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Rotation, Embedding and Topology for the Szekeres Geometry

Charles Hellaby
Dept. of Maths. and Applied Maths, University of Cape Town, Rondebosch, 7701, South Africa
[email protected]
   Robert G. Buckley
Dept. of Physics and Astronomy, University of Texas at San Antonio, San Antonio, Texas 78249, USA
[email protected]
Abstract

Recent work on the Szekeres inhomogeneous cosmological models uncovered a surprising rotation effect. Hellaby showed that the angular (θ,ϕ)(\theta,\phi) coordinates do not have a constant orientation, while Buckley and Schlegel provided explicit expressions for the rate of rotation from shell to shell, as well as the rate of tilt when the 3-space is embedded in a flat 4-d Euclidean space. We here investigate some properties of this embedding, for the quasi-spherical recollapsing case, and use it to show that the two sets of results are in complete agreement. We also show how to construct Szekeres models that are closed in the ‘radial’ direction, and hence have a ‘natural’ embedded torus topology. Several explicit models illustrate the embedding as well as the shell rotation and tilt effects.

1 Previous Work

Since its discovery, the Szekeres inhomogeneous cosmological model has always intrigued relativists, having no Killing vectors on the one hand, and yet still being silent on the other hand. However, the study of this metric has been limited by its relative complication, and, in the cases of the planar and hyperboloidal models, with ϵ+1\epsilon\neq+1, lack of a Newtonian analogy from which to derive physical understanding. Still, precisely because it is one of the most realistic inhomogeneous exact solutions of Einstein’s field equations, which gives it much potential for application in modelling relatively complex cosmological structures on a range of scales, a fuller description of the geometry and the evolution of this spacetime is indispensable to a proper physical understanding.

Szekeres models can be viewed as distortions of Lemaître-Tolman and Ellis models. The three arbitrary functions of the Lemaître-Tolman-Ellis metrics appear in the Szekeres metric playing essentially the same physical roles, but there are three more arbitrary functions that control the deviation from spherical, planar, or pseudo-spherical (hyperboloidal) symmetry. All 6 arbitrary functions depend on the coordinate rr, which is a sort of ‘radial’ coordinate label for comoving 3-surfaces in the quasi-spherical case, and, in the quasi-planar and quasi-hyperboloidal cases, whatever the appropriate equivalent happens to be.

It was obvious from the beginning that the constant rr 2-surfaces (on each time slice) were not arranged ‘concentrically’, and in Szekeres’ original paper [25] he described the 3-spaces as “a set of displaced or ‘non-concentric’ spheres, planes and pseudospheres.”

This non-concentric arrangement was understood and taken into account when slices through Szekeres models were plotted, for example [1, 2, 5, 21, 23, 24, 4, 3, 10]. Again, because of the relative complication of doing this, it hasn’t been attempted very often. Since the native Szekeres coordinates are stereographic, the calculation of slices typically involved converting to angular rr-θ\theta-ϕ\phi coordinates, and then projecting into Cartesian-style XX-YY-ZZ coordinates. However, this method depends on the unstated assumption that the θ\theta-ϕ\phi coordinates maintain a ‘constant’ orientation in some sense.

So it came as a considerable surprise when it was discovered, only recently, that, in the θ\theta-ϕ\phi representation, the constant rr shells are also rotated relative to each other, except in highly specialised cases. In 2013, Buckley & Schlegel [6] stated that the constant rr shells are rotated relative to each other by specific amounts, but did not explain how this was obtained. Unaware of this, Hellaby, in 2017 [15], questioned whether the θ\theta & ϕ\phi coordinates represent a constant orientation, and by studying the variation of a suitable orthonormal tetrad, showed that they don’t. We refer to this paper as “FR”. Two years later, Buckley & Schlegel [7] provided rigorous support for their relative rotation of adjacent shells by developing a local embedding, which required not only the previously stated rotations, but also higher dimensional rotations (or ‘tilts’) in the embedding space. In particular, it demonstrated that these rotations straighten up geodesics. Clearly, this effect must be incorporated into graphical routines for generating slices through Szekeres models, and methods for doing this were presented. We refer to this paper as “PG”.

Confirming that the PG shell rotation and embedding result does indeed explain the origin of the frame rotations found in FR, would be a confirmation of both papers, and a useful validation of the new understanding of the Szekeres geometry, as well as the correct way to plot it graphically.

Further, the consideration of embeddings opens up the question of whether less obvious topologies are possible.

2 Background

2.1 The Lemaître-Tolman Spacetime

The Lemaître-Tolman (LT) spacetime [22, 27] represents a spherically symmetric cloud of dust particles that is inhomogeneous in the radial direction; both the density and the rate of expansion or contraction can vary with radius. Its metric is

ds2=dt2+R2dr21+f+R2(dθ2+sin2θdϕ2),\displaystyle{\rm d}s^{2}=-{\rm d}t^{2}+\frac{R^{\prime 2}\,{\rm d}r^{2}}{1+f}+R^{2}\big{(}{\rm d}\theta^{2}+\sin^{2}\theta{\rm d}\phi^{2}\big{)}~{}, (1)

where R=R(t,r)R=R(t,r) is the areal radius, and f=f(r)f=f(r) is a geometry-energy factor. From the Einstein field equations (EFEs), the evolution equation and the density are

R˙2\displaystyle\dot{R}^{2} =2MR+f+ΛR23,\displaystyle=\frac{2M}{R}+f+\frac{\Lambda R^{2}}{3}~{}, (2)
κρ\displaystyle\kappa\rho =2MR2R,\displaystyle=\frac{2M^{\prime}}{R^{2}R^{\prime}}~{}, (3)

where M=M(r)M=M(r) is the total gravitational mass interior to each constant rr shell, and Λ\Lambda is the cosmological constant. When Λ=0\Lambda=0, the evolution equation (2) has parametric solutions, for example when f<0f<0,

R=M(f)(1cosη),t=a+M(f)3/2(ηsinη).\displaystyle R=\frac{M}{(-f)}\big{(}1-\cos\eta\big{)}~{},~{}~{}~{}~{}~{}~{}t=a+\frac{M}{(-f)^{3/2}}\big{(}\eta-\sin\eta\big{)}~{}. (4)

and a=a(r)a=a(r) is the local ‘bang time’; the time on each constant rr worldline at which R(t,r)=0R(t,r)=0 is t=at=a. The factors

L=M(f)andT=M(f)3/2\displaystyle L=\frac{M}{(-f)}~{}~{}~{}~{}\mbox{and}~{}~{}~{}~{}T=\frac{M}{(-f)^{3/2}} (5)

can be thought of as a scale length and a scale time for the worldline at rr; 2L2L is the maximum areal radius reached, and 2πT2\pi T is the duration from bang to crunch. The derivative RR^{\prime} that appears in the metric can be expressed parametrically as

R\displaystyle R^{\prime} =M(f)(1ϕ1)(1cosη)fMf2(32ϕ11)(1cosη)\displaystyle=\frac{M^{\prime}}{(-f)}(1-\phi_{1})(1-\cos\eta)-\frac{f^{\prime}M}{f^{2}}\left(\frac{3}{2}\phi_{1}-1\right)(1-\cos\eta)
(f)1/2aϕ2(1cosη),\displaystyle~{}~{}~{}~{}-(-f)^{1/2}a^{\prime}\phi_{2}(1-\cos\eta)~{}, (6)
where ϕ1=sinη(ηsinη)(1cosη)2,ϕ2=sinη(1cosη)2.\displaystyle\phi_{1}=\frac{\sin\eta(\eta-\sin\eta)}{(1-\cos\eta)^{2}}~{},~{}~{}~{}~{}~{}~{}\phi_{2}=\frac{\sin\eta}{(1-\cos\eta)^{2}}~{}. (7)

The Ellis [9] metrics are equivalents of the LT case, having planar and hyperboloidal (pseudo-spherical) symmetry.

2.2 The Szekeres Spacetime

The Szekeres (S) spacetimes [25, 26] can be thought of as distortions of the LT and Ellis ones. In addition to the free functions f(r)f(r), M(r)M(r) and a(r)a(r) they have 3 more functions S(r)S(r), P(r)P(r) and Q(r)Q(r) that specify the deviation from symmetry — spherical, planar, or hyperboloidal. The metric is

ds2=dt2+(RREE)2dr2ϵ+f+R2E2(dp2+dq2),\displaystyle{\rm d}s^{2}=-{\rm d}t^{2}+\frac{\left(R^{\prime}-\dfrac{RE^{\prime}}{E}\right)^{2}{\rm d}r^{2}}{\epsilon+f}+\frac{R^{2}}{E^{2}}\big{(}{\rm d}p^{2}+{\rm d}q^{2}\big{)}~{}, (8)

where ϵ=+1,0,1\epsilon=+1,0,-1, and

E=S2((pP)2S2+(qQ)2S2+ϵ).\displaystyle E=\frac{S}{2}\left(\frac{(p-P)^{2}}{S^{2}}+\frac{(q-Q)^{2}}{S^{2}}+\epsilon\right)~{}. (9)

Since S=0S=0 is not possible for a regular metric, we assume S>0S>0. In fact the last term in (8) is R2R^{2} times the 2-metric for a unit sphere, pseudo-sphere, or plane, depending on whether ϵ\epsilon is +1+1, 1-1, or 0. Thus the 3-spaces are foliated by a collection of symmetric 2-spaces, but they are not arranged symmetrically, as we shall see. By the EFEs, R(t,r)R(t,r) obeys exactly the same evolution equation (2), while the density ρ\rho is more complicated,

κρ\displaystyle\kappa\rho =2(M3MEE)R2(RREE).\displaystyle=\frac{2\left(M^{\prime}-\dfrac{3ME^{\prime}}{E}\right)}{R^{2}\left(R^{\prime}-\dfrac{RE^{\prime}}{E}\right)}~{}. (10)

For more information about the Szekeres metric, see for example [20, 16, 17, 14, 28, 6, 7].

2.3 Angular Form of the Szekeres Metric

The standard stereographic mapping, for the ϵ=+1\epsilon=+1 case,

p=P+Scot(θ2)cosϕ,q=Q+Scot(θ2)sinϕ,\displaystyle p=P+S\cot\left(\frac{\theta}{2}\right)\cos\phi~{},~{}~{}~{}~{}~{}~{}q=Q+S\cot\left(\frac{\theta}{2}\right)\sin\phi~{}, (11)

transforms the metric into a more complicated, non-diagonal form,

ds2\displaystyle{\rm d}s^{2} =[1ϵ+f(R+RS{Scosθ+sinθ(Pcosϕ+Qsinϕ)})2\displaystyle=\Bigg{[}\frac{1}{\epsilon+f}\left(R^{\prime}+\frac{R}{S}\big{\{}S^{\prime}\cos\theta+\sin\theta\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}\big{\}}\right)^{2}
+R2S2{Ssinθ+(1cosθ)(Pcosϕ+Qsinϕ)}\displaystyle~{}~{}~{}~{}+\frac{R^{2}}{S^{2}}\big{\{}S^{\prime}\sin\theta+(1-\cos\theta)\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}\big{\}}
+R2S2{(1cosθ)2(PsinϕQcosϕ)}]dr2\displaystyle~{}~{}~{}~{}+\frac{R^{2}}{S^{2}}\big{\{}(1-\cos\theta)^{2}\big{(}P^{\prime}\sin\phi-Q^{\prime}\cos\phi\big{)}\big{\}}\Bigg{]}{\rm d}r^{2}
R2S{Ssinθ+(1cosθ)(Pcosϕ+Qsinϕ)}drdθ\displaystyle~{}~{}~{}~{}-\frac{R^{2}}{S}\big{\{}S^{\prime}\sin\theta+(1-\cos\theta)\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}\big{\}}\,{\rm d}r\,{\rm d}\theta
R2sinθS{(1cosθ)2(PsinϕQcosϕ)}drdϕ\displaystyle~{}~{}~{}~{}-\frac{R^{2}\sin\theta}{S}\big{\{}(1-\cos\theta)^{2}\big{(}P^{\prime}\sin\phi-Q^{\prime}\cos\phi\big{)}\big{\}}\,{\rm d}r\,{\rm d}\phi
+R2(dθ2+sin2θdϕ2).\displaystyle~{}~{}~{}~{}+R^{2}({\rm d}\theta^{2}+\sin^{2}\theta\,{\rm d}\phi^{2})~{}. (12)

For each (t,r)(t,r) 2-sphere, it is sometimes convenient to define a local cartesian frame by

x=Rsinθcosϕy=Rsinθsinϕz=Rcosθ.\displaystyle\begin{aligned} x&=R\sin\theta\cos\phi\\ y&=R\sin\theta\sin\phi\\ z&=R\cos\theta~{}.\end{aligned} (13)

2.4 The Szekeres Dipole

The factor 𝒟=E/E{\mathcal{D}}=E^{\prime}/E that appears in both the metric (8) and the density (10) controls the deviation from spherical, hyperboloidal or planar symmetry, and for ϵ0\epsilon\neq 0 it behaves like a dipole. The dipole has maximum value and orientation

𝒟m=EE|m=JS,pmP=PS{ϵSJ}H2,qmQ=QS{ϵSJ}H2,whereJ=ϵ2S2+ϵ(P2+Q2),H=P2+Q2.\displaystyle\begin{aligned} {\mathcal{D}}_{m}=\left.\frac{E^{\prime}}{E}\right|_{m}&=\frac{J}{S}~{},~{}~{}~{}~{}~{}~{}p_{m}-P=\frac{P^{\prime}S\big{\{}\epsilon S^{\prime}-J\big{\}}}{H^{2}}~{},~{}~{}~{}~{}~{}~{}q_{m}-Q=\frac{Q^{\prime}S\big{\{}\epsilon S^{\prime}-J\big{\}}}{H^{2}}~{},\\ \mbox{where}&~{}~{}~{}~{}~{}~{}~{}~{}J=\sqrt{\epsilon^{2}S^{\prime 2}+\epsilon\big{(}P^{\prime 2}+Q^{\prime 2}\big{)}}\;~{},~{}~{}~{}~{}~{}~{}~{}H=\sqrt{P^{\prime 2}+Q^{\prime 2}}\;~{}.\end{aligned} (14)

