BANACH CENTER PUBLICATIONS, VOLUME 41 INSTITUTE OF MATHEMATICS POLISH ACADEMY OF SCIENCES
WARSZAWA 1997
POST-NEWTONIAN HYDRODYNAMIC EQUATIONS USING THE (3+1) FORMALISM IN
GENERAL RELATIVITY
H I D E K I A S A D A
Department of Earth and Space Science
Graduate School of Science, Osaka University, Toyonaka, Osaka 560, Japan E-mail: asada@vega.ess.sci.osaka-u.ac.jp
Abstract. The post-Newtonian (PN) hydrodynamic equations are obtained in the (3+1) formalism, which include the 2.5PN order as the reaction due to the quadrupole gravitational radiation. These equations are valid in various slice conditions, while we adopt a kind of trans- verse gauge condition to determine the shift vector. In particular, we describe methods to solve the 2PN tensor potential which arises from the spatial 3-metric. Our formulaton in the PN ap- proximation using the (3+1) formalism will be useful for numerical computations providing an initial data for the final merging phase of coalescing binary neutron stars which can be treated only by fully general relativistic simulations.
1. Introduction. Aiming at the direct detection of gravitational waves from rela- tivistic astrophysical objects, kilometer-size interferometric gravitational wave detectors, such as LIGO [1] and VIRGO [2], are now under construction. Coalescing binary neutron stars are the most promising sources of gravitational waves for such detectors. After a long time emission of gravitational waves, the orbital separation of binary becomes com- parable to the radius of the neutron star. Then, each of binary neutron stars begins to behave as a hydrodynamic object, not as a point particle, because they are tidally coupled with each other. Recently, Lai, Rasio and Shapiro [3] have pointed out that such a tidal coupling of binary neutron stars is very important for their evolution in the final merging phase because the tidal effect causes the instability of their circular motion. The general relativistic gravity is also important because in such a phase, the orbital separation is less than ten times the Schwarzschild radius of the system. Thus, we need not only a hydrodynamic treatment, but also a general relativistic one to study the final phase of binary neutron stars.
1991 Mathematics Subject Classification: 83C25, 83C35.
The paper is in final form and no version of it will be published elsewhere.
[85]
Surely fully general relativistic simulation must be the best method, but it is also one of the most difficult ones. Although much effort has been focused and much progress can be expected there [4], it will take a long time until numerical relativistic calculations become reliable. One of the main reasons is that we do not know the behavior of the geometric variables in the strong field around coalescing binary neutron stars. According to this, we do not know what sort of gauge condition is useful and how to give an appropriate general relativistic initial condition for coalescing binary neutron stars.
The other reason is a technical one: In numerical relativistic simulations, gravitational waves are generated when we need to cover a region L > λ ∼ the wavelength in order to perform accurate simulations. This is in contrast with the case of Newtonian and/or PN simulations, in which we only need to cover a region (λ >)L > R ∼ the orbital separation.
At present, we had better search other methods to prepare an initial condition for binary neutron stars.
The PN approximation in the fluid was pioneered by Chandrasekhar et al. [5] who ob- tained the equation of motion up to the 2.5PN order. However, their expressions include potentials for non-compact sources which should be solved rather carefully in practical cases. On the other hand, using the ADM gauge, Blanchet, Damour and Sch¨ afer obtained the formula, including the 1PN effects and the quadrupole radiation reaction (2.5PN ef- fect) [6], which only consists of potentials for compact sources. Their formula actually works well in simulations of the coalescing binary neutron stars [7]. Our aim is to establish the formulation up to the 2.5PN hydrodynamic equation for a fairly wide class of gauge conditions and, in particular, to provide methods to solve the 2PN tensor potential which does not appear at the 1PN order [6].
We use the units of c = G = 1 in this paper. Greek and Latin indices take 0, 1, 2, 3 and 1, 2, 3, respectively.
