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Stable numerical simulation of Einstein equations
in gravitational collapse space–time

Takuya Tsuchiya [email protected] Center for Liberal Arts and Sciences, Hachinohe Institute of Technology, Japan Ryosuke Urakawa Waseda University Advanced Research Institute for Science and Engineering, Japan Gen Yoneda Graduate School of Fundamental Science and Engineering, Waseda University, Japan
Abstract

We perform simulations in a gravitational collapsing model using the Einstein equations. In this paper, we review the equations for constructing the initial values and the evolution form of the Einstein equations called the BSSN formulation. In addition, since we treat a nonvacuum case, we review the evolution equations of the matter fields of a perfect fluid. To make the simulations stable, we propose a modified system, which decreases numerical errors in analysis, and we actually perform stable simulations with decreased numerical errors.

1 Introduction

Numerical relativity, which solves the Einstein equations numerically, has been widely studied [1, 2, 3, 4]. In particular, for the direct observation of gravitational waves (e.g., [5]), numerical relativity makes important contributions.

Stable numerical simulations are important to clarify the details of phenomena. Since the Einstein equations are the nonlinear partial differential equations, numerical errors tend to accumulate. Although there are some research studies to reduce the numerical errors, they are mainly in the vacuum case. Thus, we suggest a modified system to reduce numerical errors by modifying the evolution equation in a perfect fluid.

The structure of this paper is as follows. We review the space–time decomposition of the Einstein equations in a perfect fluid in Sec. 2. In Sec. 3, we introduce the equations for the numerical simulations of the Einstein equations as the initial value problem in the perfect fluid. We perform some simulations in the dust case and propose a modified system to reduce the numerical errors in Sec. 4. We summarize this paper in Sec. 5. In this paper, indices such as (μ,ν,λ,)(\mu,\nu,\lambda,\cdots) and (i,j,k,)(i,j,k,\cdots) run from 0 to 3 and 1 to 3, respectively. We use the Einstein convention of summation of repeated up–down indices.

2 Abstract for numerical simulations of Einstein equations in perfect fluid

The Einstein equations are as follows.

Rμν(4)12R(4)gμν=8πTμν,\displaystyle{}^{(4)}R_{\mu\nu}-\dfrac{1}{2}{}^{(4)}Rg_{\mu\nu}=8\pi T_{\mu\nu}, (1)

where gμνg_{\mu\nu} is the four-dimensional metric, Rμν(4){}^{(4)}R_{\mu\nu} is the four-dimensional Ricci tensor, R(4)gμνRμν(4){}^{(4)}R\equiv g^{\mu\nu}{}^{(4)}R_{\mu\nu}, gμνg^{\mu\nu} is the inverse of gμνg_{\mu\nu}, and TμνT_{\mu\nu} is the stress–energy tensor. Eq. (1) is not a dynamical form because the time and space components are mixed. Generally, we often carry out space–time decomposition of Eq. (1) for performing the simulations.

There are some dynamical forms of Eq. (1), the most basic formulation is the ADM formulation [6, 7]:

tγij\displaystyle\partial_{t}\gamma_{ij} =2αKij+γjm(Diβm)+γim(Djβm),\displaystyle=-2\alpha K_{ij}+\gamma_{jm}(D_{i}\beta^{m})+\gamma_{im}(D_{j}\beta^{m}), (2)
tKij\displaystyle\partial_{t}K_{ij} =DiDjα+αRij+αKKij2αγmnKmiKnj\displaystyle=-D_{i}D_{j}\alpha+\alpha R_{ij}+\alpha KK_{ij}-2\alpha\gamma^{mn}K_{mi}K_{nj}
8παSij+4παSγij4παρHγij+β(DKij)\displaystyle\quad-8\pi\alpha S_{ij}+4\pi\alpha S\gamma_{ij}-4\pi\alpha\rho_{\text{H}}\gamma_{ij}+\beta^{\ell}(D_{\ell}K_{ij})
+Ki(Djβ)+Kj(Diβ),\displaystyle\quad+K_{\ell i}(D_{j}\beta^{\ell})+K_{\ell j}(D_{i}\beta^{\ell}), (3)
\displaystyle\mathcal{H} R+K2γimγnjKijKmn16πρH0,\displaystyle\equiv R+K^{2}-\gamma^{im}\gamma^{nj}K_{ij}K_{mn}-16\pi\rho_{\text{H}}\approx 0, (4)
i\displaystyle\mathcal{M}_{i} γjm(DjKmi)DiK8πJi0,\displaystyle\equiv\gamma^{jm}(D_{j}K_{mi})-D_{i}K-8\pi J_{i}\approx 0, (5)