The locus E=0E^{\prime}=0 lies on the (p,q)(p,q) circle

((pP)SS+P)+((qQ)SS+Q)=P2+Q2+ϵS2.\displaystyle\left(\frac{(p-P)S^{\prime}}{S}+P^{\prime}\right)+\left(\frac{(q-Q)S^{\prime}}{S}+Q^{\prime}\right)=P^{\prime 2}+Q^{\prime 2}+\epsilon S^{\prime 2}~{}. (15)

For the quasi-spherical case, ϵ=+1\epsilon=+1, the dipole function can be written as

𝒟=EE=Scosθ+sinθ(Pcosϕ+Qsinϕ)S,\displaystyle{\mathcal{D}}=\frac{E^{\prime}}{E}=-\frac{S^{\prime}\cos\theta+\sin\theta\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}}{S}~{}, (16)

and it is evident that E/EE^{\prime}/E ranges between opposite extremes, passing through zero on an ‘equatorial’ circle. Note that here EE^{\prime} still represents the rr derivative at constant pp & qq. The angular position of the dipole maximum is found from

sinθm\displaystyle\sin\theta_{m} =HJ,cosθm=SJ,cosϕm=PH,sinϕm=QH,\displaystyle=\frac{-H}{J}~{},~{}~{}~{}~{}~{}~{}\cos\theta_{m}=\frac{-S^{\prime}}{J}~{},~{}~{}~{}~{}~{}~{}\cos\phi_{m}=\frac{P^{\prime}}{H}~{},~{}~{}~{}~{}~{}~{}\sin\phi_{m}=\frac{Q^{\prime}}{H}~{}, (17)

or, expressed in local Cartesian coordinates, the position of the maximum on the (x,y,z)(x,y,z) unit sphere is

xm\displaystyle x_{m} =sinθmcosϕm=PJ,ym=sinθmsinϕm=QJ,zm=cosθm=SJ,\displaystyle=\sin\theta_{m}\cos\phi_{m}=\frac{-P^{\prime}}{J}~{},~{}~{}~{}~{}~{}~{}y_{m}=\sin\theta_{m}\sin\phi_{m}=\frac{-Q^{\prime}}{J}~{},~{}~{}~{}~{}~{}~{}z_{m}=\cos\theta_{m}=\frac{-S^{\prime}}{J}~{}, (18)

while the E=0E^{\prime}=0 locus is in the plane

Px+Qy+Sz=0.\displaystyle P^{\prime}x+Q^{\prime}y+S^{\prime}z=0~{}. (19)

The dipole has two obvious effects — in the grrg_{rr} component of (8) it creates a non-uniform separation between adjacent 2-spheres of constant rr, and in (10), it creates a variation of the density distribution around each sphere. These effects are in addition to the rr-dependent inhomogeneity of the underlying LT model.

2.5 The Rotations

Relative to the angular form of the Szekeres metric (12), there is another more subtle effect of SS, PP & QQ. The angular coordinates θ\theta & ϕ\phi of (12) do not in fact represent a constant orientation, and their cardinal directions do not parallel transport from one shell to the next. Adjacent 2-spheres have a relative rotation: the sphere at r+δrr+\delta r is rotated

by QSδrabout the x axis\displaystyle\frac{Q^{\prime}}{S}\delta r~{}~{}~{}~{}\mbox{about the $x$ axis} (20a)
and by PSδrabout the y axis,\displaystyle\frac{-P^{\prime}}{S}\delta r~{}~{}~{}~{}\mbox{about the $y$ axis}~{}, (20b)

relative to the one at rr [6]. Four justifications for this were given in [7]. Firstly there is an argument about nearest points on the two spheres, explained in PG, section V.B and fig 4. Secondly, it was shown that geodesics look much straighter once these rotations are incorporated into plots. Thirdly was the calculation in PG appendix C, perhaps not entirely rigorous, that added displacements and rotations to the LT metric, ending up with the S metric. Fourthly, an embedding of any given constant tt 3-space of the angular S metric for ϵ=+1\epsilon=+1, into a 4-d space that is flat or has constant curvature, turned out to require the above-stated rotations.

3 Embeddings

3.1 Global Embedding of Positively Curved LT 3-Spaces

Let 𝔼4\mathbb{E}^{4} be a 4-d Euclidean space with Cartesian coordinates, X,Y,Z,WX,Y,Z,W, and let the LT 3-spaces have positive curvature, 1f0-1\leq f\leq 0. At a fixed time tt, RR becomes a function of rr only. We define a 3-surface Σ\Sigma by

X\displaystyle X =R(r)sinθcosϕ,\displaystyle=R(r)\sin\theta\cos\phi~{}, (21a)
Y\displaystyle Y =R(r)sinθsinϕ,\displaystyle=R(r)\sin\theta\sin\phi~{}, (21b)
Z\displaystyle Z =R(r)cosθ,\displaystyle=R(r)\cos\theta~{}, (21c)
W\displaystyle W =0rR(r)α(r)dr,\displaystyle=\int_{0}^{r}R^{\prime}(r)\alpha(r)\,{\rm d}r~{}, (21d)

so then

dX\displaystyle{\rm d}X =Rsinθcosϕdr+RcosθcosϕdθRsinθsinϕdϕ,\displaystyle=R^{\prime}\sin\theta\cos\phi\,{\rm d}r+R\cos\theta\cos\phi\,{\rm d}\theta-R\sin\theta\sin\phi\,{\rm d}\phi~{}, (22a)
dY\displaystyle{\rm d}Y =Rsinθsinϕdr+Rcosθsinϕdθ+Rsinθcosϕdϕ,\displaystyle=R^{\prime}\sin\theta\sin\phi\,{\rm d}r+R\cos\theta\sin\phi\,{\rm d}\theta+R\sin\theta\cos\phi\,{\rm d}\phi~{}, (22b)
dZ\displaystyle{\rm d}Z =RcosθdrRsinθdθ,\displaystyle=R^{\prime}\cos\theta\,{\rm d}r-R\sin\theta\,{\rm d}\theta~{}, (22c)
dW\displaystyle{\rm d}W =Rα(r).\displaystyle=R^{\prime}\alpha(r)~{}. (22d)

Here R(r)R(r) is the LT areal radius R(t,r)R(t,r) at a particular time, and α\alpha is

α\displaystyle\alpha =±f(r)1+f(r).\displaystyle=\pm\sqrt{\frac{-f(r)}{1+f(r)}}\;~{}. (23)

Now in [13] the function ff was interpreted as f=cos2ψf=-\cos^{2}\psi where ψ\psi is the angle of the tangent cone to the embedded surface at rr, and in this notation, then, α=cotψ\alpha=\cot\psi:

tanψ=dRdW=R|Rf1+f|=±1+ff=1α\displaystyle\tan\psi=\frac{{\rm d}R}{{\rm d}W}=\frac{R^{\prime}}{\left|R^{\prime}\sqrt{\dfrac{-f}{1+f}}\;\right|}=\pm\sqrt{\dfrac{1+f}{-f}}\;=\frac{1}{\alpha} (24)
cosψ=f,sinψ=1+f,cotψ=α.\displaystyle\to~{}~{}~{}~{}~{}~{}~{}~{}\cos\psi=\sqrt{-f}\;~{},~{}~{}~{}~{}\sin\psi=\sqrt{1+f}\;~{},~{}~{}~{}~{}\cot\psi=\alpha~{}. (25)

Since f0f\leq 0, closed models are quite likely, in which case there will be at least one point rmr_{m} that is a maximum (or minimum) in RR where R=0R^{\prime}=0, f=1f=-1, but R/1+fR^{\prime}/\sqrt{1+f}\; is finite [18, 13]. As a spatial extremum is approached and traversed, RR^{\prime}, ψ\psi and α\alpha change sign, RR^{\prime} & ψ\psi passing through zero and α\alpha diverging. This ensures dW/dr{\rm d}W/{\rm d}r retains a constant sign111This is not essential, and other choices could lead to different valid embeddings..

Using this embedding, (21) and (22) show that the metric of the 3-surface becomes

dX2\displaystyle{\rm d}X^{2} +dY2+dZ2+dW2=R2dr21+f+R2(dθ2+sin2θdϕ2)\displaystyle+{\rm d}Y^{2}+{\rm d}Z^{2}+{\rm d}W^{2}=\frac{R^{\prime 2}\,{\rm d}r^{2}}{1+f}+R^{2}\big{(}{\rm d}\theta^{2}+\sin^{2}\theta\,{\rm d}\phi^{2}\big{)} (26)

which is the spatial part of the LT metric, dt=0{\rm d}t=0.

In the case that

R=Ksinr,R=Kcosr\displaystyle R=K\sin r~{},~{}~{}~{}~{}R^{\prime}=K\cos r ,f=sin2r,Kconstant,\displaystyle~{},~{}~{}~{}~{}f=-\sin^{2}r~{},~{}~{}~{}~{}K~{}\mbox{constant,} (27)
we find
R2dr21+f+R2(dθ2+sin2θdϕ2)\displaystyle\frac{R^{\prime 2}\,{\rm d}r^{2}}{1+f}+R^{2}\big{(}{\rm d}\theta^{2}+\sin^{2}\theta\,{\rm d}\phi^{2}\big{)} =K2(dr2+sin2r(dθ2+sin2θdϕ2))\displaystyle=K^{2}\Big{(}{\rm d}r^{2}+\sin^{2}r\big{(}{\rm d}\theta^{2}+\sin^{2}\theta\,{\rm d}\phi^{2}\big{)}\Big{)} (28)

and Σ\Sigma becomes the 3-sphere.

3.2 Buckley & Schlegel’s Local Szekeres Embedding

For quasi-spherical S models with f<0f<0, their constant tt 3-spaces can be embedded in a 4-d flat space, but for general ff, one must embed in a 4-space of constant curvature [7]. We here consider the former case. Let 𝔼4\mathbb{E}^{4} be a 4-d Euclidean space with Cartesian coordinates, X,Y,Z,WX,Y,Z,W. In this 4-space, a 3-surface is constructed from a sequence of 2-spheres, by expanding, shifting and rotating a unit sphere, as a function of parameter rr. Suitable choices of the expansion, shift and rotation functions ensure the intrinsic metric of the 3-surface is identical with the positively curved, quasi-spherical Szekeres 3-spaces of constant tt. While an embedding is primarily a visualisation tool, in this case it also provides a clear confirmation of Buckley and Schlegel’s rotations, given in equation (20).

It is also convenient to define local Cartesian coordinates, x,y,z,wx,y,z,w near each constant rr shell. In these coordinates, the 2-spherical shell lies in the w=0w=0 3-space, according to (13), so the accumulated displacements and rotations are ignored, and the focus is on the local rate of displacement and rotation.

Buckley & Schlegel’s embedding equation is

V(r,θ,ϕ)=R(r)AT(r)U(θ,ϕ)+Δ(r),\displaystyle V(r,\theta,\phi)=R(r)A^{T}(r)U(\theta,\phi)+\Delta(r)~{}, (29)

where VV is a point in 𝔼4\mathbb{E}^{4} and UU is a unit sphere,

V=(XYZW),U=(sinθcosϕsinθsinϕcosθ0),\displaystyle V=\begin{pmatrix}X\\ Y\\ Z\\ W\end{pmatrix}~{},~{}~{}~{}~{}~{}~{}U=\begin{pmatrix}\sin\theta\cos\phi\\ \sin\theta\sin\phi\\ \cos\theta\\ 0\end{pmatrix}~{}, (30)

while the rotation matrix AA, and the displacement vector Δ\Delta, are functions of rr that satisfy the following differential equations (DEs)

A(r)\displaystyle A^{\prime}(r) =Ω(r)A(r)=(00PSPSα00QSQSαPSQS0SSαPSαQSαSSα0)A(r),\displaystyle=\Omega^{\prime}(r)A(r)=\begin{pmatrix}0&0&\dfrac{P^{\prime}}{S}&\dfrac{P^{\prime}}{S}\alpha\\[5.69054pt] 0&0&\dfrac{Q^{\prime}}{S}&\dfrac{Q^{\prime}}{S}\alpha\\[5.69054pt] -\dfrac{P^{\prime}}{S}&-\dfrac{Q^{\prime}}{S}&0&\dfrac{S^{\prime}}{S}\alpha\\[5.69054pt] -\dfrac{P^{\prime}}{S}\alpha&-\dfrac{Q^{\prime}}{S}\alpha&-\dfrac{S^{\prime}}{S}\alpha&0\end{pmatrix}A(r)~{}, (31)
Δ(r)\displaystyle\Delta^{\prime}(r) =AT(r)D(r)=AT(r)(RPSRQSRSSRα),\displaystyle=A^{T}(r)D^{\prime}(r)=A^{T}(r)\begin{pmatrix}R\dfrac{P^{\prime}}{S}\\[5.69054pt] R\dfrac{Q^{\prime}}{S}\\[5.69054pt] R\dfrac{S^{\prime}}{S}\\[5.69054pt] R^{\prime}\alpha\end{pmatrix}~{}, (32)

where α\alpha is given by (23), and here too one may specify that it have the same sign as RR^{\prime}. The intrinsic 3-metric of the embedded 3-surface is derived from the differential of VV, using (29)-(32),

