_{0})$ and $(\hat{r}_{L},-\hat{z}_{0})$. If the observation point $P$ lies in the space (coloured orange) between the hyperbolas, then the cusp locus $C$ of the bifurcation surface intersects the source distribution shown in figure 11. But if the observation point $P$ lies in the space (coloured yellow) that is bounded by the inner hyperbola, then $\unicode[STIX]{x1D6E5}$ is positive throughout the source distribution and the cusp locus $C$ lies to the left of the source distribution shown in figure 11. On the other hand, at observation points in $0\leqslant \unicode[STIX]{x1D703}_{P}\leqslant \unicode[STIX]{x1D703}_{L}^{\text{c}}$ and $\unicode[STIX]{x03C0}-\unicode[STIX]{x1D703}_{L}^{\text{c}}\leqslant \unicode[STIX]{x1D703}_{P}\leqslant \unicode[STIX]{x03C0}$ (outside the coloured regions), $\unicode[STIX]{x1D6E5}$ is negative throughout the source distribution and the cusp locus $C$ lies to the right of the source distribution shown in figure 11. In cases where the lower boundary of the source distribution shown in figure 11 falls on or within the light cylinder, i.e. $\hat{r}_{L}\leqslant 1$ but $\hat{r}_{U}>1$, the two arms of the inner hyperbola shown here coalesce onto the $\hat{r}_{P}$-axis and the cusp locus of the bifurcation surface intersects the source distribution for all points of the (expanded orange) space inside the outer hyperbola.

Figure 12

Figure 13. The solutions $v=v_{S}(u)$ of (7.36) for $\hat{z}=0$, $\hat{R}_{P}=100$ and $\unicode[STIX]{x1D703}_{P}=\unicode[STIX]{x03C0}/3$ in the vicinity of the saddle point $(\hat{r}_{S},0)$ of the function $\text{Re}[\unicode[STIX]{x1D719}_{-}(u,v)]$. As shown by figures 14 and 15, the segments here designated by ${\mathcal{L}}_{S}$ satisfy the condition in (7.37) and so constitute the paths of steepest descent through the saddle point $(\hat{r}_{S},0)$.

Figure 13

Figure 14. The function $\unicode[STIX]{x1D6FE}_{S}(u)$, here plotted for $\hat{z}=0$, $\hat{R}_{P}=100$ and $\unicode[STIX]{x1D703}_{P}=\unicode[STIX]{x03C0}/3$, shows that of the two segments of the solution to (7.36) for which $v_{S}(u)\geqslant 0$ (the upper segments in figure 13), only the segment $u\geqslant \hat{r}_{S}$ (on the right) satisfies the requirement in (7.37).

Figure 14

Figure 15. The function $\unicode[STIX]{x1D6FE}_{S}(u)$, here plotted for $\hat{z}=0$, $\hat{R}_{P}=100$ and $\unicode[STIX]{x1D703}_{P}=\unicode[STIX]{x03C0}/3$, shows that of the two segments of the solution to (7.36) for which $v_{S}(u)\leqslant 0$ (the lower segments in figure 13), only the segment $u\leqslant \hat{r}_{S}$ (on the left) satisfies the requirement in (7.37).

