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2012 – Solutions

Yichen Shi Easter 2014

1.

(a) Explain the following terms: covariant , connection components.

A ∇ on a M is a map sending every pair of smooth vector fields X, Y to a smooth vector field ∇X Y , with properties

∇fX+gY Z = f∇X Z + g∇Y Z

∇X (Y + Z) = ∇X Y + ∇X Z

∇X (fY ) = f∇X Y + (∇X f)Y µ In a basis eµ the connection components Γνρ are defined by

µ ∇ρeσ = ∇eρ eσ = Γρσeµ

The Christoffel symbols are the coordinate basis components of the Levi-Civita connection, which is defined on any manifold with a metric.

(b) What does it mean for a connection to be torsion-free? Define the Levi-Civita connection and derive the formula 1 Γµ = gµσ(∂ g + ∂ g − ∂ g ). νρ 2 ρ σν ν σρ σ νρ

A connection ∇ is torsion-free if [∇a, ∇b]f = 0 for any function f. For a torsion-free connection, if X and Y are vector fields then ∇X Y − ∇Y X = [X,Y ]. On a manifold with a metric, the metric singles out a preferred connection. Let M be a manifold with a metric g. There exists a unique torsion-free connection ∇, the Levi-Civita connection, which is metric compatible, i.e., ∇g = 0. Hence we have

l l ∇igjk = 0 = ∂igjk − Γijgkl − Γikgjl

l l ⇒ ∂igjk = Γijgkl + Γikgjl l l¨¨ l Hl l¨¨ Hl l ⇒ ∂igjk + ∂jgik − ∂kgij = Γijgkl +¨Γikgjl + Γjigkl + ΓjkHgHil −¨Γkigjl − ΓkjHgHil = 2Γijgkl, k since torsion free implies Γ[ij] = 0. 1 ⇒ Γl g = (∂ g + ∂ g − ∂ g ) ij kl 2 i jk j ik k ij 1 ⇒ Γl = gkl(∂ g + ∂ g − ∂ g ). ij 2 i jk j ik k ij

1 (c) A 2d has metric

ds2 = dr2 + f(r)2dφ2 where φ is periodically identified with period 2π (so curves of constant r are circles).

(i) Determine the necessary and sufficient conditions on f(r) for the circle r = r0 to have the property that all vectors are invariant under around the circle.

We want that for any vector field X,

a b µ ν µ ν ρ ∇V X = 0, or, V ∇aX = 0 ⇒ V ∂µX + V ΓµρX = 0,

∂ for some V indicating “around the circle”. Since ∂φ is tangent to the circle, we take ∂ V = . ∂φ Hence our equation reduces to ν ν ρ ∂φX + ΓφρX = 0. To find the Γ’s, we start with the Lagrangian

L =r ˙2 + f(r)2φ˙2.

The are

2f 0 f 0 f 2φ¨ + 2ff 0r˙φ˙ = 0 ⇒ φ¨ + r˙φ˙ = 0 ⇒ Γφ = Γφ = ; f rφ φr f

0 ˙2 r 0 r¨ − ff φ = 0 ⇒ Γφφ = −ff . φ φ r ⇒ ν = φ : ∂φX + ΓφrX = 0; r r φ ⇒ ν = r : ∂φX + ΓφφX = 0, which give f 0 ∂ Xφ + Xr = 0; ∂ Xr − ff 0Xφ = 0. φ f φ

r f 2 φ The first gives ∂φX = − f 0 ∂φX . Substituting it into the second, we have

2 φ 02 φ ∂φX + f X = 0.

φ 1 2 r And the second gives ∂φX = ff 0 ∂φX . Substituting it into the first, we have

2 r 02 r ∂φX + f X = 0.

Hence Xφ(φ) = Xφ(0) cos(f 0φ) + X0φ(0) sin(f 0φ); Xr(φ) = Xr(0) cos(f 0φ) + X0r(0) sin(f 0φ). So we require Xφ(0) = Xφ(2π) and Xr(0) = Xr(2π). This is true iff

0 f = n, n ∈ Z.

2 (ii) Deduce that there is a 2-parameter family of functions f(r) for which all circles of constant r have this property.

From (i), we have f(r) = nr + c, c = const.