ds2\displaystyle{\rm d}s^{2} =g(dV,dV)=dVTdV\displaystyle=g({\rm d}V,{\rm d}V)={\rm d}V^{T}\,{\rm d}V (33)
dV\displaystyle{\rm d}V =(Rdr)ATU+R((AT)dr)U+RAT(Uθdθ+Uϕdϕ)+Δdr\displaystyle=(R^{\prime}\,{\rm d}r)A^{T}U+R((A^{T})^{\prime}\,{\rm d}r)U+RA^{T}(U_{\theta}\,{\rm d}\theta+U_{\phi}\,{\rm d}\phi)+\Delta^{\prime}\,{\rm d}r (34)
=RATUdr+R(AT(Ω)T)Udr+RAT(Uθdθ+Uϕdϕ)+ATDdr\displaystyle=R^{\prime}A^{T}U\,{\rm d}r+R(A^{T}(\Omega^{\prime})^{T})U\,{\rm d}r+RA^{T}(U_{\theta}\,{\rm d}\theta+U_{\phi}\,{\rm d}\phi)+A^{T}D^{\prime}\,{\rm d}r (35)
=AT[(RU+R(Ω)TU+D)dr+RUθdθ+RUϕdϕ]\displaystyle=A^{T}\big{[}(R^{\prime}U+R(\Omega^{\prime})^{T}U+D^{\prime}){\rm d}r+RU_{\theta}\,{\rm d}\theta+RU_{\phi}\,{\rm d}\phi\big{]} (36)
ds2\displaystyle{\rm d}s^{2} =[(RUT+RUTΩ+(D)T)dr+RUθTdθ+RUϕTdϕ]\displaystyle=\big{[}(R^{\prime}U^{T}+RU^{T}\Omega^{\prime}+(D^{\prime})^{T}){\rm d}r+RU_{\theta}^{T}\,{\rm d}\theta+RU_{\phi}^{T}\,{\rm d}\phi\big{]}
[(RU+R(Ω)TU+D)dr+RUθdθ+RUϕdϕ]\displaystyle~{}~{}~{}~{}~{}~{}\big{[}(R^{\prime}U+R(\Omega^{\prime})^{T}U+D^{\prime}){\rm d}r+RU_{\theta}\,{\rm d}\theta+RU_{\phi}\,{\rm d}\phi\big{]} (37)
=dr2{R2UTU+RR[UT(Ω)TU+UTΩU]+R[UTD+(D)TU]\displaystyle={\rm d}r^{2}\big{\{}R^{\prime 2}U^{T}U+RR^{\prime}\big{[}U^{T}(\Omega^{\prime})^{T}U+U^{T}\Omega^{\prime}U\big{]}+R^{\prime}\big{[}U^{T}D^{\prime}+(D^{\prime})^{T}U\big{]}
+R2UTΩ(Ω)TU+R[UTΩD+(D)T(Ω)TU]+(D)TD}\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}+R^{2}U^{T}\Omega^{\prime}(\Omega^{\prime})^{T}U+R\big{[}U^{T}\Omega^{\prime}D^{\prime}+(D^{\prime})^{T}(\Omega^{\prime})^{T}U\big{]}+(D^{\prime})^{T}D^{\prime}\big{\}}
+drdθ{RR[UTUθ+UθTU]+R2[UTΩUθ+UθT(Ω)TU]\displaystyle~{}~{}~{}+{\rm d}r{\rm d}\theta\big{\{}RR^{\prime}\big{[}U^{T}U_{\theta}+U_{\theta}^{T}U\big{]}+R^{2}\big{[}U^{T}\Omega^{\prime}U_{\theta}+U_{\theta}^{T}(\Omega^{\prime})^{T}U\big{]}
+R[(D)TUθ+UθTD]}\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}+R\big{[}(D^{\prime})^{T}U_{\theta}+U_{\theta}^{T}D^{\prime}\big{]}\big{\}}
+drdϕ{RR[UTUϕ+UϕTU]+R2[UTΩUϕ+UϕT(Ω)TU]\displaystyle~{}~{}~{}+{\rm d}r{\rm d}\phi\big{\{}RR^{\prime}\big{[}U^{T}U_{\phi}+U_{\phi}^{T}U\big{]}+R^{2}\big{[}U^{T}\Omega^{\prime}U_{\phi}+U_{\phi}^{T}(\Omega^{\prime})^{T}U\big{]}
+R[(D)TUϕ+UϕTD]}\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}+R\big{[}(D^{\prime})^{T}U_{\phi}+U_{\phi}^{T}D^{\prime}\big{]}\big{\}}
+dθ2{R2UθTUθ}+dθdϕ{R2[UθTUϕ+UϕTUθ]}+dϕ2{R2UϕTUϕ}\displaystyle~{}~{}~{}+{\rm d}\theta^{2}\big{\{}R^{2}U_{\theta}^{T}U_{\theta}\big{\}}+{\rm d}\theta{\rm d}\phi\big{\{}R^{2}\big{[}U_{\theta}^{T}U_{\phi}+U_{\phi}^{T}U_{\theta}\big{]}\Big{\}}+{\rm d}\phi^{2}\big{\{}R^{2}U_{\phi}^{T}U_{\phi}\big{\}} (38)

where

Uθ=(cosθcosϕcosθsinϕsinθ0),Uϕ=(sinθsinϕsinθcosϕ00)\displaystyle U_{\theta}=\begin{pmatrix}\cos\theta\cos\phi\\ \cos\theta\sin\phi\\ -\sin\theta\\ 0\end{pmatrix}~{},~{}~{}~{}~{}~{}~{}~{}~{}U_{\phi}=\begin{pmatrix}-\sin\theta\sin\phi\\ \sin\theta\cos\phi\\ 0\\ 0\end{pmatrix} (39)

Evaluating the various matrix products, we find

0=UTΩU=UT(Ω)TU=UTUθ=UθTU=UTUϕ=UϕTU=UθTUϕ=UϕTUθ\displaystyle 0=U^{T}\Omega^{\prime}U=U^{T}(\Omega^{\prime})^{T}U=U^{T}U_{\theta}=U_{\theta}^{T}U=U^{T}U_{\phi}=U_{\phi}^{T}U=U_{\theta}^{T}U_{\phi}=U_{\phi}^{T}U_{\theta} (40a)
1=UTU=UθTUθ\displaystyle 1=U^{T}U=U_{\theta}^{T}U_{\theta} (40b)
UϕTUϕ=sin2θ\displaystyle U_{\phi}^{T}U_{\phi}=\sin^{2}\theta (40c)
(D)TU=UTD=RS{sinθ(Pcosϕ+Qsinϕ)+Scosθ}\displaystyle(D^{\prime})^{T}U=U^{T}D^{\prime}=\frac{R}{S}\big{\{}\sin\theta\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}+S^{\prime}\cos\theta\big{\}} (40d)
(D)T(Ω)TU=UTΩD=RS2{Ssinθ(Pcosϕ+Qsinϕ)(P2+Q2)cosθ}\displaystyle(D^{\prime})^{T}(\Omega^{\prime})^{T}U=U^{T}\Omega^{\prime}D^{\prime}=\frac{R}{S^{2}}\big{\{}S^{\prime}\sin\theta\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}-\big{(}P^{\prime 2}+Q^{\prime 2}\big{)}\cos\theta\big{\}}
+Rα2S{sinθ(Pcosϕ+Qsinϕ)+cosθS}\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}+\frac{R^{\prime}\alpha^{2}}{S}\big{\{}\sin\theta\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}+\cos\theta S^{\prime}\big{\}} (40e)
(D)TD=R2S2{P2+Q2+S2}+R2α2\displaystyle(D^{\prime})^{T}D^{\prime}=\frac{R^{2}}{S^{2}}\big{\{}P^{\prime 2}+Q^{\prime 2}+S^{\prime 2}\big{\}}+R^{\prime 2}\alpha^{2} (40f)
UTΩ(Ω)TU=α2S2({Scosθ+sinθ(Pcosϕ+Qsinϕ)}2\displaystyle U^{T}\Omega^{\prime}(\Omega^{\prime})^{T}U=\frac{\alpha^{2}}{S^{2}}\Big{(}\big{\{}S^{\prime}\cos\theta+\sin\theta\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}\big{\}}^{2}
+sin2θS2{Pcosϕ+Qsinϕ}2+cos2θ{P2+Q2})\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}+\frac{\sin^{2}\theta}{S^{2}}\big{\{}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{\}}^{2}+\cos^{2}\theta\big{\{}P^{\prime 2}+Q^{\prime 2}\big{\}}\Big{)} (40g)
UTΩUθ=UθT(Ω)TU={Pcosϕ+Qsinϕ}S\displaystyle U^{T}\Omega^{\prime}U_{\theta}=U_{\theta}^{T}(\Omega^{\prime})^{T}U=-\frac{\big{\{}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{\}}}{S} (40h)
UTΩUϕ=UϕT(Ω)TU=cosθsinθ{PsinϕQcosϕ}S\displaystyle U^{T}\Omega^{\prime}U_{\phi}=U_{\phi}^{T}(\Omega^{\prime})^{T}U=\frac{\cos\theta\sin\theta\big{\{}P^{\prime}\sin\phi-Q^{\prime}\cos\phi\big{\}}}{S} (40i)
(D)TUθ=UθTD=RS{cosθ(Pcosϕ+Qsinϕ)Ssinθ}\displaystyle(D^{\prime})^{T}U_{\theta}=U_{\theta}^{T}D^{\prime}=\frac{R}{S}\big{\{}\cos\theta\big{(}P^{\prime}\cos\phi+Q^{\prime}\sin\phi\big{)}-S^{\prime}\sin\theta\big{\}} (40j)
(D)TUϕ=UϕTD=RsinθS{PsinϕQcosϕ}\displaystyle(D^{\prime})^{T}U_{\phi}=U_{\phi}^{T}D^{\prime}=-\frac{R\sin\theta}{S}\big{\{}P^{\prime}\sin\phi-Q^{\prime}\cos\phi\big{\}} (40k)

and we recover the metric (12) of the angular form of the quasi-spherical Szekeres metric.

3.3 Visualising the Local Embedding Geometry

Although there is no physical significance to the embedding of a given spacetime into one of higher dimension, it can be very helpful for visualising the spacetime geometry, and that is what we explore here.

We note that the constant ww projection of DD^{\prime}, (32), is anti-parallel to the (x,y,z)(x,y,z) direction of the dipole maximum, (18). For the local rate-of-rotation matrix Ω\Omega^{\prime}, the fixed point locus is a 2-plane,

ΩV=0Vfp=(SλSμ(Pλ+Qμ)(Pλ+Qμ)α),λ,μindependent parameters,\displaystyle\Omega^{\prime}\>V=0~{}~{}~{}~{}~{}~{}\to~{}~{}~{}~{}~{}~{}V_{fp}=\begin{pmatrix}S^{\prime}\lambda\\ S^{\prime}\mu\\[2.84526pt] -(P^{\prime}\lambda+Q^{\prime}\mu)\\[5.69054pt] \dfrac{(P^{\prime}\lambda+Q^{\prime}\mu)}{\alpha}\end{pmatrix}~{},~{}~{}~{}~{}\lambda,\mu~{}\mbox{independent parameters}, (41)

which makes Ω\Omega^{\prime} the derivative of a simple rotation (not a double or isoclinic rotation). The constant ww projections of DD^{\prime} and VfpV_{fp} are orthogonal. This last fact ensures the maximum tilt-displacements occur along the dipole axis (where the max & min are located) — see fig 3.3 — and thus enables the following argument.

In the local (x,y,z,w)(x,y,z,w) frame, the constant rr 2-sphere lies in the xx-yy-zz 3-space, and the direction o=(0,0,0,1)o=(0,0,0,1) is orthogonal to that space. In going from the 2-sphere at rr to the 2-sphere at r+δrr+\delta r, the displacement of the sphere centres is DδrD^{\prime}\,\delta r; the rate of perpendicular displacement is RαR^{\prime}\alpha, and the rates of sideways displacement are RP/SRP^{\prime}/S, RQ/SRQ^{\prime}/S, & RS/SRS^{\prime}/S, towards the ++ve xx, yy, & zz directions222We here assume that PP^{\prime}, QQ^{\prime}, & SS^{\prime} are positive. Where the opposite sign occurs, the relevant direction is changed in the obvious way.. The slant angle, between oo and the line of centres, is

cosγ=oD|D|=RαR2𝒟m2+R2α2\displaystyle\cos\gamma=o\cdot\frac{D^{\prime}}{|D^{\prime}|}=\frac{R^{\prime}\alpha}{\sqrt{R^{2}{\mathcal{D}}_{m}^{2}+R^{\prime 2}\alpha^{2}}\;} (42)

which we could re-write as ‘component’ angles333These ‘components’ are the projections of γ\gamma onto the xx-ww, yy-ww, and zz-ww planes, such that tan2γ=tan2γx+tan2γy+tan2γz\tan^{2}\gamma=\tan^{2}\gamma_{x}+\tan^{2}\gamma_{y}+\tan^{2}\gamma_{z}.

tanγx=RPRαS,tanγy=RQRαS,tanγz=RSRαS.\displaystyle\tan\gamma_{x}=\frac{RP^{\prime}}{R^{\prime}\alpha S}~{},~{}~{}~{}~{}~{}~{}\tan\gamma_{y}=\frac{RQ^{\prime}}{R^{\prime}\alpha S}~{},~{}~{}~{}~{}~{}~{}\tan\gamma_{z}=\frac{RS^{\prime}}{R^{\prime}\alpha S}~{}. (43)

Since the total rotation used in (29) is ATA^{T}, we see from (31) that the local rotation-rate matrix to examine is (Ω)T(\Omega^{\prime})^{T}. The components of the local rate-of-shell-rotation are thus

ωxzδr=PSδr,ωyzδr=QSδr,ωxyδr=0,\displaystyle\omega_{xz}^{\prime}\,\delta r=\frac{-P^{\prime}}{S}\,\delta r~{},~{}~{}~{}~{}~{}~{}\omega_{yz}^{\prime}\,\delta r=\frac{-Q^{\prime}}{S}\,\delta r~{},~{}~{}~{}~{}~{}~{}\omega_{xy}^{\prime}\,\delta r=0~{}, (44)

with senses as noted above, and the components of rate-of-tilt are

ζxwδr=PαSδr,ζywδr=QαSδr,ζzwδr=SαSδr.\displaystyle\zeta_{xw}^{\prime}\,\delta r=\frac{-P^{\prime}\alpha}{S}\,\delta r~{},~{}~{}~{}~{}~{}~{}\zeta_{yw}^{\prime}\,\delta r=\frac{-Q^{\prime}\alpha}{S}\,\delta r~{},~{}~{}~{}~{}~{}~{}\zeta_{zw}^{\prime}\,\delta r=\frac{-S^{\prime}\alpha}{S}\,\delta r~{}. (45)

Therefore the rates of tilt are α/R\alpha/R times the rates of sideways displacement, and a 3-plane parallel to w=0w=0 is tilted down on the x-x, y-y, & z-z sides by ζxw\zeta_{xw}, ζyw\zeta_{yw}, & ζzw\zeta_{zw}, respectively.