Figure 15

Figure 16. The complex $\hat{r}=u+\text{i}v$ plane with a shift in the position of the imaginary axis which places the saddle point $(\hat{r}_{S},0)$ of $\unicode[STIX]{x1D719}_{-}(u,v,\hat{z},\hat{R}_{P},\unicode[STIX]{x1D703}_{P})$ at the origin. The curves ${\mathcal{L}}_{S}$, ${\mathcal{L}}_{C}$ and ${\mathcal{L}}_{U}$ delineate the paths of steepest descent of $\exp (-\text{i}m\unicode[STIX]{x1D719}_{-})$ through the following critical points, respectively: the saddle point $(\hat{r}_{S},0)$, the cusp point $(\hat{r}_{C},0)$ and the boundary point $(\hat{r}_{U},0)$. Here, the cusp point lies between the lower and upper boundaries $(\hat{r}_{L},0)$ and $(\hat{r}_{U},0)$ of the source distribution (see figure 11). The segment $\hat{r}_{C}+\unicode[STIX]{x1D716}\leqslant u\leqslant \hat{r}_{U}$ of the real axis, together with ${\mathcal{L}}_{S}$, ${\mathcal{L}}_{C}$, ${\mathcal{L}}_{U}$ and the indentation ${\mathcal{L}}_{\unicode[STIX]{x1D716}}$, surrounding the singularity of $G_{j}^{\text{out}}|_{\unicode[STIX]{x1D719}=\unicode[STIX]{x1D719}_{-}}$ at the cusp point, constitute the contours of integration for the evaluation of the part $[\boldsymbol{E}_{-}^{\text{b}}\quad \boldsymbol{B}_{-}^{\text{b}}]$ of the field given by (7.59). The arrows show the adopted directions of integration along the various contours. This figure is plotted for the following set of values of the parameters: $\hat{R}_{P}=10^{2}$, $\unicode[STIX]{x1D703}_{P}=\unicode[STIX]{x03C0}/3$, $\hat{z}=0$, $m=10$ and $\hat{r}_{U}=1.15474$.

Figure 16

Figure 17. The complex $\hat{r}=u+\text{i}v$ plane with a shift in the position of the imaginary axis which places the saddle point $(\hat{r}_{S},0)$ of $\unicode[STIX]{x1D719}_{-}(u,v,\hat{z},\hat{R}_{P},\unicode[STIX]{x1D703}_{P})$ at the origin. The curves ${\mathcal{K}}_{C}$ and ${\mathcal{K}}_{U}$ delineate the paths of steepest descent of $\exp (-\text{i}m\unicode[STIX]{x1D719}_{+})$ through the cusp point $(\hat{r}_{C},0)$ and the boundary point $(\hat{r}_{U},0)$, respectively. Here, the cusp point lies between the lower and upper boundaries $(\hat{r}_{L},0)$ and $(\hat{r}_{U},0)$ of the source distribution (see figure 11). The segment $\hat{r}_{C}+\unicode[STIX]{x1D716}\leqslant u\leqslant \hat{r}_{U}$ of the real axis, together with ${\mathcal{K}}_{S}$, ${\mathcal{K}}_{U}$ and the indentation ${\mathcal{K}}_{\unicode[STIX]{x1D716}}$, surrounding the singularity of $G_{j}^{\text{out}}|_{\unicode[STIX]{x1D719}=\unicode[STIX]{x1D719}_{+}}$ at the cusp point, constitute the contours of integration for the evaluation of the part $[\boldsymbol{E}_{+}^{\text{b}}\quad \boldsymbol{B}_{+}^{\text{b}}]$ of the field given by (7.61). The arrows show the adopted directions of integration along the various contours. This figure is plotted for the same set of values of the parameters as those for figure 16.

Figure 17

Figure 18. Paths of steepest descent of the exponential kernel $\exp (-\text{i}m\unicode[STIX]{x1D719}_{-})$ for an observation point in the transitional interval $\unicode[STIX]{x1D703}_{L}^{\text{c}}<\unicode[STIX]{x1D703}_{P}<\unicode[STIX]{x1D703}_{L}^{\text{s}}$ and a source element within $\hat{z}_{U}^{\text{c}}\leqslant \hat{z}\leqslant \hat{z}_{0}$. This figure is plotted for the following set of values of the parameters: $\hat{R}_{P}=10$, $\unicode[STIX]{x1D703}_{P}=181\unicode[STIX]{x03C0}/540$, $m=10$, $\hat{z}=-0.025$, $\hat{r}_{U}=1.1547$. Radial coordinate $\hat{r}_{S}=1.1548$ of the stationary point of the phase $\unicode[STIX]{x1D719}_{-}$ here exceeds the outer radius $\hat{r}_{U}$ of the source distribution.