(iii) For this 2-parameter family, show that the metric is locally isometric to the Euclidean metric. Is it globally isometric?

Locally isometric means we can find coordinates such that the metric looks like

ds2 = dr˜2 +r ˜2dφ˜2, r˜ =r ˜(r), φ˜ = φ˜(φ).

Indeed we have

ds2 = dr2 + (nr + c)2dφ2 = dr˜2 +r ˜2dφ˜2

where we have setr ˜ = r + c/n and φ˜ = nφ. Hence we have a local . We have a global isometry only when n = 1, since now φ˜ is periodically identified with period 2πn.

2.

Let Ta be tangent to a 1-parameter family of timelike of the Levi-Civita connection, parame- terized by proper time. Let Sa be a deviation vector for this family.

(a) Explain the term deviation vector. Explain why [S, T ] = 0.

A 1-parameter family of geodesics is a map γ : I × I0 → M where I and I0 both are open intervals in R, such that for fixed s, γ(s, t) is a with affine parameter t, and s is the parameter that labels the geodesic. Further, the map (s, t) → γ(s, t) is smooth and one-to-one with a smooth inverse.

A deviation vector Sa is the displacement of two objects travelling along two such neighbouring geodesics such that xa(s + δs, t) ' xa(s, t) + δsSa(s, t)

a a a ∂x (s,t) a ∂x (s,t) where S (s, t) = ∂s . Note that T (s, t) = ∂t .

The family of geodesics forms a two-dimensional surface Σ ⊂ M. Treating s and t as coordinates, we can extend them to (s, t, u, ...) defined in a neighbourhood of Σ. This gives a coordinate chart on Σ where S = ∂/∂s and T = ∂/∂t are vector fields satisfying

[S, T ] = 0.

3 (b) State and prove the geodesic deviation equation. You may assume the definition of the Riemann R(X,Y )Z = ∇X ∇Y Z − ∇Y ∇X Z − ∇[X,Y ]Z.

The geodesic deviation equation is ∇T ∇T S = R(T,S)T if ∇ has vanishing torsion.

Proof: Vanishing torsion implies ∇X Y − ∇Y X = [X,Y ]; we have from above [S, T ] = 0; and we have ∇T T = 0 since T is tangent to affinely parametrised geodesics. Hence

R(T,S)T = ∇T ∇ST − ∇S∇T T − ∇[T,S]T = ∇T ∇T S.

(c) Prove that if Sa and T a are orthogonal at one point along a geodesic γ (belonging to the 1-parameter family) then they are orthogonal everywhere along γ.

1 1 ∇ (T · S) = (∇ T ) · S + T · (∇ S) = T ∇ S = T ∇ T = ∇ (T · T ) = ∇ (-1) = 0 T T T T S 2 S 2 S since T is timelike. Hence there is no change in the value of T · S along the geodesic.

(d) Suppose that is four-dimensional with Riemann tensor

1 R = R(g g − g g ) abcd 12 ac bd ad bc Show that R must be constant.

We first contract the given Riemann tensor to find 1 1 R = R(4g − g ) = Rg . bd 12 bd bd 4 bd Using this, we have the 1 1 G = R − Rg = − Rg . ab ab 2 ab 4 ab a But ∇ Gab = 0. Hence ∇aR = 0, i.e., R is constant.

a a a (e) Assume that S is orthogonal to T . Let f = SaS . Show that, in the above spacetime, 1 K = (∇ S) (∇ S)a − Rf T a T 12 is constant along a geodesic γ in the family.

4 1 1 ∇ K = ∇ (∇ S · ∇ S) − (∇ R)S · S − R∇ (S · S) T T T T 12 T 12 T 1 = 2∇ ∇ S · ∇ S − RS · ∇ S (since R here is constant) T T T 6 T 1 = 2R(T,S)T · ∇ S − RS · ∇ S T 6 T 1 = 2R T bT cSdT e∇ Sa − RSaT e∇ S abcd e 6 e a 1 1 = R(g g − g g )T bT cSdT e∇ Sa − RSaT e∇ S 6 ac bd ad bc e 6 e a 1 1 1 = RT T SdT e∇ Sa − RT T cS T e∇ Sa − RS T e∇ Sa 6 d a e 6 c a e 6 a e 1 1 1 = R(T Sd)T T e∇ Sa − R(T T c)S T e∇ Sa − RS T e∇ Sa 6 d a e 6 c a e 6 a e 1 1 = RS T e∇ Sa − RS T e∇ Sa (since T Sd = 0 by orthogonality and T is timelike) 6 a e 6 a e d = 0.