Both these effects, the centre displacement and the tilt, decrease the shell separation where 𝒟{\mathcal{D}} has the same sign as RR^{\prime} (the ’closing edge’) and increase it where 𝒟{\mathcal{D}} has the opposite sign (the ’opening edge’). The no-shell-crossing conditions ensure the separation stays positive all round each sphere. Fig 3.3 illustrates the arrangement for the case when R>0R^{\prime}>0. Although finite displacements are shown, one should think of δr\delta r as infinitesimal, so that only first order effects are relevant. The four displacements shown are:

the ww-separation of shell centres =δw0=Rαδr,\displaystyle=\delta w_{0}=R^{\prime}\alpha\,\delta r~{}, (46a)
the increase in shell radius =δd0=Rαtanψδr=Rδr,\displaystyle=\delta d_{0}=R^{\prime}\alpha\tan\psi\,\delta r=R^{\prime}\,\delta r~{}, (46b)
the tilt down displacement where 𝒟{\mathcal{D}} is max =δw1=Rζδr=Rα𝒟mδr,\displaystyle=\delta w_{1}=R\zeta^{\prime}\,\delta r=R\alpha{\mathcal{D}}_{m}\,\delta r~{}, (46c)
the dipole displacement of the shell centre =δd1=R𝒟mδr.\displaystyle=\delta d_{1}=R{\mathcal{D}}_{m}\,\delta r~{}. (46d)

Interestingly, δd0\delta d_{0} & δw0\delta w_{0} make the same angle as δd1\delta d_{1} & δw1\delta w_{1}. This angle coincidence is possibly the reason why the calculation in appendix C of PG actually works — because the displaced & tilted shell ar r+δrr+\delta r more or less lies on the LT tangent cone to the 3-surface at rr, to first order.

*(1,16)(145,54) maxminδw0\delta w_{0}δd1\delta d_{1}γ\gammaδw0\delta w_{0}δd0\delta d_{0}δw1\delta w_{1}δd1\delta d_{1}δw0\delta w_{0}δd0\delta d_{0}δd1\delta d_{1}δw1\delta w_{1}ψ\psi Fig 1.   Sketch of the displacement and tilt effects in the embedding, with one dimension suppressed. Because the sketch shows finite displacements, instead of infinitesimal ones, the distances shown are not exact. The green shows the embedding of the underlying LT model — the shells at rr (lower) and r+δrr+\delta r (upper) and the local tangent cone. The blue vectors show the ww displacement between the two shells and the radial expansion of the second shell (assumed positive here). The cyan shows the displaced and tilted shell at r+δrr+\delta r of the Szekeres model. The red vectors show the sideways displacement of the shell centre, and the down or up displacement due to the tilt. The dipole maximum is located at the left side, and the minimum at the right. The E=0E^{\prime}=0 locus, the ‘widest’ part of the 2-sphere at r+δrr+\delta r is shifted by δd1\delta d_{1}; this is consistent — a tilted slice through the LT cone has a displaced ‘greatest width’. The tilt axis is the magenta dashed line, and it is perpendicular to the red displacement δd1\delta d_{1}. The θ\theta-ϕ\phi rotation is not shown.

Looking at the next shell pair, at r+δrr+\delta r and r+2δrr+2\delta r, the local LT tangent cone is now tilted by ζ\zeta, and the r+2δrr+2\delta r shell is tilted further. The slant angle γ\gamma is also tilted by ζ\zeta.

A reflection in the bottom plane gives an idea of the R<0R^{\prime}<0 case. Where R<0R^{\prime}<0, α\alpha also flips sign and 𝒟m{\mathcal{D}}_{m} goes to 𝒟m-{\mathcal{D}}_{m} in (46).

3.4 Origins, Extrema & Self-Intersections

Using the expressions in (46), we examine the limiting values of these embedding quantities near origins and spatial extrema. We assume there are no shell crossings. If there are, then RR^{\prime} & α\alpha do not always flip signs together. We also assume a well behaved rr coordinate, with RR finite & non-zero everywhere except at an origin, r=ror=r_{o}, and RR^{\prime} finite & non-zero everywhere except at a spatial extremum, r=rer=r_{e}. We further assume ‘generic’ arbitrary functions, so that, for example, RR^{\prime} & 𝒟{\mathcal{D}} go linearly through zero at an extremum444One may intentionally choose functions that give other behaviour at specific locations, such as RR^{\prime} or 𝒟{\mathcal{D}} going quadratically to zero and not changing sign. . The results are gathered in table 3.4.
flips sign with flips sign behaviour at behaviour 𝒟m𝒟m{\mathcal{D}}_{m}\to-{\mathcal{D}}_{m} with RR^{\prime} R01/αR^{\prime}\to 0\leftarrow 1/\alpha at R0R\to 0 RR RR~{}\to~{}const 0\to~{}0 as (rro)(r-r_{o}) RR^{\prime} R0R^{\prime}~{}\to~{}0 as (rre)(r-r_{e}) \to~{}const 0\neq 0 α\alpha α\alpha~{}\to~{}\infty as (rre)1(r-r_{e})^{-1} 0\to~{}0 as (rro)(r-r_{o}) 𝒟m{\mathcal{D}}_{m} 𝒟m0{\mathcal{D}}_{m}~{}\to~{}0 as (rre)(r-r_{e}) \to~{}const (or 0) δw0\delta w_{0} No No RαR^{\prime}\alpha~{}\to~{}const 0\to~{}0 as (rro)(r-r_{o}) δd0\delta d_{0} No Yes R0R^{\prime}~{}\to~{}0 as (rre)(r-r_{e}) \to~{}const 0\neq 0 δw1\delta w_{1} Yes Yes Rα𝒟mR\alpha{\mathcal{D}}_{m}~{}\to~{}const 0\to~{}0 as (rro)2(r-r_{o})^{2} δd1\delta d_{1} Yes No R𝒟m0R{\mathcal{D}}_{m}~{}\to~{}0 as (rre)(r-r_{e}) 0\to~{}0 as (rro)(r-r_{o}) dipole slant δd1/δw0\delta d_{1}/\delta w_{0} Yes No (R𝒟m)/(Rα)0(R{\mathcal{D}}_{m})/(R^{\prime}\alpha)~{}\to~{}0 as (rre)(r-r_{e}) \to~{}const tilt rate δw1/R\delta w_{1}/R Yes Yes α𝒟m\alpha{\mathcal{D}}_{m}~{}\to~{}const 0\to~{}0 as (rro)(r-r_{o})
Table 1.   The behaviour of embedding displacements near origins and spatial extrema. See (46) and the illustration in fig. 3.3.

Now, at an origin, where R(t,ro)0tR(t,r_{o})\to 0~{}\forall~{}t, we see that the dipole slant does not disappear, but the tilt-rate must disappear.

In contrast, at a spatial extremum, where R(t,re)0tR^{\prime}(t,r_{e})\to 0~{}\forall~{}t, the dipole slant must disappear, whereas the tilt rate does not disappear.

The condition for no local self-intersection (of adjacent shells), referring to fig 3.3 and (46), is just:

|δw1|\displaystyle|\delta w_{1}| <|δw0|,\displaystyle<|\delta w_{0}|~{},
|Rα𝒟mδr|\displaystyle|R\alpha{\mathcal{D}}_{m}\,\delta r| <|Rαδr|,\displaystyle<|R^{\prime}\alpha\,\delta r|~{},
𝒟m\displaystyle{\mathcal{D}}_{m} <|RR|.\displaystyle<\left|\frac{R^{\prime}}{R}\right|~{}. (47)

Interestingly, this is just the no-shell-crossing conditions for SS, PP & QQ [16, 14].

3.5 Centre-Line Curvature

We now consider the locus of 2-sphere centres in the embedding space; that is, in the (X,Y,Z,W)(X,Y,Z,W) frame. (The previous section mostly used the local (x,y,z,w)(x,y,z,w) frame.)

For simplicity, we will consider a model in which P=Q=0P^{\prime}=Q^{\prime}=0 everywhere. Between rr and r+δrr+\delta r, the slant angle between oo and the line of centres changes by γzδr\gamma_{z}^{\prime}\,\delta r. Part of this change is due to the fact that in the same span, the 2-spheres of constant rr undergo a tilt in the same direction by an angle ζzwδr\zeta_{zw}^{\prime}\,\delta r, and oo’s angle changes along with them by the same amount. The rest must be due to the change in the angle of the line of centres itself. See fig 3.5. If we denote this change of the line-of-centres angle by δξ\delta\xi, we can write

δξ\displaystyle\delta\xi =γzδr+ζzwδr\displaystyle=\gamma_{z}^{\prime}\,\delta r+\zeta_{zw}^{\prime}\,\delta r (48)

[Uncaptioned image]

Fig 2.   A diagram of the contributions to the centre line curvature. Solid lines represent values at rr, and dashed lines represent values at r+δrr+\delta r. The green lines show the shells’ orientations. The blue lines are the vectors oo orthogonal to the shells, and the change between them is the rate of tilt, ζzw\zeta_{zw}^{\prime}. The red lines are the tangent vectors of the line of centres, which changes by δξ\delta\xi. The angles between the two, written in purple, are the slant angles γz\gamma_{z}. Looking at the solid blue line and the dashed red line, we can see that the total angle between them is equal to γ+δξ\gamma+\delta\xi, but also equal to ζzwδr+γz+γzδr\zeta_{zw}^{\prime}\delta r+\gamma_{z}+\gamma_{z}^{\prime}\delta r, giving the result δξ=γzδr+ζzwδr\delta\xi=\gamma_{z}^{\prime}\delta r+\zeta_{zw}^{\prime}\delta r.

Eq (45) gives ζzw\zeta_{zw}^{\prime} directly. We can calculate γz\gamma_{z}^{\prime} from eq (43) as follows:

γzsec2γz\displaystyle\gamma_{z}^{\prime}\sec^{2}\gamma_{z} =γz(1+tan2γz)=1αSSRR′′R2αSSRαRα2SS+RRα(SS)\displaystyle=\gamma_{z}^{\prime}(1+\tan^{2}\gamma_{z})=\frac{1}{\alpha}\frac{S^{\prime}}{S}-\frac{R\,R^{\prime\prime}}{R^{\prime 2}\alpha}\frac{S^{\prime}}{S}-\frac{R\,\alpha^{\prime}}{R^{\prime}\alpha^{2}}\frac{S^{\prime}}{S}+\frac{R}{R^{\prime}\alpha}\left(\frac{S^{\prime}}{S}\right)^{\prime} (49)
γz\displaystyle\gamma_{z}^{\prime} =R2αSSRR′′αSSRRαSS+RRα(SS)R2(SS)2+R2α2,\displaystyle=\frac{R^{\prime 2}\alpha\frac{S^{\prime}}{S}-R\,R^{\prime\prime}\alpha\frac{S^{\prime}}{S}-R\,R^{\prime}\alpha^{\prime}\frac{S^{\prime}}{S}+R\,R^{\prime}\alpha\left(\frac{S^{\prime}}{S}\right)^{\prime}}{R^{2}\left(\frac{S^{\prime}}{S}\right)^{2}+R^{\prime 2}\alpha^{2}}~{}, (50)

and this can be re-expressed in terms of ζzw\zeta_{zw}^{\prime},

γzsec2γz\displaystyle\gamma_{z}^{\prime}\sec^{2}\gamma_{z} =γz(1+tan2γz)=ζzwα2+RR′′R2α2ζzw+2RαRα3ζzwRRα2ζzw′′\displaystyle=\gamma_{z}^{\prime}(1+\tan^{2}\gamma_{z})=-\frac{\zeta_{zw}^{\prime}}{\alpha^{2}}+\frac{R\,R^{\prime\prime}}{R^{\prime 2}\alpha^{2}}\zeta_{zw}^{\prime}+2\frac{R\,\alpha^{\prime}}{R^{\prime}\alpha^{3}}\zeta_{zw}^{\prime}-\frac{R}{R^{\prime}\alpha^{2}}\zeta_{zw}^{\prime\prime} (51)
γz\displaystyle\gamma_{z}^{\prime} =R2α2ζzw+RR′′α2ζzw+2RRααζzwRRα2ζzw′′R2ζzw2+R2α4.\displaystyle=\frac{-R^{\prime 2}\alpha^{2}\zeta_{zw}^{\prime}+R\,R^{\prime\prime}\alpha^{2}\zeta_{zw}^{\prime}+2R\,R^{\prime}\alpha\,\alpha^{\prime}\zeta_{zw}^{\prime}-R\,R^{\prime}\alpha^{2}\zeta_{zw}^{\prime\prime}}{R^{2}\zeta_{zw}^{\prime 2}+R^{\prime 2}\alpha^{4}}~{}. (52)

Locally about any point, the line of centres can be approximated as following a section of a circle. The radius of this circle is determined by dividing the length traversed in a small span by the corresponding change in angle δξ\delta\xi. We therefore need to express δξ\delta\xi in terms of path length along the line, rather than in terms of δr\delta r. The distance δl\delta l between the centre of shell rr and that of shell r+δrr+\delta r follows from the displacement components given in eqs (46a) and (46d):

δl\displaystyle\delta l =δrR2(SS)2+R2α2\displaystyle=\delta r\sqrt{R^{2}\left(\frac{S^{\prime}}{S}\right)^{2}+R^{\prime 2}\alpha^{2}} (53)

The local radius of curvature of the line of centres is then

ρzw\displaystyle\rho_{zw} =δlδξ\displaystyle=\frac{\delta l}{\delta\xi}
=[R2(SS)2+R2α2]3/2R2(αα3)SSRR′′αSSRRαSS+RRα(SS)R2α(SS)3\displaystyle=\frac{\left[R^{2}\left(\frac{S^{\prime}}{S}\right)^{2}+R^{\prime 2}\alpha^{2}\right]^{3/2}}{R^{\prime 2}(\alpha-\alpha^{3})\frac{S^{\prime}}{S}-R\,R^{\prime\prime}\alpha\frac{S^{\prime}}{S}-R\,R^{\prime}\alpha^{\prime}\frac{S^{\prime}}{S}+R\,R^{\prime}\alpha\left(\frac{S^{\prime}}{S}\right)^{\prime}-R^{2}\alpha\left(\frac{S^{\prime}}{S}\right)^{3}} (54)

The relationship between the two contributions, the rate of tilt γz\gamma_{z}^{\prime} and the rate of change of slant ζzw\zeta_{zw}^{\prime}, is somewhat complicated, but becomes much simpler near an extremum in RR. Starting from equation (51), replace RR^{\prime} by R2(rre)R_{2}(r-r_{e}) (where R2R_{2} is the value of R′′R^{\prime\prime} at rer_{e}), α\alpha by αerre\frac{\alpha_{e}}{r-r_{e}}, and α\alpha^{\prime} by αe(rre)2-\frac{\alpha_{e}}{(r-r_{e})^{2}}. This gives

γzsec2γz\displaystyle\gamma_{z}^{\prime}\sec^{2}\gamma_{z} =ζzwαe2(rre)2RR2αe2ζzwRR2αe2(rre)ζzw′′\displaystyle=-\frac{\zeta_{zw}^{\prime}}{\alpha_{e}^{2}}(r-r_{e})^{2}-\frac{R}{R_{2}\alpha_{e}^{2}}\zeta_{zw}^{\prime}-\frac{R}{R_{2}\alpha_{e}^{2}}(r-r_{e})\zeta_{zw}^{\prime\prime} (55)

Since by table 3.4 ζzw\zeta_{zw}^{\prime} approaches a constant at the spatial extremum, ζzw′′\zeta_{zw}^{\prime\prime} is small there, so we can drop the last term, as well as the first. The middle term dominates, and its sign depends only on R2R_{2} and ζzw\zeta_{zw}^{\prime}. Therefore, γz\gamma_{z}^{\prime} and ζzw\zeta_{zw}^{\prime} have the same sign near maxima, where R′′R^{\prime\prime} is negative, and opposite signs near minima, where R′′R^{\prime\prime} is positive. Consequently, the slant and tilt effects both increase the curvature of the line of centres near a spatial maximum, but oppose each other near a spatial minimum555 This was first observed in numerical output, which also indicates the tilt-rate is the larger contribution in determining the centre-line curvature..