2. (3+1) Formalism for post-Newtonian approximation (3+1) Formalism. In the (3+1) formalism, the metric is split as
g µν = γ µν − ˆ n µ n ˆ ν , (2.1) where ˆ n µ = (−α, 0). Then the line element is written as
ds 2 = −(α 2 − β i β i )dt 2 + 2β i dtdx i + γ ij dx i dx j . (2.2) In order to distinguish the wave part from the non-wave part (for example, Newtonian potential) in the metric, we use ˜ γ ij = ψ −4 γ ij instead of γ ij where ψ = det(γ ij ) 1/12 so that det(˜ γ ij ) = 1 is satisfied. Using the extrinsic curvature, K ij , we define ˜ A ij as
A ˜ ij ≡ ψ −4 A ij ≡ ψ −4 K ij − 1
3 γ ij K
. (2.3)
The Einstein equation is split into the constraint equations and the evolution equations.
The former are called Hamiltonian and momentum constraints which respectively become
∆ψ = ˜ 1
8 tr ˜ Rψ − 2πρ H ψ 5 − ψ 5 8
˜ A ij A ˜ ij − 2 3 K 2
, (2.4)
D ˜ j (ψ 6 A ˜ j i ) − 2
3 ψ 6 D ˜ i K = 8πψ 6 J i , (2.5)
where we introduce ρ H = T µν n µ n ν and J j = −T µν n µ γ j ν , and ˜ D i , ˜ ∆ and tr ˜ R are the covariant derivative, Laplacian and the scalar curvature with respect to ˜ γ ij . Evolution equations for the spatial metric and extrinsic curvature are respectively
∂
∂n ˜ γ ij = − 2α ˜ A ij + ˜ γ il
∂β l
∂x j + ˜ γ jl
∂β l
∂x i − 2 3 γ ˜ ij
∂β l
∂x l , (2.6)
∂
∂n
A ˜ ij = 1 ψ 4
h α
R ij − 1
3 γ ij trR
− ˜ D i D ˜ j α − 1
3 ˜ γ ij ∆α ˜
− 2 ψ
ψ ,i α ,j + ψ ,j α ,i − 2
3 ˜ γ ij ˜ γ kl ψ ,k α ,l i + α(K ˜ A ij − 2 ˜ A il A ˜ l j ) + ∂β m
∂x i
A ˜ mj + ∂β m
∂x j
A ˜ mi − 2 3
∂β m
∂x m A ˜ ij
− 8π α ψ 4
S ij − 1
3 γ ij S l l
, (2.7)
∂
∂n ψ = ψ 6
−αK + ∂β i
∂x i
, (2.8)
∂
∂n K = α ˜ A ij A ˜ ij + 1 3 K 2
− 1 ψ 4
∆α − ˜ 2
ψ 5 γ ˜ kl ψ ,k α ,l + 4πα(S i i + ρ H ), (2.9) where R ij , γ, S ij and ∂n ∂ denote, respectively, the Ricci tensor with respect of γ ij , deter- minant of γ ij , T kl γ k i γ l j and ∂t ∂ − β i ∂ ∂x
i.
In order to clarify the wave property of ˜ γ ij , we impose a kind of transverse gauge* to h ij as
h ij,j = 0. (2.10)
Finally, we consider the matter as the perfect fluid, T µν = (ρ + ρε + P )u µ u ν + P g µν , where u µ , ρ, ε and P are the four velocity, the mass density, the specific internal energy and the pressure.
Post-Newtonian approximation. Each metric variable, which is relevant to the present paper, is expanded as
ψ = 1 + (2) ψ + (4) ψ + (6) ψ + (7) ψ + . . . , α = 1 − U + U 2
2 + X
+ (6) α + (7) α + . . . , β i = (3) β i + (5) β i + (6) β i + (7) β i + (8) β i + . . . , h ij = (4) h ij + (5) h ij + . . . ,
A ˜ ij = (3) A ˜ ij + (5) A ˜ ij + (6) A ˜ ij + . . . , K = (3) K + (5) K + (6) K + . . . ,
(2.11)
where subscripts denote the PN order (c −n ) and U is the Newtonian potential satisfying
∆ f lat U = −4πρ. (2.12)
* Hereafter, we call this condition merely the transverse gauge.