(f) Obtain a second order for the evolution of f along γ. Hence deduce that if R > 0 then geodesics which are close initially will diverge exponentially. What happens if R < 0?

∇T ∇T f = ∇T ∇T (S · S)

= 2∇T (S · ∇T S)

= 2(∇T S) · (∇T S) + 2S · ∇T ∇T S 1 = 2(K + Rf) + 2S · R(T,S)T 12 1 1 = 2K + Rf + 2Sa R(g g − g g )T bT cSd 6 12 ac bd ad bc 1 1  1 = 2K + Rf + RSTT cSd − RS T T cSd 6 6 c d 6 d c 1 = 2K + Rf (since SdT = 0). 3 d So the differential equation for the evolution of f is

d2f 1 − Rf − 2K = 0, dt2 3 from which we can see that if R > 0, the late-time solution is dominated by an exponential growth ∼ exp(pR/3 t), but if R < 0 there are oscillations.

3.

In the study of linearised perturbations of Minkowski spacetime, it is assumed that there exist global µ coordinates x with respect to which the metric has components gµν = ηµν + hµν where the components of hµν have absolute values much smaller than 1.

ρ ¯ 1 µ¯ (a) Let h = h ρ and hµν = hµν − 2 hηµν . By imposing the gauge condition ∂ hµν = 0, derive the linearised Einstein equation in the form ρ ¯ ∂ ∂ρhµν = −16πTµν

5 You may use µ µ µ τ µ τ µ R νρσ = ∂ρΓνσ − ∂σΓνρ + ΓνσΓτρ − ΓνρΓτσ, valid in a coordinate basis.

To first order, the Christoffel symbols are 1 Γµ = ηµσ(∂ h + ∂ h − ∂ h ) νρ 2 ν σρ ρ σν σ νρ And to first order, the Riemann are

µ µ µ R νρσ = ∂ρΓνσ − ∂σΓνρ 1 = ηµα(∂ ∂ h + ∂ ∂ h − ∂ ∂ h − ∂ ∂ h − ∂ ∂ h + ∂ ∂ h ) 2 ν ρ ασ σ ρ αν α ρ νσ ν σ αρ ρ σ αν α σ νρ

1 ⇒ Rρ = (∂ ∂ hρ + ∂ ∂ hρ − ∂ρ∂ h − ∂ ∂ hρ − ∂ ∂ hρ + ∂ρ∂ h ) νρσ 2 ν ρ σ σ ρ ν ρ νσ ν σ ρ ρ σ ν σ νρ 1 1 = ∂ρ∂ h − ∂ρ∂ h − ∂ ∂ h (ν σ)ρ 2 ρ νσ 2 ν σ = Rνσ

Now, 1 1 1 1 R − g R = ∂ρ∂ h − ∂ρ∂ h − ∂ ∂ h − η (∂ρ∂σh − ∂ρ∂ h) µν 2 µν (µ ν)ρ 2 ρ µν 2 µ ν 2 µν σρ ρ 1 1 1 1 1 1 = ∂ρ∂ (h¯ − hη¯ ) + ∂ρ∂ (h¯ − hη¯ ) − ∂ρ∂ (h¯ − hη¯ ) 2 µ νρ 2 νρ 2 ν µρ 2 µρ 2 ρ µν 2 µν 1 1 1 + ∂ ∂ h¯ − η (∂ρ∂σ(h¯ − hη¯ ) + ∂ρ∂ h¯) 2 µ ν 2 µν σρ 2 σρ ρ X1 1 1 ¨ ρ ¯ Xρ X ¯ ρ ¯ ρ ¨¯¨ = ∂ ∂(µhν)ρ − ∂ ∂(µXhηXνX)ρ − ∂ ∂ρhµν + ∂¨∂ρhηµν 2 2 ¨4 H ¨ ¨ 1 H ¯ 1 ρ σ¯ 1 ρ¨ ¯ 1 ρ¨ ¯ + ∂µ∂Hν h − ηµν ∂ ∂ hσρ + ηµν¨∂ ∂ρh − ηµν¨∂ ∂ρh 2 H 2 ¨4 ¨ ¨2 ¨ ¯ 1 ¯ 1 ¯ ¯ where hµν = hµν − 2 hηµν gives hµν = hµν − 2 hηµν and h = −h. Hence from 1 R − g R = 8πT , µν 2 µν µν we get the linearised Einstein equation 1 1 ∂ρ∂ h¯ − ∂ρ∂ h¯ − η ∂ρ∂σh¯ = 8πT . (µ ν)ρ 2 ρ µν 2 µν σρ µν µ¯ Imposing the gauge condition ∂ hµν = 0, the first and the third terms disappear and we arrive at