4 Comparison of Rotations in PG & FR

In order to connect the shell rotations found in PG with the frame rotation effect found in FR, let us now set up the orthonormal basis of FR, within the 𝔼4\mathbb{E}^{4} of section 3.2. Since the basis orientation is time-independent, we will only look at spatial components. Thus there will be 3 vectors intrinsic to the embedded surface, and one perpendicular to it. We shall need to refer to 3 different fames; the Cartesian coordinates of 𝔼4\mathbb{E}^{4}, the Szekeres angular coordinates, and the orthonormal tetrad of the embedded surface. Our index convention is

i,j,k,\displaystyle i,j,k,\cdots~{}~{} Szekeres coordinatesr,θ,ϕ\displaystyle-~{}~{}\mbox{Szekeres coordinates}~{}r,\theta,\phi
s,u,v,\displaystyle s,u,v,\cdots~{}~{} 4-d flat coordinatesX,Y,Z,W\displaystyle-~{}~{}\mbox{4-d flat coordinates}~{}X,Y,Z,W (56)
(a),(b),(c),\displaystyle(a),(b),(c),\cdots~{}~{} ortho-normal basis indices(θ),(ϕ),(n),(N).\displaystyle-~{}~{}\mbox{ortho-normal basis indices}~{}(\theta),(\phi),(n),(N)~{}.

4.1 Orthonormal Basis

From (36), the mapping between (r,θ,ϕ)(r,\theta,\phi) and V=(X,Y,Z,W)V=(X,Y,Z,W) consists of

Vr\displaystyle\frac{\partial V}{\partial r} =AT(RU+R(Ω)TU+D),Vθ=ATRUθ,Vϕ=ATRUϕ,\displaystyle=A^{T}(R^{\prime}U+R(\Omega^{\prime})^{T}U+D^{\prime})~{},~{}~{}~{}~{}\frac{\partial V}{\partial\theta}=A^{T}RU_{\theta}~{},~{}~{}~{}~{}\frac{\partial V}{\partial\phi}=A^{T}RU_{\phi}~{}, (57)
Λis\displaystyle\to~{}~{}~{}~{}~{}~{}~{}~{}\Lambda^{s}_{i} =(X,Y,Z,W)(r,θ,ϕ)=(VrVθVϕ)\displaystyle=\frac{\partial(X,Y,Z,W)}{\partial(r,\theta,\phi)}=\begin{pmatrix}\displaystyle\frac{\partial V}{\partial r}&\displaystyle\frac{\partial V}{\partial\theta}&\displaystyle\frac{\partial V}{\partial\phi}\end{pmatrix} (58)

which also constitute vectors in the 3-surface along the rr, θ\theta & ϕ\phi directions. Thus one may easily find a vector orthogonal to that 3-surface,

N¯\displaystyle\overline{N} =AT(αsinθcosϕαsinθsinϕαcosθ1),\displaystyle=A^{T}\begin{pmatrix}\alpha\sin\theta\cos\phi\\ \alpha\sin\theta\sin\phi\\ \alpha\cos\theta\\ -1\end{pmatrix}~{}, (59)

and consequently a third surface vector orthogonal to the θ\theta and ϕ\phi directions (as well as N¯\overline{N}) is

n¯\displaystyle\overline{n} =AT(sinθcosϕsinθsinϕcosθα).\displaystyle=A^{T}\begin{pmatrix}\sin\theta\cos\phi\\ \sin\theta\sin\phi\\ \cos\theta\\ \alpha\end{pmatrix}~{}. (60)

Normalising these, we obtain an orthonormal basis and its dual, with components in 𝔼4\mathbb{E}^{4}; the components of e(c)\mbox{\rm e}^{(c)} are in the columns of (61), and the basis order is (θ),(ϕ),(n),(N)(\theta),(\phi),(n),(N),

eu(c)\displaystyle e_{u}{}^{(c)} =AT(cosθcosϕsinϕ1+fsinθcosϕfsinθcosϕcosθsinϕcosϕ1+fsinθsinϕfsinθsinϕsinθ01+fcosθfcosθ00f1+f)=ATe¯u,(c)\displaystyle=A^{T}\begin{pmatrix}\cos\theta\cos\phi&-\sin\phi&\sqrt{1+f}\;\sin\theta\cos\phi&\sqrt{-f}\;\sin\theta\cos\phi\\ \cos\theta\sin\phi&\cos\phi&\sqrt{1+f}\;\sin\theta\sin\phi&\sqrt{-f}\;\sin\theta\sin\phi\\ -\sin\theta&0&\sqrt{1+f}\;\cos\theta&\sqrt{-f}\;\cos\theta\\ 0&0&\sqrt{-f}\;&-\sqrt{1+f}\;\end{pmatrix}=A^{T}\overline{e}_{u}{}^{(c)}~{}, (61)
e(b)s\displaystyle e_{(b)}{}^{s} =(cosθcosϕcosθsinϕsinθ0sinϕcosϕ001+fsinθcosϕ1+fsinθsinϕ1+fcosθffsinθcosϕfsinθsinϕfcosθ1+f)A=e¯(b)As.\displaystyle=\begin{pmatrix}\cos\theta\cos\phi&\cos\theta\sin\phi&-\sin\theta&0\\ -\sin\phi&\cos\phi&0&0\\ \sqrt{1+f}\;\sin\theta\cos\phi&\sqrt{1+f}\;\sin\theta\sin\phi&\sqrt{1+f}\;\cos\theta&\sqrt{-f}\;\\ \sqrt{-f}\;\sin\theta\cos\phi&\sqrt{-f}\;\sin\theta\sin\phi&\sqrt{-f}\;\cos\theta&-\sqrt{1+f}\;\end{pmatrix}A=\overline{e}_{(b)}{}^{s}A~{}. (62)

Equation (62) gives the flat-space components of e(b)\mbox{\rm e}_{(b)} in 𝔼4\mathbb{E}^{4}.

4.2 Variation of the Embedded Basis

Consider a path parametrised by λ\lambda, within the embedded 3-surface, which is also a 3-space of constant time in the Szekeres metric, so that r=r(λ)r=r(\lambda), θ=θ(λ)\theta=\theta(\lambda), ϕ=ϕ(λ)\phi=\phi(\lambda). The tangent vector is vj=dxj/dλv^{j}={\rm d}x^{j}/{\rm d}\lambda, and the path in 𝔼4\mathbb{E}^{4} is V=V(r(λ),θ(λ),ϕ(λ))V=V(r(\lambda),\theta(\lambda),\phi(\lambda)). Along this path, the variation of the flat space basis vector e(b)\mbox{\rm e}_{(b)} within 𝔼4\mathbb{E}^{4} is

𝐯e(b)\displaystyle\nabla_{\mathbf{v}}\mbox{\rm e}_{(b)} =vses(e(b)euu)=vs(e(b)euu,s+e(b)esueu)=vse(b)euu,s,\displaystyle=v^{s}\,\nabla_{\mbox{\rm e}_{s}}\big{(}e_{(b)}{}^{u}\mbox{\rm e}_{u}\big{)}=v^{s}\big{(}e_{(b)}{}^{u}{}_{,s}\,\mbox{\rm e}_{u}+e_{(b)}{}^{u}\nabla_{\mbox{\rm e}_{s}}\,\mbox{\rm e}_{u}\big{)}=v^{s}\,e_{(b)}{}^{u}{}_{,s}\,\mbox{\rm e}_{u}~{}, (63)

so that the frame rotation matrix of FR is (see eq (21) of that paper)

𝒱(c)(b)\displaystyle{\cal V}^{(c)}{}_{(b)} =(𝐯e(b))(e(c))=(vse(b)euu,s)(evev(c))=vse(b)euu,s(c)\displaystyle=\big{(}\nabla_{\mathbf{v}}\,\mbox{\rm e}_{(b)}\big{)}(\mbox{\rm e}^{(c)})=\big{(}v^{s}\,e_{(b)}{}^{u}{}_{,s}\,\mbox{\rm e}_{u}\big{)}\big{(}e_{v}{}^{(c)}\,\mbox{\rm e}^{v}\big{)}=v^{s}\,e_{(b)}{}^{u}{}_{,s}\,e_{u}{}^{(c)}
=viΛise(b)euu,s=(c)vie(b)euu,i.(c)\displaystyle=v^{i}\,\Lambda^{s}_{i}\,e_{(b)}{}^{u}{}_{,s}\,e_{u}{}^{(c)}=v^{i}\,e_{(b)}{}^{u}{}_{,i}\,e_{u}{}^{(c)}~{}. (64)

We have

e(b),ru=e¯(b)Au+e¯(b)Au,r=(e¯(b)Ωu+e¯(b))u,rAe(b),θu=e¯(b)Au,θ,e(b)=u,ϕe¯(b)Au,ϕ,\displaystyle\begin{aligned} e_{(b)}{}^{u}{}_{,r}&=\overline{e}_{(b)}{}^{u}\,A^{\prime}+\overline{e}_{(b)}{}^{u}{}_{,r}\,A=\big{(}\overline{e}_{(b)}{}^{u}\,\Omega^{\prime}+\overline{e}_{(b)}{}^{u}{}_{,r}\big{)}A\\ e_{(b)}{}^{u}{}_{,\theta}&=\overline{e}_{(b)}{}^{u}{}_{,\theta}\,A~{},~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}e_{(b)}{}^{u}{}_{,\phi}=\overline{e}_{(b)}{}^{u}{}_{,\phi}\,A~{},\end{aligned} (65)

so that

𝒱(c)=(b)vie(b)euu,i(c)\displaystyle{\cal V}^{(c)}{}_{(b)}=v^{i}\,e_{(b)}{}^{u}{}_{,i}\,e_{u}{}^{(c)} ={r˙(e¯(b)Ωu+e¯(b))u,r+θ˙e¯(b)+u,θϕ˙e¯(b)}u,ϕAATe¯u(c)\displaystyle=\big{\{}\dot{r}\big{(}\overline{e}_{(b)}{}^{u}\,\Omega^{\prime}+\overline{e}_{(b)}{}^{u}{}_{,r}\big{)}+\dot{\theta}\,\overline{e}_{(b)}{}^{u}{}_{,\theta}+\dot{\phi}\,\overline{e}_{(b)}{}^{u}{}_{,\phi}\big{\}}A\,A^{T}\,\overline{e}_{u}{}^{(c)}
={r˙(e¯(b)Ωu+e¯(b))u,r+θ˙e¯(b)+u,θϕ˙e¯(b)}u,ϕe¯u.(c)\displaystyle=\big{\{}\dot{r}\big{(}\overline{e}_{(b)}{}^{u}\,\Omega^{\prime}+\overline{e}_{(b)}{}^{u}{}_{,r}\big{)}+\dot{\theta}\,\overline{e}_{(b)}{}^{u}{}_{,\theta}+\dot{\phi}\,\overline{e}_{(b)}{}^{u}{}_{,\phi}\big{\}}\overline{e}_{u}{}^{(c)}~{}. (66)

The basis derivatives with respect to Szekeres angular coordinates are

e¯(b),rs\displaystyle\overline{e}_{(b)}{}^{s}{}_{,r} =f2(00000000sinθcosϕ1+fsinθsinϕ1+fcosθ1+f1fsinθcosϕfsinθsinϕfcosθf11+f),\displaystyle=\frac{f^{\prime}}{2}\begin{pmatrix}0&0&0&0\\ 0&0&0&0\\ \dfrac{\sin\theta\cos\phi}{\sqrt{1+f}\;}&\dfrac{\sin\theta\sin\phi}{\sqrt{1+f}\;}&\dfrac{\cos\theta}{\sqrt{1+f}\;}&\dfrac{-1}{\sqrt{-f}\;}\\[8.53581pt] \dfrac{-\sin\theta\cos\phi}{\sqrt{-f}\;}&\dfrac{-\sin\theta\sin\phi}{\sqrt{-f}\;}&\dfrac{-\cos\theta}{\sqrt{-f}\;}&\dfrac{-1}{\sqrt{1+f}\;}\end{pmatrix}~{}, (67a)
e¯(b),θs\displaystyle\overline{e}_{(b)}{}^{s}{}_{,\theta} =(sinθcosϕsinθsinϕcosθ000001+fcosθcosϕ1+fcosθsinϕ1+fsinθ0fcosθcosϕfcosθsinϕfsinθ0),\displaystyle=\begin{pmatrix}-\sin\theta\cos\phi&-\sin\theta\sin\phi&-\cos\theta&0\\ 0&0&0&0\\ \sqrt{1+f}\;\cos\theta\cos\phi&\sqrt{1+f}\;\cos\theta\sin\phi&-\sqrt{1+f}\;\sin\theta&0\\ \sqrt{-f}\;\cos\theta\cos\phi&\sqrt{-f}\;\cos\theta\sin\phi&-\sqrt{-f}\;\sin\theta&0\end{pmatrix}~{}, (67b)
e¯(b),ϕs\displaystyle\overline{e}_{(b)}{}^{s}{}_{,\phi} =(cosθsinϕcosθcosϕ00cosϕsinϕ001+fsinθsinϕ1+fsinθcosϕ00fsinθsinϕfsinθcosϕ00).\displaystyle=\begin{pmatrix}-\cos\theta\sin\phi&\cos\theta\cos\phi&0&0\\ -\cos\phi&-\sin\phi&0&0\\ -\sqrt{1+f}\;\sin\theta\sin\phi&\sqrt{1+f}\;\sin\theta\cos\phi&0&0\\ -\sqrt{-f}\;\sin\theta\sin\phi&\sqrt{-f}\;\sin\theta\cos\phi&0&0\end{pmatrix}~{}. (67c)

Using eqs (67a)-(67c) and (61)-(62) in (66) above, we find that

𝒱(θ)(n)\displaystyle{\cal V}^{(\theta)}{}_{(n)} =fSsinθ[(1+f)fcosθ]{Pcosϕ+Qsinϕ}vr1+fS+1+fvθ,\displaystyle=\dfrac{-fS^{\prime}\sin\theta-[(1+f)-f\cos\theta]\{P^{\prime}\cos\phi+Q^{\prime}\sin\phi\}v^{r}}{\sqrt{1+f}\;S}+\sqrt{1+f}\;v^{\theta}~{}, (68a)
𝒱(ϕ)(n)\displaystyle{\cal V}^{(\phi)}{}_{(n)} =[1(1+f)(1cosθ)]{PsinϕQcosϕ}vr1+fS+1+fsinθvϕ,\displaystyle=\dfrac{[1-(1+f)(1-\cos\theta)]\{P^{\prime}\sin\phi-Q^{\prime}\cos\phi\}v^{r}}{\sqrt{1+f}\;S}+\sqrt{1+f}\;\sin\theta v^{\phi}~{}, (68b)
𝒱(ϕ)(θ)\displaystyle{\cal V}^{(\phi)}{}_{(\theta)} =(PsinϕQcosϕ)sinθSvr+cosθvϕ.\displaystyle=\dfrac{-(P^{\prime}\sin\phi-Q^{\prime}\cos\phi)\sin\theta}{S}v^{r}+\cos\theta v^{\phi}~{}. (68c)

Eqs (68a)-(68c) agree with FR(25)-(27), confirming that the frame rotation effects found in [15] are fully consistent with, and therefore explained by, the shell rotations and tilts uncovered in [6] & [7].