Figure 18

Figure 19. Paths of steepest descent of the exponential kernel $\exp (-\text{i}m\unicode[STIX]{x1D719}_{-})$ for an observation point in the transitional interval $\unicode[STIX]{x1D703}_{U}\leqslant \unicode[STIX]{x1D703}_{P}\leqslant \unicode[STIX]{x1D703}_{P}^{\text{s}}|_{\hat{r}=\hat{r}_{L},\hat{z}=\hat{z}_{0}}$ and a source element within $\hat{z}_{L}^{\text{c}}\leqslant \hat{z}\leqslant \hat{z}_{0}$. This figure is plotted for the following set of values of the parameters: $\hat{R}_{P}=10$, $\unicode[STIX]{x1D703}_{P}=52\unicode[STIX]{x03C0}/135$, $m=10$, $\hat{z}_{0}=0.1$, $\hat{z}=0.08$, $\hat{r}_{L}=1.06657$ and $\hat{r}_{U}=1.06667$. Radial coordinate of the lower boundary of the source distribution here exceeds the location $\hat{r}_{C}=1.06652$ of the cusp but the stationary point $\hat{r}_{S}=1.06662$ of the phase $\unicode[STIX]{x1D719}_{-}$ falls within the source distribution.

Figure 19

Figure 20. Paths of steepest descent of the exponential kernel $\exp (-\text{i}m\unicode[STIX]{x1D719}_{+})$ for an observation point in the transitional interval $\unicode[STIX]{x1D703}_{U}\leqslant \unicode[STIX]{x1D703}_{P}\leqslant \unicode[STIX]{x1D703}_{P}^{\text{s}}|_{\hat{r}=\hat{r}_{L},\hat{z}=\hat{z}_{0}}$ and a source element within $\hat{z}_{L}^{\text{c}}\leqslant \hat{z}\leqslant \hat{z}_{0}$. The parameters for this figure have the same values as those for figure 19.

Figure 20

Figure 21. Logarithmic plot of the radial component of normalized Poynting vector $\hat{\boldsymbol{S}}$ versus the angle $\unicode[STIX]{x1D703}_{P}$ between the rotation axis and the radiation direction depicting directive gain of the radiation source at a distance of 10 light-cylinder radii. Since this distribution is symmetric with respect to the equatorial plane $\unicode[STIX]{x1D703}_{P}=90^{\circ }$, its remaining half in $90^{\circ }<\unicode[STIX]{x1D703}_{P}<180^{\circ }$ is not shown here. Values of the parameters used for plotting this figure are those for Case Ia described in § 11.1. (Only a discrete set of values of $\hat{\boldsymbol{n}}_{\infty }\boldsymbol{\cdot }\hat{\boldsymbol{S}}$ are plotted, instead of a continuous curve, to render the required computing time for the points in $60^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 70^{\circ }$ manageable.)

Figure 21

Figure 22. Vertically shifted distributions of the radial component of the normalized Poynting vector $\hat{\boldsymbol{S}}$ in $60^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 70^{\circ }$ for the following set of values of $\hat{R}_{P}$: (a$10$, (b$10^{2}$, (c$10^{3}$, (d$10^{4}$, (e$10^{5}$ and (f$10^{6}$. In this figure, the values of the normalizing factors in $\hat{\boldsymbol{S}}$ for $\hat{R}_{P}>10$ have been shifted, relative to that for $\hat{R}_{P}=10$, by the following amounts: (b$20$ dBi, (c$40$ dBi, (d$60$ dBi, (e$80$ dBi and (f$100$ dBi. Note that these shifted curves would have been coincident had the Poynting vector been decaying as $\hat{R}_{P}^{-2}$. The parts of these distributions in $0\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 60^{\circ }$ and $70^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 90^{\circ }$ (which are not plotted here) are coincident with one another and with those for $\hat{R}_{P}=10$ that are shown in figure 21. (Values of the parameters used for plotting this figure are those for Case Ia described in § 11.1.)