From Eqs.(2.6) and (2.7), the wave equation for h ij is written as
− ∂ 2
∂t 2 + ∆ f lat
h ij
= 1 − α 2
ψ 4
∆ f lat h ij + ∂ 2
∂n 2 − ∂ 2
∂t 2
h ij
+ 2α ψ 4
h − 2α ψ
˜ D i D ˜ j − 1 3 ˜ γ ij ∆ ˜
ψ + 6α ψ 2
˜ D i ψ ˜ D j ψ − 1
3 γ ˜ ij D ˜ k ψ ˜ D k ψ
− ˜ D i D ˜ j − 1 3 ˜ γ ij ∆ ˜
α − 2 ψ
˜ D i ψ ˜ D j α + ˜ D j ψ ˜ D i α − 2
3 γ ˜ ij D ˜ k ψ ˜ D k α i + 2α 2
K ˜ A ij − 2 ˜ A il A ˜ l j + 2α
β , i m A ˜ mj + β m ,j A ˜ mi − 2
3 β m ,m A ˜ ij
− 16π α 2 ψ 4
S ij − 1
3 γ ij S l l
− ∂
∂n
β m ,i γ ˜ mj + β m ,j γ ˜ mi − 2 3 β m ,m γ ˜ ij
+ 2 ∂α
∂n A ˜ ij
≡τ ij .
(2.13)
Thus, (4) h ij in the near zone is determined from
∆ f lat(4) h ij = (4) τ ij , (2.14)
while (5) h ij in the near zone is derived from
(5) h ij (t) = 1 4π
∂
∂t Z
(4) τ ij (t, y)d 3 y. (2.15) This integral is evaluated so that we obtain [6,8]
(5) h ij (t) = − 4 5
d 3 dt 3
I ij − 1
3 δ ij I kk
, (2.16)
where I ij = R ρx i x j d 3 x.
Up to the 2.5PN order, the hydrodynamic equations become
∂S i
∂t + ∂(S i v j )
∂x j = −
1 + 2U + 5
4 U 2 + 6 (4) ψ + X P ,i + ρ ∗ h
U ,i
n
1 + ε + P ρ + 3
2 v 2 − U + 5
8 v 4 + 4v 2 U + 3
2 v 2 − U
ε + P ρ
+ 3 (3) β j v j o
− X ,i
1 + ε + P ρ + v 2
2
+ 2v 2 (4) ψ ,i − (6) α ,i − (7) α ,i
+ v j n
(3) β j,i
1 + ε + P ρ + v 2
2 + 3U
+ (5) β j,i + (6) β j,i
o
+ (3) β j (3) β j,i
+ 1
2 v j v k ( (4) h jk,i + (5) h jk,i ) + O(c −8 ) i
, (2.17)
∂H
∂t + ∂(Hv j )
∂x j = − P h
v j ,j + ∂
∂t
1
2 v 2 + 3U + ∂
∂x j n 1
2 v 2 + 3U v j o
+ O(c −5 ) i
, (2.18)
where S i = αψ 6 (ρ + ρε + P )u 0 u i , S 0 = αψ 6 (ρ + ρε + P )(u 0 ) 2 and H = αψ 6 ρεu 0 .
3. Strategy to obtain 2PN tensor potential. We describe methods to solve the equation for the 2PN tensor potential (4) h ij . Although Eq.(2.14) is formally solved as
(4) h ij (t, x) = − 1 4π
Z (4) τ ij (t, y)
|x − y| d 3 y, (3.1)
it seems difficult to estimate this integral in practice since (4) τ ij → O(r −3 ) for r → ∞ and the integral is taken all over the space. Thus it is desirable to replace this equation by some tractable forms in numerical evaluation. In the following, we show two approaches:
In section 3.1, we change Eq. (3.1) into the form in which the integration is performed only over the matter distribution like the Newtonian potential. In section 3.2, we propose a method to solve Eq. (2.14) as a boundary value problem.