5 Toroidal & Rotating Embeddings

As an illustration of the rotations and tilts described in PG & FR, it would be interesting to see if one can define a Szekeres model whose embedding ‘naturally’ bends round and closes on itself, i.e. the embedded surface has the topology of a torus in the 4-d flat space, without any arbitrary identifications. It doesn’t have to be a Datt-Kantowski-Sachs (DKS) type model [8, 19], it could be a quasi-spherical model that has both a spatial maximum and a minimum; or multiple spatial maxima & minima. Of course there is no physical significance to the embedding of a spacetime666… unless it’s a brane., and the shape of the embedded surface depends on the space it is embedded into. The point here is to illustrate that the tilt can be continuously in the same sense.

Where spatial extrema occur, the conditions for no shell crossings or surface layers [16, 14] require that f=1f=-1, all 6 arbitrary functions have zero derivative, 0=M=f=a=S=P=Q0=M^{\prime}=f^{\prime}=a^{\prime}=S^{\prime}=P^{\prime}=Q^{\prime}, and RR^{\prime}, MM^{\prime}, α\alpha must change sign together.

In order to achieve this, we require 3 things as rr runs from rir_{i} to rfr_{f}: (i) the tilt/rotation matrix A(r)A(r) must run round 2π2\pi, relative to some ‘axis’, and return to the identity; (ii) the locus of centres Δ(r)\Delta(r) must form a loop; (iii) the areal radius R(r)R(r) and its derivative R(r)R^{\prime}(r) must return to their starting values, so that the join is smooth — for example RR could be (multiply) periodic in rr around this loop — and this should hold at each constant tt; (iv) ideally the 3-surface should not intersect itself in the embedding, and there should be no shell crossings.

5.1 Embedding DEs

The matrix DEs of (31) actually separate out into 4 identical sets of 4 linked DEs, but with different initial conditions,

A(r)\displaystyle A(r) =(ν1(r)ν2(r)ν3(r)ν4(r)χ1(r)χ2(r)χ3(r)χ4(r)λ1(r)λ2(r)λ3(r)λ4(r)σ1(r)σ2(r)σ3(r)σ4(r)),A(0)=I,\displaystyle=\begin{pmatrix}\nu_{1}(r)&\nu_{2}(r)&\nu_{3}(r)&\nu_{4}(r)\\ \chi_{1}(r)&\chi_{2}(r)&\chi_{3}(r)&\chi_{4}(r)\\ \lambda_{1}(r)&\lambda_{2}(r)&\lambda_{3}(r)&\lambda_{4}(r)\\ \sigma_{1}(r)&\sigma_{2}(r)&\sigma_{3}(r)&\sigma_{4}(r)\end{pmatrix}~{},~{}~{}~{}~{}~{}~{}A(0)=I~{}, (69a)
νi\displaystyle\nu_{i}^{\prime} =PS(λi+ασi),χi=QS(λi+ασi),\displaystyle=\frac{P^{\prime}}{S}(\lambda_{i}+\alpha\sigma_{i})~{},~{}~{}~{}~{}\chi_{i}^{\prime}=\frac{Q^{\prime}}{S}(\lambda_{i}+\alpha\sigma_{i})~{},
λi\displaystyle\lambda_{i}^{\prime} =PνiQχi+SασiS,σi=α(Pνi+Qχi+Sλi)S,i=1,2,3,4;\displaystyle=\frac{-P^{\prime}\nu_{i}-Q^{\prime}\chi_{i}+S^{\prime}\alpha\sigma_{i}}{S}~{},~{}~{}~{}~{}\sigma_{i}^{\prime}=-\frac{\alpha(P^{\prime}\nu_{i}+Q^{\prime}\chi_{i}+S^{\prime}\lambda_{i})}{S}~{},~{}~{}~{}~{}i=1,2,3,4~{}; (69b)
ν1(0)\displaystyle\nu_{1}(0) =1,χ1(0)=0,λ1(0)=0,σ1(0)=0,\displaystyle=1~{},~{}~{}~{}\chi_{1}(0)=0~{},~{}~{}~{}\lambda_{1}(0)=0~{},~{}~{}~{}\sigma_{1}(0)=0~{}, (69c)
ν2(0)\displaystyle\nu_{2}(0) =0,χ2(0)=1,λ2(0)=0,σ2(0)=0,\displaystyle=0~{},~{}~{}~{}\chi_{2}(0)=1~{},~{}~{}~{}\lambda_{2}(0)=0~{},~{}~{}~{}\sigma_{2}(0)=0~{}, (69d)
ν3(0)\displaystyle\nu_{3}(0) =0,χ3(0)=0,λ3(0)=1,σ3(0)=0,\displaystyle=0~{},~{}~{}~{}\chi_{3}(0)=0~{},~{}~{}~{}\lambda_{3}(0)=1~{},~{}~{}~{}\sigma_{3}(0)=0~{}, (69e)
ν4(0)\displaystyle\nu_{4}(0) =0,χ4(0)=0,λ4(0)=0,σ4(0)=1.\displaystyle=0~{},~{}~{}~{}\chi_{4}(0)=0~{},~{}~{}~{}\lambda_{4}(0)=0~{},~{}~{}~{}\sigma_{4}(0)=1~{}. (69f)

Similarly, from (32), the initial value problem (IVP) for the line of shell centres separates out into the same groups,

Δ(r)\displaystyle\Delta(r) =(XCYCZCWC),Δ(0)=0,\displaystyle=\begin{pmatrix}X_{C}\\ Y_{C}\\ Z_{C}\\ W_{C}\end{pmatrix}~{},~{}~{}~{}~{}~{}~{}\Delta(0)=0~{}, (70a)
(Δi)\displaystyle(\Delta^{i})^{\prime} =RS(Pνi+Qχi+Sλi)+Rασi,i=1,2,3,4,\displaystyle=\frac{R}{S}(P^{\prime}\nu_{i}+Q^{\prime}\chi_{i}+S^{\prime}\lambda_{i})+R^{\prime}\alpha\sigma_{i}~{},~{}~{}~{}~{}i=1,2,3,4~{}, (70b)

making 4 identical sets of 5 DEs.

5.2 Case With Only SS Varying

Let’s take the simple case of P=0=QP^{\prime}=0=Q^{\prime}, while ff, MM, aa, SS are general.
(i) Then by (31)

A(r)\displaystyle A^{\prime}(r) =Ω(r)A(r)=(00000000000SSα00SSα0)A(r)\displaystyle=\Omega^{\prime}(r)A(r)=\begin{pmatrix}0&0&0&0\\[5.69054pt] 0&0&0&0\\[5.69054pt] 0&0&0&\dfrac{S^{\prime}}{S}\alpha\\[5.69054pt] 0&0&-\dfrac{S^{\prime}}{S}\alpha&0\end{pmatrix}A(r) (71)

which integrates up to

A\displaystyle A =(1000010000cosζsinζ00sinζcosζ),ζ(r)=rirSαSdr.\displaystyle=\begin{pmatrix}1&0&0&0\\[5.69054pt] 0&1&0&0\\[5.69054pt] 0&0&\cos\zeta&\sin\zeta\\[5.69054pt] 0&0&-\sin\zeta&\cos\zeta\end{pmatrix}~{},~{}~{}~{}~{}~{}~{}\zeta(r)=\int_{r_{i}}^{r}\frac{S^{\prime}\alpha}{S}\,{\rm d}r~{}. (72)

Then from (72) and (23) we have

f=S2ζ2(S2ζ2+S2)=1(1+S2S2ζ2),f=1S2=0,ζ0,f=faS2=(1fa)S2ζ2.\displaystyle\begin{aligned} f&=\frac{-S^{2}\zeta^{\prime 2}}{(S^{2}\zeta^{\prime 2}+S^{\prime 2})}=\frac{-1}{\left(1+\dfrac{S^{\prime 2}}{S^{2}\zeta^{\prime 2}}\right)}~{},\\ f&=-1~{}~{}~{}~{}\to~{}~{}~{}~{}S^{\prime 2}=0~{},~{}~{}~{}~{}\zeta^{\prime}\neq 0~{},\\ f&=-f_{a}~{}~{}~{}~{}\to~{}~{}~{}~{}S^{\prime 2}=(1-f_{a})S^{2}\zeta^{\prime 2}~{}.\end{aligned} (73)

One may thus obtain all of f(r)f(r), α(r)\alpha(r), S(r)S(r) or ζ(r)\zeta(r) from specifying just two of them. It should be fairly easy to make ζ\zeta run from 0 to 2π2\pi, because it does not depend on time through RR or RR^{\prime}. We show below that ff and hence α\alpha will be oscillatory, and we note that α\alpha diverges where ff goes to 1-1, so S=0S^{\prime}=0 will be needed here. Thus Sα/SS^{\prime}\alpha/S needs to be non-negative, which means SS^{\prime} changes sign with α\alpha. Possible functional forms for ζ(r)\zeta(r), S(r)S(r), f(r)f(r), and α(r)\alpha(r) will be considered below.

(ii) Next by integrating (32), and requiring that the line of centres closes up, we find

Δ\displaystyle\Delta^{\prime} =ATD=AT(00RSSRα),\displaystyle=A^{T}D^{\prime}=A^{T}\begin{pmatrix}0\\[2.84526pt] 0\\[2.84526pt] R\dfrac{S^{\prime}}{S}\\[8.53581pt] R^{\prime}\alpha\end{pmatrix}~{}, (74)
rirfΔdr\displaystyle\int_{r_{i}}^{r_{f}}\Delta^{\prime}\,{\rm d}r =0=rirf(00cosζRSSsinζRαsinζRSS+cosζRα)dr.\displaystyle=0=\int_{r_{i}}^{r_{f}}\begin{pmatrix}0\\[2.84526pt] 0\\[2.84526pt] \cos\zeta R\dfrac{S^{\prime}}{S}-\sin\zeta R^{\prime}\alpha\\[8.53581pt] \sin\zeta R\dfrac{S^{\prime}}{S}+\cos\zeta R^{\prime}\alpha\end{pmatrix}{\rm d}r~{}. (75)

Generically, RR & RR^{\prime} don’t have the same time dependence, so, in order for this to be true at all times, we attempt to arrange that

rirfcosζRSSdr=0=rirfsinζRαdr,\displaystyle\int_{r_{i}}^{r_{f}}\cos\zeta R\dfrac{S^{\prime}}{S}\,{\rm d}r=0=\int_{r_{i}}^{r_{f}}\sin\zeta R^{\prime}\alpha\,{\rm d}r~{}, (76a)
rirfsinζRSSdr=0=rirfcosζRαdr.\displaystyle\int_{r_{i}}^{r_{f}}\sin\zeta R\dfrac{S^{\prime}}{S}\,{\rm d}r=0=\int_{r_{i}}^{r_{f}}\cos\zeta R^{\prime}\alpha\,{\rm d}r~{}. (76b)

In particular, if within 0ζπ0\leq\zeta\leq\pi, one can arrange that RR goes max-to-min-to-max (or min-to-max-to-min), in a manner that’s symmetric about ζ=π/2\zeta=\pi/2, then, however the time evolution goes, 2 copies of this should join up nicely. Similarly, if within 0ζπ/20\leq\zeta\leq\pi/2, one can arrange that RR goes max-to-min-to-max (or min-to-max-to-min), symmetrically about ζ=π/4\zeta=\pi/4, then 4 copies of this should also join up nicely. And so on.

(iii) To make RR & RR^{\prime} join nicely, so that the torus ‘tube’ joins itself smoothly, we could choose ff, MM & aa periodic; and of course f=1f=-1 is needed at the extrema, so ff must oscillate twice as fast.

(iv) Once a detailed model has been chosen, it can be checked for shell crossings and self intersections, and adjustments can be made as needed.