ρ ¯ ∂ ∂ρhµν = −16πTµν .

(b) Consider a vacuum plane gravitational wave solution with

ρ ¯ ikρx hµν = Re(Hµν e ) where Hµν is a constant complex matrix and kρ a constant covector. What restrictions must Hµν and kρ obey in the above gauge?

6 µ¯ In the gauge ∂ hµν = 0, µ k Hµν = 0 i.e., the waves are transverse.

Explain why there is a residual gauge freedom hµν → hµν + 2∂(µξν) provided ξµ satisfies a certain con- dition. Show that this condition is satisfied by

ρ ikρx ξµ = Re(Xµe ) where Xµ is constant.

A manifold M with metric g and energy-momentum tensor T is physically equivalent to M with φ∗(g) and energy momentum tensor φ∗(T ) if φ is a diffeomorphism. Hence

(φ−t)∗(g) = g + Lξg + ··· = η + h + Lξη + ··· is equivalent to g = η + h, i.e., h and h+Lξη describe physically equivalent metric perturbations. Since (Lξη)µν = ∂µξν +∂ν ξµ = 2∂(µξν) (think about the Killing equation), there is a residual gauge freedom

hµν → hµν + 2∂(µξν).

µ¯ The gauge condition ∂ hµν = 0 needs to be satisfied. Note first that

ρ h → h + 2∂ ξρ.

1 ⇒ h¯ = h − hη µν µν 2 µν 1 1 → h + 2∂ ξ − hη − η (2∂ρξ ) µν (µ ν) 2 µν 2 µν ρ ¯ ρ = hµν + 2∂(µξν) − ηµν ∂ ξρ. Hence we have µ¯ µ¯ µ µ  µ ρ ∂ hµν → ∂ hµν − ∂ ∂µξν −∂ ∂ν ξµ +∂ ∂ ξρηµν µ¯ µ = ∂ hµν − ∂ ∂µξν µ = −∂ ∂µξν (by gauge condition) =! 0.

This condition is satisfied by ρ ikρx ξµ = Re(Xµe ) ρ ¯ ρ ¯ since vacuum ⇒ ∂ ∂ρhµν = 0 ⇒ k kρ = 0 with the given solution of hµν .

Now show that Xµ can be chosen to bring Hµν to the form

 0 0 0 0   0 H+ H× 0  Hµν =   .  0 H× −H+ 0  0 0 0 0

Use your results to justify the statements that gravitational waves travel at the speed of light, are trans- verse, and have 2 independent polarizations.

7 µ ν ¯ First consider the null vector k = ω(1, 0, 0, 1). Then from the transverse gauge condition ∂ hµν = 0, we have here ν 0 3 ik Hµν = ik Hµ0 + ik Hµ3 = 0 ⇒ Hµ0 + Hµ3 = 0. Now, recall that we had ¯ ¯ ρ hµν → hµν + 2∂(µξν) − ηµν ∂ ξρ. ρ ⇒ Hµν → Hµν + i(kµXν + kν Xµ − ηµν k Xρ).