Direct integration method. The explicit form of (4) τ ij is
(4) τ ij = − 2 ˆ ∂ ij (X + 2 (4) ψ) + U ˆ ∂ ij U − 3U ,i U ,j + δ ij U ,k U ,k − 16π
ρv i v j − 1
3 δ ij ρv 2
−
(3) β ˙ i,j + (3) β ˙ j,i − 2
3 δ ij (3) β ˙ k,k
, (3.2)
where ˆ ∂ ij ≡ ∂x ∂
i∂x
2 j− 1 3 δ ij ∆ f lat . Since (3) β ˙ i is written as
(3) β ˙ i = ˙ p i − (X + 2 (4) ψ) ,i − n Z
ρv 2 + 3P − ρU/2
|x − y| d 3 y o
,i
, (3.3)
the source term, (4) τ ij , is split into five parts (4) τ ij = (4) τ ij (S) + (4) τ ij (U ) + (4) τ ij (C) + (4) τ ij (ρ) +
(4) τ ij (V ) , where we introduce
(4) τ ij (S) = − 16π
ρv i v j − 1
3 δ ij ρv 2 ,
(4) τ ij (U ) =U U ,ij − 1
3 δ ij U ∆ f lat U − 3U ,i U ,j + δ ij U ,k U ,k ,
(4) τ ij (C) =4 ∂
∂x j
Z (ρv i ) ·
|x − y| d 3 y + 4 ∂
∂x i
Z (ρv j ) ·
|x − y| d 3 y − 8 3 δ ij
∂
∂x k
Z (ρv k ) ·
|x − y| d 3 y,
(4) τ ij (ρ) = ˆ ∂ ij
Z
¨
ρ|x − y|d 3 y,
(4) τ ij (V ) =2 ˆ ∂ ij
Z
ρv 2 + 3P − ρU/2
|x − y| d 3 y.
(3.4)
Thus it becomes clear that (4) h ij and (5) h ij are expressed in terms of only matter vari- ables, without metric, through (4) τ ij and thus they do not depend on slicing conditions.
Then we define (4) h (∗) ij = ∆ −1 f lat(4) τ ij (∗) where the symbol ‘∗’ denotes S, U , C, ρ and V . First, since (4) τ ij (S) is a compact source, we immediately obtain
(4) h (S) ij = 4 Z
ρv i v j − 1 3 δ ij ρv 2
|x − y| d 3 y. (3.5)
Second, we consider the following equation
∆ f lat G(x, y 1 , y 2 ) = 1
|x − y 1 ||x − y 2 | . (3.6) It is possible to write (4) h (U ) ij as integrals over the matter using the function G. Eq. (3.6) has solutions [9], ln(r 1 + r 2 ± r 12 ), where r 1 = |x − y 1 |, r 2 = |x − y 2 |, r 12 = |y 1 − y 2 |. Note that ln(r 1 +r 2 −r 12 ) is not regular on the interval between y 1 and y 2 , while ln(r 1 +r 2 +r 12 ) is regular on the matter. Thus we use ln(r 1 + r 2 + r 12 ) as a Green function. Using this function, U U ,ij and U ,i U ,j are rewritten as
U U ,ij =∆ f lat
Z
d 3 y 1 d 3 y 2 ρ(y 1 )ρ(y 2 ) ∂ 2
∂y 1 i ∂y 1 j ln(r 1 + r 2 + r 12 ), U ,i U ,j =∆ f lat
Z
d 3 y 1 d 3 y 2 ρ(y 1 )ρ(y 2 ) ∂ 2
∂y 1 i ∂y 2 j ln(r 1 + r 2 + r 12 ).
(3.7)
Thus we can express (4) h (U ) ij using the integral over the matter as
(4) h (U ) ij = Z
d 3 y 1 d 3 y 2 ρ(y 1 )ρ(y 2 ) h ∂ 2
∂y 1 i ∂y j 1 − 1 3 δ ij 4 1
−3 ∂ 2
∂y 1 i ∂y 2 j − 1 3 δ ij 4 12
i ln(r 1 +r 2 +r 12 ), (3.8)
where we introduce 4 1 = ∂y ∂
k21
∂y
1kand 4 12 = ∂y ∂
k21