Figure 22

Figure 23. Angular distribution of the radiation in $0\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 90^{\circ }$ at distances $\hat{R}_{P}=10$ (curve $a$ of figure 22), $\hat{R}_{P}=10^{3}$ (curve $c$ of figure 22) and $\hat{R}_{P}=10^{6}$ (curve $f$ of figure 22). The angle between the radius vector to each point and the vertical axis stands for the polar coordinate $\unicode[STIX]{x1D703}_{P}$ of the observation point. The radial coordinate of each point on the curves $a$, $c$ and $f$ stands for the value of $10\log _{10}(\hat{\boldsymbol{S}})$ that appears in figure 22 against its coordinate $\unicode[STIX]{x1D703}_{P}$ plus $3$ dBi. The emission in $70^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 90^{\circ }$ and the conventional radiation in $0\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 60^{\circ }$ (which is too weak to show up in this plot) have distance-independent distributions. Three-dimensional distributions of the radiation patterns at the distances $\hat{R}_{P}=10,10^{3}$ and $10^{6}$ are given by the surfaces of revolution that result from the reflection of curves $a$, $c$ and $f$ with respect to the horizontal axis followed by their rotation about the vertical axis. (Values of the parameters used for plotting this figure are those for Case Ia described in § 11.1.)

Figure 23

Figure 24. Logarithmic plot of the radial component of normalized Poynting vector versus distance along the generating line of a cone (in this case the cone $\unicode[STIX]{x1D703}_{P}=62^{\circ }$) inside the solid angle $60^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 70^{\circ }$, $0\leqslant \unicode[STIX]{x1D711}_{P}\leqslant 360^{\circ }$, where the radiation depicted in figures 21–23 decays non-spherically. The best fit to the computed points (extracted from figure 22) has the slowly varying slope $-1.45$ (instead of $-2$) in this direction. (Values of the parameters used for plotting this figure are those for Case Ia described in § 11.1.)

Figure 24

Figure 25. Exponent $\unicode[STIX]{x1D6FC}$ in the distance dependence $\hat{R}_{P}^{-\unicode[STIX]{x1D6FC}}$ of the radial component of normalized Poynting vector as a function of the polar angle $\unicode[STIX]{x1D703}_{P}$ within the solid angle $60^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 70^{\circ }$, $0\leqslant \unicode[STIX]{x1D711}_{P}\leqslant 360^{\circ }$. (Values of the parameters used for plotting this figure are those for Case Ia described in § 11.1.)

Figure 25

Figure 26. The outward-propagating component of the normalized Poynting vector $\hat{\boldsymbol{S}}$ versus the polar coordinate $\unicode[STIX]{x1D703}_{P}$ of the observation point at the distance $\hat{R}_{P}=10$ for both a superluminally rotating source (curve $a$) and a corresponding stationary source (curve $s$). Since these distributions are symmetric with respect to the equatorial plane $\unicode[STIX]{x1D703}_{P}=90^{\circ }$, their remaining halves in $90^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 180^{\circ }$ are not shown here. (Values of the parameters used for plotting this figure are those for Case Ib described in § 11.2.)

Figure 26

Figure 27. Vertically shifted distributions of the radiation in $\unicode[STIX]{x1D703}_{L}\leqslant \unicode[STIX]{x1D703}_{P}\leqslant \unicode[STIX]{x03C0}/2$ at six values of $\hat{R}_{P}$: (a$10$, (b$10^{2}$, (c$10^{3}$, (d$10^{4}$, (e$10^{5}$ and (f$10^{6}$. As in figure 22, the normalization factor used here is the integral of the Poynting vector over a sphere of radius $\hat{R}_{P}=10$ divided by $4\unicode[STIX]{x03C0}$. Vertical coordinates of the points in the distributions at $\hat{R}_{P}=10^{2},10^{3},10^{4},10^{5},10^{6}$ are respectively raised by $20,40,60,80,100$ dBi relative to those in the distribution at $\hat{R}_{P}=10$. The spherically decaying parts of these distributions in $0\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 56.4^{\circ }$ are identical in shape to that for $\hat{R}_{P}=10$ (shown in figure 26) and would coincide if included in this figure. (Values of the parameters used for plotting this figure are those for Case Ib described in § 11.2.)