5.3 Case With Only PP Varying

Next we consider the case S=0=QS^{\prime}=0=Q^{\prime} (& general ff, MM, aa, PP). Then by (69) & (70), the IVP becomes

νi\displaystyle\nu_{i}^{\prime} =PS(λi+ασi),λi=PSνi,σi=PαSνi,i=1,2,3,4;\displaystyle=\frac{P^{\prime}}{S}(\lambda_{i}+\alpha\sigma_{i})~{},~{}~{}~{}~{}\lambda_{i}^{\prime}=-\frac{P^{\prime}}{S}\nu_{i}~{},~{}~{}~{}~{}\sigma_{i}^{\prime}=-\frac{P^{\prime}\alpha}{S}\nu_{i}~{},~{}~{}~{}~{}i=1,2,3,4~{}; (77a)
ν1(0)\displaystyle\nu_{1}(0) =1,λ1(0)=0,σ1(0)=0,\displaystyle=1~{},~{}~{}~{}\lambda_{1}(0)=0~{},~{}~{}~{}\sigma_{1}(0)=0~{}, (77b)
ν2(0)\displaystyle\nu_{2}(0) =0,λ2(0)=0,σ2(0)=0,\displaystyle=0~{},~{}~{}~{}\lambda_{2}(0)=0~{},~{}~{}~{}\sigma_{2}(0)=0~{}, (77c)
ν3(0)\displaystyle\nu_{3}(0) =0,λ3(0)=1,σ3(0)=0,\displaystyle=0~{},~{}~{}~{}\lambda_{3}(0)=1~{},~{}~{}~{}\sigma_{3}(0)=0~{}, (77d)
ν4(0)\displaystyle\nu_{4}(0) =0,λ4(0)=0,σ4(0)=1,\displaystyle=0~{},~{}~{}~{}\lambda_{4}(0)=0~{},~{}~{}~{}\sigma_{4}(0)=1~{}, (77e)
(Δi)\displaystyle(\Delta^{i})^{\prime} =νiRPS+σiRα,Δ(0)=0.\displaystyle=\nu_{i}\frac{RP^{\prime}}{S}+\sigma_{i}R^{\prime}\alpha~{},~{}~{}~{}~{}~{}~{}\Delta(0)=0~{}. (77f)

Clearly χi=0=ν2=λ2=σ2=YC\chi_{i}=0=\nu_{2}=\lambda_{2}=\sigma_{2}=Y_{C} for all rr.

Cyclic choices for the arbitrary functions similar to those above should again ensure closure.

5.4 Model 1, SS Only

We choose ζ\zeta to be uniformly increasing, satisfying (i) by construction, we fix P=0=QP=0=Q, and we let SS oscillate,

ζ\displaystyle\zeta =μr,\displaystyle=\mu r~{}, (78)
S\displaystyle S =S0+S1{1cos(nμr)},n,\displaystyle=S_{0}+S_{1}\big{\{}1-\cos(n\mu r)\big{\}}~{},~{}~{}~{}~{}~{}~{}n\in{\mathbb{N}}~{}, (79)

in which case, (72), (23) and (73) give777We could choose α\alpha to be the negative of the r.h.s. of (81), which would merely reflect the embedding in the W=0W=0 plane.

f\displaystyle f =11+n2S12sin2(nμr)(S0+S1{1cos(nμr)})2,\displaystyle=\frac{-1}{1+\dfrac{n^{2}S_{1}^{2}\sin^{2}(n\mu r)}{\big{(}S_{0}+S_{1}\big{\{}1-\cos(n\mu r)\big{\}}\big{)}^{2}}}~{}, (80)
α\displaystyle\to~{}~{}~{}~{}~{}~{}~{}~{}\alpha =S0S1{1cos(nμr)}nS1sin(nμr),\displaystyle=\frac{S_{0}-S_{1}\big{\{}1-\cos(n\mu r)\big{\}}}{nS_{1}\sin(n\mu r)}~{}, (81)

and the maxima of ff are at

cos(nμr)=S1S0+S1fm=11+n2S12S0(S0+2S1).\displaystyle\cos(n\mu r)=\frac{S_{1}}{S_{0}+S_{1}}~{}~{}~{}~{}\to~{}~{}~{}~{}f_{m}=\frac{-1}{1+\dfrac{n^{2}S_{1}^{2}}{S_{0}(S_{0}+2S_{1})}}~{}. (82)

For the mass and bang time we choose

M\displaystyle M =M0+M1{1cos(nμr)},a=a0a1{1cos(nμr)},\displaystyle=M_{0}+M_{1}\big{\{}1-\cos(n\mu r)\big{\}}~{},~{}~{}~{}~{}~{}~{}a=a_{0}-a_{1}\big{\{}1-\cos(n\mu r)\big{\}}~{}, (83)

in accordance with requirement (iii).

The relevant no-shell-crossing requirements are that a-a^{\prime} and a+2πTa^{\prime}+2\pi T^{\prime} have the same sign as MM^{\prime}, and that (E/E)m|M/(3M)|(E^{\prime}/E)_{m}\leq\big{|}M^{\prime}/(3M)\big{|}. The function ff, which appears in the denominator of TT, defined by eq (5), oscillates twice as fast as MM does. Thus the amplitude of ff’s variation in eq (80) needs to be small. For the model considered here, this means S1S_{1} should be small, which in turn means SS does not vary much.

Now the calculation of R(r)R(r) and R(r)R^{\prime}(r) on a constant time slice is a numerical exercise; the tt equation of (4) has to be solved to get η\eta at each rr. But, using the parametric solution (4) with zero Λ\Lambda, we can instead integrate Δ\Delta^{\prime} on surfaces of constant η\eta; if the result is zero for every constant-η\eta surface, then it will be zero for every constant-tt surface also. Using constant η\eta surfaces has the additional advantage that the bang and crunch singularities are avoided. The integrals in (76) are therefore modified to become

rirfcosζRSSdr\displaystyle\int_{r_{i}}^{r_{f}}\cos\zeta R\dfrac{S^{\prime}}{S}\,{\rm d}r =(1cosη)rirfcos[rirSαSdr]MS(f)Sdr,\displaystyle=(1-\cos\eta)\int_{r_{i}}^{r_{f}}\cos\left[\int_{r_{i}}^{r}\frac{S^{\prime}\alpha}{S}\,{\rm d}r\right]\frac{MS^{\prime}}{(-f)S}\,{\rm d}r~{}, (84a)
rirfcosζRαdr\displaystyle\int_{r_{i}}^{r_{f}}\cos\zeta R^{\prime}\alpha\,{\rm d}r =(1ϕ1)(1cosη)rirfcos[rirSαSdr]Mα(f)dr\displaystyle=(1-\phi_{1})(1-\cos\eta)\int_{r_{i}}^{r_{f}}\cos\left[\int_{r_{i}}^{r}\frac{S^{\prime}\alpha}{S}\,{\rm d}r\right]\frac{M^{\prime}\alpha}{(-f)}\,{\rm d}r
(32ϕ11)(1cosη)rirfcos[rirSαSdr]fMαf2dr\displaystyle~{}~{}~{}~{}-\left(\frac{3}{2}\phi_{1}-1\right)(1-\cos\eta)\int_{r_{i}}^{r_{f}}\cos\left[\int_{r_{i}}^{r}\frac{S^{\prime}\alpha}{S}\,{\rm d}r\right]\frac{f^{\prime}M\alpha}{f^{2}}\,{\rm d}r
ϕ2(1cosη)rirfcos[rirSαSdr](f)1/2aαdr,\displaystyle~{}~{}~{}~{}-\phi_{2}(1-\cos\eta)\int_{r_{i}}^{r_{f}}\cos\left[\int_{r_{i}}^{r}\frac{S^{\prime}\alpha}{S}\,{\rm d}r\right](-f)^{1/2}a^{\prime}\alpha\,{\rm d}r~{}, (84b)

with obvious variations for the other two. By symmetry arguments, the 4 integrals of (76) clearly evaluate to zero when the above choices are made, ensuring that (ii) is satisfied. See fig 5.4 for a sample plot of one of the terms in (84).

[Uncaptioned image] Fig 3.   The integrand cosζ(Mfα/f2)(3ϕ1/21)(1cosη)\cos\zeta(Mf^{\prime}\alpha/f^{2})(3\phi_{1}/2-1)(1-\cos\eta) of (84) at η=π/3\eta=\pi/3, for the functions and parameter values given in section 5.4 and also used in fig 5.4.

A particular example satisfying all requirements is plotted in fig 5.4, for the parameter times η=π/3\eta=\pi/3 and η=5π/3\eta=5\pi/3. The parameter values are n=2n=2, μ=π\mu=\pi, ri=1r_{i}=-1, rf=1r_{f}=1, S0=1S_{0}=1, S1=0.1S_{1}=0.1, M0=0.1M_{0}=0.1, M1=0.05M_{1}=0.05, a0=0a_{0}=0, a1=0.1a_{1}=0.1. The no-shell-crossing conditions [18, 16] that are applicable here are (a)/M0(-a^{\prime})/M^{\prime}\geq 0, (a+2πT)/M0(a^{\prime}+2\pi T^{\prime})/M^{\prime}\geq 0, (E/E)m|M/(3M)|(E^{\prime}/E)_{m}\leq\big{|}M^{\prime}/(3M)\big{|}; and it has been checked that the chosen functions and parameter values satisfy them, though not by much. The construction used here puts strong limits on the variation of SS.

[Uncaptioned image]      [Uncaptioned image]      [Uncaptioned image] Fig 4.   An example of an embedded Szekeres model with a ‘natural’ torus topology as described in section 5. The path of the sphere centres (red), and a selection of sphere diameters (blue), are shown in the (Z,W)(Z,W) plane. Each diameter represents a complete 2-sphere, and the sequence of 2-spheres describes an embedded 3-surface in the flat 4-d (X,Y,Z,W)(X,Y,Z,W) space. The arbitrary functions and parameter values of this model are listed in section 5.4. The left plot is for η=π/3\eta=\pi/3, the middle one for η=π\eta=\pi, and the right one for η=5π/3\eta=5\pi/3. These are not constant time plots, so they are indicative rather than precise.

5.5 Model 2, SS Only

This is a much wobblier version of the toroidal model, that has 3 lobes instead of 2. The key defining functions are

M(r)=M0+M1{1cos(nμ0r)},f(r)=1+f1{1cos(2nμ0r)},a(r)=0,ζ=μ0{1+μ1cos(nμ0r)},S/S=ζ/α,\displaystyle\begin{aligned} M(r)&=M_{0}+M_{1}\big{\{}1-\cos(n\mu_{0}r)\big{\}}~{},\\ f(r)&=-1+f_{1}\big{\{}1-\cos(2n\mu_{0}r)\big{\}}~{},\\ a(r)&=0~{},\\ \zeta^{\prime}&=\mu_{0}\big{\{}1+\mu_{1}\cos(n\mu_{0}r)\big{\}}~{},\\ S^{\prime}/S&=\zeta^{\prime}/\alpha~{},\end{aligned} (85)

from which we find

α=12f1sin2(nμ0r)2f1sin(nμ0r),ζ=μ0(r+μ1sin(nμ0r)nμ0)SS=2f1μ0sin(nμ0r)(1+μ1cos(nμ0r))12f1sin2(nμ0r)S=S0exp{μ112f1sin2(nμ0r)2f1n}[(12f1+4f1cos2(nμ0r))22f1cos(nμ0r)12f1sin2(nμ0r)]1/(2n)\displaystyle\begin{aligned} \alpha&=\frac{\sqrt{1-2f_{1}\sin^{2}(n\mu_{0}r)}\;}{\sqrt{2f_{1}}\;\sin(n\mu_{0}r)}~{},~{}~{}~{}~{}\zeta=\mu_{0}\left(r+\frac{\mu_{1}\sin(n\mu_{0}r)}{n\mu_{0}}\right)\\ \frac{S^{\prime}}{S}&=\frac{\sqrt{2f_{1}}\;\mu_{0}\sin(n\mu_{0}r)\big{(}1+\mu_{1}\cos(n\mu_{0}r)\big{)}}{\sqrt{1-2f_{1}\sin^{2}(n\mu_{0}r)}\;}\\ S&=S_{0}\exp\left\{\frac{-\mu_{1}\sqrt{1-2f_{1}\sin^{2}(n\mu_{0}r)}\;}{\sqrt{2f_{1}}\;n}\right\}\\ &~{}~{}~{}~{}\left[\frac{(1-2f_{1}+4f_{1}\cos^{2}(n\mu_{0}r))}{2\sqrt{2f_{1}}\;}-\cos(n\mu_{0}r)\sqrt{1-2f_{1}\sin^{2}(n\mu_{0}r)}\;\right]^{1/(2n)}\end{aligned} (86)

We can choose the value of  S0S_{0}  to make  S=1S=1  at  r=0r=0. For the plots in fig 5.5, the parameters are

M0=0.55,M1=0.7,f1=0.06,n=3,μ0=1,μ1=0.8,t=1.\displaystyle M_{0}=0.55~{},~{}~{}~{}~{}M_{1}=0.7~{},~{}~{}~{}~{}f_{1}=0.06~{},~{}~{}~{}~{}n=3~{},~{}~{}~{}~{}\mu_{0}=1~{},~{}~{}~{}~{}\mu_{1}=0.8~{},~{}~{}~{}~{}t=1~{}. (87)

[Uncaptioned image]      [Uncaptioned image] [Uncaptioned image]      [Uncaptioned image] Fig 5.   An embedded Szekeres torus model with 3 lobes, showing just its intersection with the (Z,W)(Z,W) plane. The red curve is the path of the sphere centres, and each black line is the diameter of a 2-sphere at a particular rr value. The arbitrary functions and parameter values of this model are listed in section 5.5. The times of the plots are t=0.02t=0.02, t=1t=1, t=3t=3, and t=5t=5.

What’s interesting here is that there are parts where the tilt is changing more rapidly and parts where it’s hardly changing. Although the effect found in section 3.5, that the dipole displacement and the tilt have opposing effects on the curvature of the path of centres near a spatial minimum, is evident here, in the models we tried, after shell crossings had been eliminated, the tilt curvature seems to dominate.