To achieve the longitudinal gauge H0ν = 0, set

ρ k0Xν + kν X0 − η0ν k Xρ := iH0ν , i.e., k0X0 + k1X1 + k2X2 + k3X3 = iH00;

k0X1 + k1X0 = iH01;

k0X2 + k2X0 = iH02;

k0X3 + k3X0 = iH03. Or,       k0 k1 k2 k3 X0 H00  k1 k0 0 0   X1   H10      = i    k2 0 k0 0   X2   H20  k3 0 0 k0 X3 H30

After row reduction, the last equation is 0 on both sides. Hence there exists multiple solutions for Xµ. We µ can impose the traceless condition H µ = 0 to fix the gauge. Combining the results of the transverse and the longitudinal gauge conditions gives H3ν = 0. Hence,

 0 0 0 0   0 H+ H× 0  Hµν =   .  0 H× −H+ 0  0 0 0 0

ρ ¯ ρ Gravitational wave travels at the speed of light since ∂ ∂ρhµν = 0 gives k kρ = 0. It is transverse since, µ¯ µ as mentioned earlier, ∂ hµν = 0 gives k Hµν = 0. And it has two independent polarisations as represented by H× and H+.

(c) (i) Explain briefly why it is not possible to define an energy-momentum tensor for the gravitational field in General Relativity.

The energy in the gravitational field should be quadratic in the first of the metric, which in turn can always be set to zero at any point by a change of coordinates.

(ii) Explain how to define a symmetric tensor tµν that is quadratic in the linearized gravitational field µ hµν and conserved, i.e., ∂ tµν = 0.

The Einstein tensor to second order is

(1) (1) (2) (2) Gµν [g] = Gµν [h] + Gµν [h ] + Gµν [h]

Assume that no matter is present, i.e., Gµν [g] = 0 and at first order, the linearised Einstein equation is G(1)[h] = 0. At second order, (1) (2) Gµν [h ] = 8πtµν [h]

8 where 1 t [h] := − G(2)[h] µν 8π µν µ Consider the contracted Bianchi identity ∇ Gµν = 0. At first order,

µ (1) ∂ Gµν [h] = 0

(2) µ (1) (2) for arbitrary first order perturbation h, i.e., if we replace h with h then ∂ Gµν [h ] = 0. At second order, X ¨ µXX(1) (2) µ (2) (1)¨¨ ∂ Gµν X[hXX] + ∂ Gµν [h] + h¨Gµν [h] = 0 where the third term vanished since we assumed that the equation of motion G(1)[h] = 0 is obeyed.

µ ⇒ ∂ tµν = 0

Hence tµν is a symmetric tensor that is (i) quadratic in the linear perturbation h, (ii) conserved if h satisfies its equation of motion, and (iii) appears on the RHS of the second order Einstein equation.

(iii) Why is tµν unsatisfactory as a definition of an energy-momentum tensor for hµν ?

tµν is unsatisfactory as it is not invariant under the gauge transformation hµν → hµν + 2∂(µξν). This is how the impossibility of localising gravitational energy arises in linearised theory.

4.

(a) (i) What is a Killing vector field?

A vector field X is a Killing vector field if

LX g = 0,

i.e., ∇aXb + ∇bXa = 0

(ii) Show that if a spacetime admits a Killing vector field then along any geodesic there is a conserved quantity.

a a a Let X be a Killing vector field and let V be tangent to an affinely parametrised geodesic. Then XaV is constant along the geodesic. Proof: a b a b a b a ∇V (XaV ) = V ∇b(XaV ) = XaV ∇bV + V V ∇bXa = 0 b a b where V ∇bV = 0 as V is tangent to an affinely parametrised geodesic (it is the geodesic equation!), and b a the second term vanishes as V V is symmetric but ∇bXa is antisymmetric by the Killing equation.

(iii) Write down 3 linearly independent Killing vector fields of the metric

ds2 = A(z)2(−dt2 + dx2 + dy2) + dz2

where A(z) is a positive function.

∂ Let T := ∂t . We claim that T is a Killing vector. Proof: ρ ρ ρ (LX g)µν = X ∂ρgµν + gρν ∂µX + gρµ∂ν X = 0

9 where the later two terms vanish since Xt = 1 while other Xρ = 0, and the first term vanishes since z ∂ρ6=zgµν = 0 as the entries of gµν depend only on z, and for ρ = z, this term vanishes still since X = 0. ∂ ∂ Similarly, X := ∂x and Y := ∂y are Killing vectors.

Note that if a Killing vector field X generates , then LX g = 0. And since

L[X,Y ] = LX LY − LY LX = 0, we can find a third Killing vector field by taking the commutator of the first two, given that X and Y are independent Killing vector fields, i.e., [X,Y ] 6= 0.

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