Figure 27

Figure 28. Polar diagrams of the distributions depicted by curve $a$ of figure 26 (shown in blue) and curves $c$ and $f$ of figure 27 (shown in red and black, respectively). The angle between the radius vector to each point and the vertical axis stands for the polar coordinate $\unicode[STIX]{x1D703}_{P}$ of the observation point. The radial coordinate of each point on the curves $a$, $c$ and $f$ stands for the value of $10\log _{10}(\hat{\boldsymbol{S}})$ that appears in figure 27 against its coordinate $\unicode[STIX]{x1D703}_{P}$ plus $30$ dBi. All three distributions coincide in $0\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 56.4^{\circ }$ where their decay with distance complies with the inverse-square law. Three-dimensional distributions of the radiation patterns at the distances $\hat{R}_{P}=10$, $\hat{R}_{P}=10^{3}$ and $\hat{R}_{P}=10^{6}$ are given by the surfaces of revolution that result from the reflection of curves $a$, $c$ and $f$ with respect to the horizontal axis followed by their rotation about the vertical axis. (Values of the parameters used for plotting this figure are those for Case Ib described in § 11.2.)

Figure 28

Figure 29. Angular dependence of the exponent $\unicode[STIX]{x1D6FC}$ in the power-law $\hat{R}_{P}^{-\unicode[STIX]{x1D6FC}}$ that best describes the decay of the Poynting vector with distance over the range $10\leqslant \hat{R}_{P}\leqslant 10^{6}$. Vertical coordinates of the points plotted in this figure were obtained by applying the procedure illustrated in figure 24 to the data in figure 27. (Values of the parameters used for plotting this figure are those for Case Ib described in § 11.2.)

Figure 29

Figure 30. Logarithmic plot of the time-averaged value of the radial component of the normalized Poynting vector versus the polar angle $\unicode[STIX]{x1D703}_{P}$ for the radiation from the source described in § 10.2 at $10$ light-cylinder radii. The Poynting vector is here divided by the mean value of the flux of power across a sphere of radius $\hat{R}_{P}=10$ (concentric with the ring-shaped source) per unit solid angle. The vertical axis therefore marks the directivity of the radiation source described in § 10.2 at $10$ light-cylinder radii. The distribution of this radiation is independent of the azimuthal angle $\unicode[STIX]{x1D711}_{P}$ and is symmetric with respect to the equatorial plane $\unicode[STIX]{x1D703}_{P}=90^{\circ }$. The sharp changes across $\unicode[STIX]{x1D703}_{P}=60^{\circ }$ and $\unicode[STIX]{x1D703}_{P}=70^{\circ }$ reflect the fact that only an observer in $60^{\circ }<\unicode[STIX]{x1D703}_{P}<70^{\circ }$ can receive the cusped radiation generated by the superluminally rotating volume elements of the distribution pattern of the source. (Values of the parameters used for plotting this figure are those for Case II described in § 11.3.)

Figure 30

Figure 31. Vertically shifted time-averaged values of the radial component of the normalized Poynting vector over the limited range of polar angles where the cusped radiation from the source described in § 10.2 is observable. Curves $a$ to $f$ respectively correspond to the values $10,10^{2},\ldots ,10^{6}$ of the dimensionless distance $\hat{R}_{P}$. The distribution at each $\hat{R}_{P}$ with a value ${\geqslant}10^{2}$ is here shifted upward relative to the preceding distribution at $\hat{R}_{P}/10$ by $20$ dBi. The separation of the curves in this figure is a measure of the degree to which the dependence of the radial component of time-averaged Poynting vector on distance differs from $\hat{R}_{P}^{-2}$. Had $\hat{\boldsymbol{n}}\boldsymbol{\cdot }\hat{\boldsymbol{S}}$ been decaying as $\hat{R}_{P}^{-2}$, a tenfold increase in the value of distance would have resulted in a $20$ dBi decrease in the value of $10\log _{10}(\hat{\boldsymbol{n}}\boldsymbol{\cdot }\hat{\boldsymbol{S}})$ and so the curves $c$, $d$, $e$ and $f$ would have been coincident with curve $a$. The parts of the radiation distribution in $0\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 60^{\circ }$ and $70^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 90^{\circ }$ are identical in shape to those for $\hat{R}_{P}=10$ (shown in figure 31) at all distances and would have coincided had they been included in this figure. (Values of the parameters used for plotting this figure are those for Case II described in § 11.3.)