5.6 Model 3, PP Only

For this model, the only non-sphericity function we vary is PP. By [11] we expect the line of centres to be bent, and by section 2.5, we expect there to be shell rotation. It is defined by

M(r)=M0+M1{1cos(nμr)},f(r)=1+f1{1cos(2nμr)}=1+2f1sin2(2nμr),a(r)=0,S(r)=1,Q(r)=0,ζ=μr,P/S=ζ/α,α=12f1sin2(nμr)2f1sin(nμr),P=μ2f1sin(nμr)12f1sin(nμr)2,P(r)=12nln((12f1{12cos2(nμr)})22f1cos(nμr)12f1sin2(nμr)),M0=0.75,M1=0.25,f1=0.02,μ=1,n=6,t=1.\displaystyle\begin{aligned} M(r)&=M_{0}+M_{1}\big{\{}1-\cos(n\mu r)\big{\}}~{},\\ f(r)&=-1+f_{1}\big{\{}1-\cos(2n\mu r)\big{\}}=-1+2f_{1}\sin^{2}(2n\mu r)~{},\\ a(r)&=0~{},\\ S(r)&=1~{},~{}~{}~{}~{}~{}~{}Q(r)=0~{},\\ \zeta&=\mu r~{},\\ P^{\prime}/S&=\zeta^{\prime}/\alpha~{},\\ \to~{}~{}~{}~{}~{}~{}~{}~{}\alpha&=\frac{\sqrt{1-2f_{1}\sin^{2}(n\mu r)}\;}{\sqrt{2f_{1}}\;\sin(n\mu r)}~{},\\ P^{\prime}&=\frac{\mu\sqrt{2f_{1}}\;\sin(n\mu r)}{\sqrt{1-2f_{1}\sin(n\mu r)^{2}}\;}~{},\\ P(r)&=\frac{1}{2n}\ln\Bigg{(}\frac{(1-2f_{1}\{1-2\cos^{2}(n\mu r)\})}{2\sqrt{2f_{1}}}\\ &~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}-\cos(n\mu r)\sqrt{1-2f_{1}\sin^{2}(n\mu r)}\;\Bigg{)}~{},\\ M_{0}=0.75~{},~{}~{}~{}~{}M_{1}&=0.25~{},~{}~{}~{}~{}f_{1}=0.02~{},~{}~{}~{}~{}\mu=1~{},~{}~{}~{}~{}n=6~{},~{}~{}~{}~{}t=1~{}.\end{aligned} (88)

and is illustrated in fig 5.6.

[Uncaptioned image] [Uncaptioned image]      [Uncaptioned image] Fig 6.   Three views of a less symmetric embedded Szekeres torus model, in the (X,Z,W)(X,Z,W) 3-space, at time t=1t=1. The red curve is the path of the sphere centres, each blue circle is the outline of a 2-sphere at a particular rr value, and the green dots indicate the location of θ=0\theta=0 on the 2-sphere; the rotation of the (θ,ϕ)(\theta,\phi) coordinates is not very large in this model. The arbitrary functions and parameter values of this model are listed in section 5.6.

Apart from the toroidal topology, the line of centres no longer lies in a 2-plane, and the direction of the ‘north pole’ θ=0\theta=0, rotates between shells; however these variations are fairly small.

5.7 Model 4, PP Only

This model is not toroidal; it is a spatially closed model defined by

M(r)=sin3(μr){M0+M1sin(μr)},f(r)=sin2(μr),a(r)=πM(f)3/2,S(r)=1,Q(r)=0,P(r)=sin(μr){P0+P1sin(μr)},α=tan(μr),M0=1,M1=5,P0=1,P1=0.3,μ=π,η=8π/5.\displaystyle\begin{aligned} M(r)&=\sin^{3}(\mu r)\big{\{}M_{0}+M_{1}\sin(\mu r)\big{\}}~{},\\ f(r)&=-\sin^{2}(\mu r)~{},\\ a(r)&=\frac{-\pi M}{(-f)^{3/2}}~{},\\ S(r)&=1~{},~{}~{}~{}~{}~{}~{}Q(r)=0~{},\\ P(r)&=\sin(\mu r)\big{\{}P_{0}+P_{1}\sin(\mu r)\big{\}}~{},\\ \to~{}~{}~{}~{}~{}~{}~{}~{}\alpha&=\tan(\mu r)~{},\\ M_{0}=1~{},~{}~{}~{}~{}M_{1}&=5~{},~{}~{}~{}~{}P_{0}=1~{},~{}~{}~{}~{}P_{1}=0.3~{},~{}~{}~{}~{}\mu=\pi~{},~{}~{}~{}~{}\eta=8\pi/5~{}.\end{aligned} (89)

Fig 5.7 shows 3 views of the resulting embedding. The right hand view shows there is substantial rotation of the θ=0\theta=0 direction.

[Uncaptioned image] [Uncaptioned image]      [Uncaptioned image] Fig 7.   Three views of the embedded Szekeres model 4, at time η=π\eta=\pi which corresponds to t=0t=0. The blue circles represent 2-spheres of constant rr; tilting relative to the line of sight makes some appear elliptical. The red curve is the centre path — the locus of sphere centres, and the green lines show the direction of θ=0\theta=0 for each plotted sphere/circle. The YY coordinate is suppressed, and the centre path lies in Y=0Y=0.

5.8 Model 5, RW as Szekeres

The Szekeres models become homogeneous, despite the non-symmetric coordinates, if the LT functions ff, MM & aa take the RW form, regardless of the SS, PP & QQ functions888See [12] around eq (2.24) and section 1.3.4 of [20].. Such a model is obtained with M=M0sin3(μr)M=M_{0}\sin^{3}(\mu r), f=sin2(μr)f=-\sin^{2}(\mu r), a=0a=0, S=1S=1, Q=0Q=0 and P=P0sin(μr)(P0+P1sin(μr))P=P_{0}\sin(\mu r)(P_{0}+P_{1}\sin(\mu r)), along with parameter values M0=1M_{0}=1, P0=0.7P_{0}=0.7, P1=0.09P_{1}=0.09, μ=π\mu=\pi, and the result is shown in fig 5.8.

[Uncaptioned image] [Uncaptioned image]      [Uncaptioned image] Fig 8.   Three views of the embedded RW-Szekeres model 5, showing it is actually a 3-sphere in very non-symmetric coordinates. The centre path (red line) is bent round, and the ‘north’ (green lines) show significant variation.

Although the overall embedded shape is clearly a 3-sphere, the slicing is not only non-parallel, it also has shell rotation as shown by the variation of the ‘north’ direction.

6 Conclusions

A correct understanding of the geometry of the Szekeres metric is important both for physical interpretation, when it is used for models of inhomogeneous gravitating structures, and also for a more accurate graphical depiction of those models. Though the ‘non-concentric’ property of constant rr shells was known from the start, it was only recently shown there is a hidden shell rotation effect, that appears when the usual angular coordinates are used. Hitherto, it was tacitly assumed these coordinates had a constant orientation, as is the case for Lemaître-Tolman (LT) models.

In this paper we have shown that two independent results about Szekeres shell rotations are in full agreement. In FR [15] it was shown, using the rotation rate of an orthonormal tetrad, that the (θ,ϕ)(\theta,\phi) coordinates of (12) do not in general retain any kind of constant orientation. In [6] the relative rotation of adjacent (θ,ϕ)(\theta,\phi) shells was stated, and in PG [7] this was explained in several ways, notably an embedding that further introduced higher dimensional tilts. The forms of the results in FR & PG are sufficiently different that an alignment is called for. We have reviewed the embedding of a f<0f<0 Szekeres model in flat 4-d Euclidean space, and discussed its visualisation. It is striking that the embedding of a Szekeres model is locally the same to first order as that of the underlying LT model at the corresponding rr value. By showing how to derive the FR results from the PG results, we have confirmed the reality of these rotations and tilts, and thereby their importance for graphing Szekeres slices. Methods for this graphing are suggested in PG.

To illustrate the higher dimensional tilts, we have constructed Szekeres models whose 3-spaces ‘naturally’ have the topology of a torus, when embedded in a 4-d Euclidean flat space, without arbitrary identifications. Explicit Szekeres models that are closed in the rr direction, with or without an arbitrary identification, had not been been previously considered. Models 1 & 2 had just SS varying, but nicely demonstrated the toroidal embedding as well as non-trivial radius and tilt structure. Models 3 & 4 had just PP varying, and additionally demonstrated a non-planar curve of shell centres. Importantly, model 4 clearly exhibited the shell rotation described in PG. Clearly, models in which all 3 of the Szekeres functions SS, PP & QQ vary could produce even more interesting embedded shapes.

Some questions for future investigations are
(i) Can one find a different (p,q)(p,q) to (θ,ϕ)(\theta,\phi) transformation that incorporates the rotation, (20), found by Buckley & Schlegel? Is it reasonably neat or too complicated? Does the resulting metric look at all useful or useable?
(ii) Can one apply or extend the embedding to the DKS-type (“β=0\beta^{\prime}=0”) Szekeres models?
(iii) Is there a reasonably simple or elegant embedding of the ϵ+1\epsilon\neq+1 Szekeres models?
(iv) Is it possible to create a quasi-spherical Szekeres model in which the shell rotation turns the ‘north pole’ through 180 degrees? Can such a model be given a toroidal topology, of any kind? That would make the transformation to (θ,ϕ)(\theta,\phi) coordinates clearly inconsistent.

References

  • [1] K. Bolejko, Phys. Rev. D 73, 123508 (2006), “Structure Formation in the Quasispherical Szekeres Model”.
  • [2] K. Bolejko, Phys. Rev. D 75, 043508 (2007), “Evolution of Cosmic Structures in Different Environments in the Quasispherical Szekeres Model”.
  • [3] K. Bolejko, J. Cosm. Astropart. Phys. 2017, 06:025 (2017), “Cosmological Backreaction Within the Szekeres Model and Emergence of Spatial Curvature”. arXiv:1704.02810 [astro-ph.CO].
  • [4] K. Bolejko, M.A. Nazer, D.L. Wiltshire, J. Cosm. Astropart. Phys. 2016, 06:035 (2016), “Differential Cosmic Expansion and the Hubble Flow Anisotropy”. arXiv:1512.07364.
  • [5] K. Bolejko & R. Sussman, Phys. Lett. B 697, 265-70 (2011), “Cosmic Spherical Void Via Coarse-Graining and Averaging Non-Spherical Structures”. arXiv:1008.3420.
  • [6] R.G. Buckley & E.M. Schlegel, Phys. Rev. D 87, 023524, 1-13 (2013), “CMB Dipoles and Other Low-Order Multipoles in the Quasispherical Szekeres Model”. arXiv:1907.08684 [astro-ph.CO].
  • [7] R.G. Buckley & E.M. Schlegel, Phys. Rev. D 101, 023511, 1-26 (2020), “Physical Geometry of the Quasispherical Szekeres Models”. arXiv:1908.02697 [gr-qc].
  • [8] B. Datt, Zeit. Physik 108, 314 (1938), “Über eine Klasse von Lösungen der Gravitationsgleichungen der Relativität”. Reprinted in English with historical introduction in: Gen. Rel. Grav. 31, 1619-27 (1999).
  • [9] G.F.R. Ellis, J. Math. Phys. 8, 1171-94 (1967), “Dynamics of Pressure-Free Matter in General Relativity”.
  • [10] I.D. Gaspar, J.C. Hidalgo, R.A. Sussman & I. Quiros, Phys. Rev. D 97, 104029 (2018), “Black Hole Formation from the Gravitational Collapse of a Non-Spherical Network of Structures”. arXiv:1802.09123 [gr-qc].
  • [11] I. Georg & C. Hellaby, Phys. Rev. D 95, 124016, 1-16 (2017), “Symmetry and Equivalence in Szekeres Models”. arXiv:1702.05347.
  • [12] S.W. Goode & J. Wainwright, Phys. Rev. D 26, 3315-26 (1982), “Singularities and Evolution of the Szekeres Cosmological Models”.
  • [13] C. Hellaby, Class. Quantum Grav. 4, 635-650 (1987), “A Kruskal-Like Model with Finite Density”.
  • [14] C. Hellaby, Proc. Sci. PoS(ISFTG), 005, 1-50 (2009), “Modelling Inhomogeneity in the Uni-verse”. https://pos.sissa.it/cgi-bin/reader/conf.cgi?confid=81. arXiv:0910.0350 [gr-qc].
  • [15] C. Hellaby, Class. Quantum Grav. 34, 145006, 1-20 (2017), “Frame Rotation in the Szekeres Spacetimes”. arXiv:1706.00622 [gr-qc].
  • [16] C. Hellaby & A. Krasiński, Phys. Rev. D 66, 084011, 1-27 (2002), “You Can’t Get Through Szekeres Wormholes: Regularity, Topology and Causality in Quasi-Spherical Szekeres Models”. arXiv:gr-qc/0206052.
  • [17] C. Hellaby & A. Krasiński, Phys. Rev. D 77, 023529, 1-26 (2008), “Physical and Geometrical Interpretation of the ϵ0\epsilon\leq 0 Szekeres Models”. arXiv:0710.2171 [gr-qc].
  • [18] C. Hellaby & K. Lake, Astrophys. J. 290, 381-387 (1985), “Shell Crossings and the Tolman Model”.; plus errata in Astrophys. J.300 461 1986.
  • [19] R. Kantowski & R.K. Sachs, J. Math. Phys. 7, 443-6 (1966), “Some Spatially Homogeneous Anisotropic Relativistic Cosmological Models”.
  • [20] A. Krasiński, Inhomogeneous Cosmological Models, Cambridge U P, 1997, ISBN 0 521 48180 5.
  • [21] A. Krasiński & K. Bolejko, Phys. Rev. D 85, 124016 (2012), “Apparent Horizons in the Quasispherical Szekeres Models”.
  • [22] G. Lemaître, Ann. Soc. Sci. Bruxelles A53, 51-85 (1933), “L’Universe en Expansion”. Reprinted in English with historical introduction in: Gen. Rel. Grav. 29, 641-80 (1997).
  • [23] R.A. Sussman & I.D. Gaspar, Phys. Rev. D 92, 083533 (2015), “Multiple Non-Spherical Structures from the Extrema of Szekeres Scalars”. arXiv:1508.03127 [gr-qc].
  • [24] R.A. Sussman, I.D. Gaspar & J.C. Hidalgo, J. Cosm. Astropart. Phys. 2016, 03:012 (2016), “Coarse-Grained Description of Cosmic Structure from Szekeres Models”. Errata in: J. Cosm. Astropart. Phys. 2016, 06:E03 (2016). arXiv:1507.02306 [gr-qc].
  • [25] P. Szekeres, Comm. Math. Phys. 41, 55-64 (1975), “A Class of Inhomogeneous Cosmological Models”.
  • [26] P. Szekeres, Phys. Rev. D 12, 2941-8 (1975), “Quasispherical Gravitational Collapse”.
  • [27] R.C. Tolman, Proc. Nat. Acad. Sci. U.S.A. 20, 169-76 (1934), “Effect of Inhomogeneity on Cosmological Models”. Reprinted with historical introduction in: Gen. Rel. Grav. 29, 935-43 (1997).
  • [28] A. Walters and C. Hellaby, J. Cosm. Astropart. Phys. 2012, 12:001, 1-40 (2012), “Constructing Realistic Szekeres Models from Initial and Final Data”. arXiv:1211.2110 [gr-qc].