Figure 31

Figure 32. The results shown in figures 30 and 31 are here depicted in polar coordinates. The value of the radial coordinate of each point on curve $a$ corresponds to that of the time-averaged radial component of the normalized Poynting vector in logarithmic units (shown on the vertical axis of figure 30) plus $10$ dBi, and the value of the polar angle of each point corresponds to that of $\unicode[STIX]{x1D703}_{P}$. This holds true also for the points on curves $c$ and $f$ except that their radial coordinates in $60^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 70^{\circ }$ respectively correspond to the shifted values of $10\log _{10}(\hat{\boldsymbol{n}}\boldsymbol{\cdot }\hat{\boldsymbol{S}})$ for $\hat{R}_{P}=10^{3}$ and $10^{6}$ shown on the vertical axis of figure 31. Three-dimensional distributions of the radiation patterns at the distances $\hat{R}_{P}=10,10^{3}$ and $10^{6}$ are given by the surfaces of revolution that result from the reflection of curves $a$, $c$ and $f$ with respect to the horizontal axis followed by their rotation about the vertical axis. (Values of the parameters used for plotting this figure are those for Case II described in § 11.3.)

Figure 32

Figure 33. The exponent $\unicode[STIX]{x1D6FC}$ in the dependence $\hat{R}_{P}^{-\unicode[STIX]{x1D6FC}}$ of the time-averaged radial component of the Poynting vector on the distance $\hat{R}_{P}$ at the polar angles $60^{\circ }\leqslant \unicode[STIX]{x1D703}_{P}\leqslant 70^{\circ }$ within the cusped radiation beam shown in figure 32. To derive the value of this exponent I have used the data shown in figure 31 to plot $\log (\hat{\boldsymbol{n}}\boldsymbol{\cdot }\hat{\boldsymbol{S}})$ versus $\log \hat{R}_{P}$ at each of the specified $\unicode[STIX]{x1D703}_{P}$ values and to fit the resulting graph with $\log (\hat{\boldsymbol{n}}\boldsymbol{\cdot }\hat{\boldsymbol{S}})=\unicode[STIX]{x1D6FC}^{\prime }-\unicode[STIX]{x1D6FC}\log \hat{R}_{P}-\unicode[STIX]{x1D6FC}^{\prime \prime }(\log \hat{R}_{P})^{2}$ in which $\unicode[STIX]{x1D6FC}$, $\unicode[STIX]{x1D6FC}^{\prime }$ and $\unicode[STIX]{x1D6FC}^{\prime \prime }$ are constants (as in figure 24). The values of $\unicode[STIX]{x1D6FC}^{\prime \prime }$ in the best fits to the data, though significantly smaller than the corresponding values of $\unicode[STIX]{x1D6FC}$ shown here, are also positive. Thus the exponent $\unicode[STIX]{x1D6FC}$ is itself a slowly increasing function of $\hat{R}_{P}$ at any given $\unicode[STIX]{x1D703}_{P}$. (Values of the parameters used for plotting this figure are those for Case II described in § 11.3.)

Figure 33

Figure 34. Fractions of linear polarization $L/I$ (the upper blue dots) and circular polarization $V/I$ (the lower red dots) for the radiation generated by an electric current that flows across the radial dimension of the dielectric ring at $\hat{R}_{P}=10^{2}$. (Values of the parameters used for plotting this figure are those for Case II described in § 11.3.)

Figure 34

Figure 35. The polarization position angle $\unicode[STIX]{x1D713}_{S}$ as a function of the polar coordinate $\unicode[STIX]{x1D703}_{P}$ of the observation point for the radiation generated by an electric current whose direction is everywhere perpendicular to the axis of rotation at $\hat{R}_{P}=10^{2}$. (Values of the parameters used for plotting this figure are those for Case II described in § 11.3.)

Figure 35

Figure 36. The function $\hat{\unicode[STIX]{x1D711}}_{\text{ret}}$ versus $\unicode[STIX]{x1D711}$ for the following fixed set of values of $(r,z;r_{P},\unicode[STIX]{x1D711}_{P},z_{P},t_{P})$ at which $\unicode[STIX]{x1D6E5}$ is positive: $\hat{r}=10$, $\hat{z}=0$, $\hat{r}_{P}=89.13$, $\unicode[STIX]{x1D711}_{P}=\unicode[STIX]{x03C0}/2$, $\hat{z}_{P}=45.34$, $t_{P}=98.92\unicode[STIX]{x1D714}^{-1}$. In this example the time and location of the observer is such that the detected field receives simultaneous contributions from the first three rotation cycles of the source point with the initial ($t=0$) position $\unicode[STIX]{x1D711}=0$, i.e. from $0\leqslant \unicode[STIX]{x1D711}\leqslant 6\unicode[STIX]{x03C0}$. The range ${\mathcal{R}}_{\unicode[STIX]{x1D711}}$ of $\unicode[STIX]{x1D711}$ for which $\hat{\unicode[STIX]{x1D711}}_{\text{ret}}$ falls between $0$ and $2\unicode[STIX]{x03C0}$ consists of the four disjoint intervals $\unicode[STIX]{x1D711}_{1}\leqslant \unicode[STIX]{x1D711}<\unicode[STIX]{x1D711}_{2}$, $2\unicode[STIX]{x03C0}\leqslant \unicode[STIX]{x1D711}<\unicode[STIX]{x1D711}_{3}$, $\unicode[STIX]{x1D711}_{4}\leqslant \unicode[STIX]{x1D711}<\unicode[STIX]{x1D711}_{5}$ and $\unicode[STIX]{x1D711}_{6}<\unicode[STIX]{x1D711}<\unicode[STIX]{x1D711}_{7}$ representing the azimuthal extent of the retarded distribution of the source. The points ($0,\unicode[STIX]{x1D711}_{1}$) and ($\unicode[STIX]{x1D711}_{2},2\unicode[STIX]{x03C0},\unicode[STIX]{x1D711}_{5}$) of the intersections of the above curve with the lines $\hat{\unicode[STIX]{x1D711}}_{\text{ret}}=0$ and $\hat{\unicode[STIX]{x1D711}}_{\text{ret}}=2\unicode[STIX]{x03C0}$ coalesce onto inflection points when the coordinates $(r,z;r_{P},z_{P})$ assume values for which $\unicode[STIX]{x1D6E5}$ vanishes and the source point lies on the cusp locus $C$ of the bifurcation surface.

Figure 36

Figure 37. Time-averaged value of the temporal rate of change of the radiation energy density for Case Ia (described in § 11.1) at polar angles where the radiation decays non-spherically. The curves $a$, $b$, $c$, $d$, $e$ and $f$ respectively correspond to the following values of the distance $\hat{R}_{P}$: $10$ (blue), $10^{2}$ (orange), $10^{3}$ (red), $10^{4}$ (cyan), $10^{5}$ (green) and $10^{6}$ (black). The radiation frequency and the electric current density have the values $\unicode[STIX]{x1D708}=2.5$ GHz and $|j_{z}|=0.01~\text{A}~\text{m}^{-2}$, respectively, and the ratio of the radiation to rotation frequencies is $m=10$. To display all six sets of results on the same graph, I have here multiplied the ordinates of the points for $\hat{R}_{P}=10^{2}$, $10^{3}$, $10^{4}$, $10^{5}$ and $10^{6}$ by the factors $10^{2}$, $10^{4}$, $10^{6}$, $10^{8}$ and $10^{10}$, respectively.

Figure 37

Figure 38. The exponent $\unicode[STIX]{x1D6FD}$ in the dependence $\hat{R}_{P}^{-\unicode[STIX]{x1D6FD}}$ of $\unicode[STIX]{x2202}{\mathcal{U}}/\unicode[STIX]{x2202}t_{P}$ (shown in figure 37) on distance at polar angles $\unicode[STIX]{x1D703}_{P}$ where the radiation decays non-spherically.