where γijgij\gamma_{ij}\equiv g_{ij} is the induced metric, γij\gamma^{ij} is the inverse of γij\gamma_{ij}, and KijK_{ij} is the extrinsic curvature defined as Eq. (2). α1/g00\alpha\equiv 1/\sqrt{-g^{00}} and βiα2g0i\beta^{i}\equiv\alpha^{2}g^{0i} are the lapse function and the shift vector, respectively. DiD_{i} is the covariant derivative associated with γij\gamma_{ij}, RijR_{ij} is the Ricci tensor in three dimensions, KγijKijK\equiv\gamma^{ij}K_{ij}, and RγijRijR\equiv\gamma^{ij}R_{ij}. ρHα2g0μg0νTμν\rho_{\mathrm{H}}\equiv\alpha^{2}g^{0\mu}g^{0\nu}T_{\mu\nu} is the mass density, Jiαg0μTμiJ_{i}\equiv\alpha g^{0\mu}T_{\mu i} is the momentum density, SijTijS_{ij}\equiv T_{ij} is the stress tensor, and SγijSijS\equiv\gamma^{ij}S_{ij}. \mathcal{H} and i\mathcal{M}_{i} are the Hamiltonian constraint and the momentum constraint, respectively. The symbol \approx means zero in the mathematical sense but nonzero in the numerical sense.

In the calculation in the nonvacuum case, we also solve the evolution equations of matter fields. These equations are given by the space–time decomposition of gμλ(μTλν)=0g^{\mu\lambda}(\nabla_{\mu}T_{\lambda\nu})=0, where μ\nabla_{\mu} is the covariant derivative associated with gμνg_{\mu\nu}. For the perfect fluid case, the stress–energy tensor is given as

Tμν={ρ(1+ϵ)+p}gμλgνωuλuω+pgμν,\displaystyle T_{\mu\nu}=\{\rho(1+\epsilon)+p\}g_{\mu\lambda}g_{\nu\omega}u^{\lambda}u^{\omega}+pg_{\mu\nu}, (6)

where ρ\rho is the rest mass, ϵ\epsilon is the inner energy, uμu^{\mu} is the four velocity, and pp is the pressure. The evolution equations of ϵ\epsilon and ρui\rho u^{i} are given by gμλ(μTλν)=0g^{\mu\lambda}(\nabla_{\mu}T_{\lambda\nu})=0. The evolution equation of ρ\rho is given by the continuous equation μ(ρuμ)=0\nabla_{\mu}(\rho u^{\mu})=0. On the other hand, pp is usually given by other conditions such as the equation of state.

3 Basic equations

3.1 Equations for initial values

If we set the initial values, they have to satisfy the constraints \mathcal{H} and i\mathcal{M}_{i}. The dynamical variables γij\gamma_{ij} and KijK_{ij} include 12 components because they are symmetric tensors. However, there are only four constraints. Thus, according to [8], we reformulate the constraints such that

γ^ij(D^iD^jψ)\displaystyle\hat{\gamma}^{ij}(\hat{D}_{i}\hat{D}_{j}\psi) =18ψR^+112ψ5K22πψ5ρH\displaystyle=\frac{1}{8}\psi\hat{R}+\frac{1}{12}\psi^{5}K^{2}-2\pi\psi^{5}\rho_{\text{H}}
18ψ7γ^imγ^jnA^ijA^mn,\displaystyle\quad-\frac{1}{8\psi^{7}}\hat{\gamma}^{im}\hat{\gamma}^{jn}\hat{A}_{ij}\hat{A}_{mn}, (7)
γ^jm(D^jD^mXi)\displaystyle\hat{\gamma}^{jm}(\hat{D}_{j}\hat{D}_{m}X_{i}) =13γ^jm(D^iD^jXm)+23ψ6(D^iK)\displaystyle=-\frac{1}{3}\hat{\gamma}^{jm}(\hat{D}_{i}\hat{D}_{j}X_{m})+\frac{2}{3}\psi^{6}(\hat{D}_{i}K)
R^ijγ^jmXm+8πψ6Ji,\displaystyle\quad-\hat{R}_{ij}\hat{\gamma}^{jm}X_{m}+8\pi\psi^{6}J_{i}, (8)

where A^ijψ2(Kij(1/3)Kψ4γ^ij)\hat{A}_{ij}\equiv\psi^{2}(K_{ij}-(1/3)K\psi^{4}\hat{\gamma}_{ij}), ψ\psi satisfies relations such as γij=ψ4γ^ij\gamma_{ij}=\psi^{4}\hat{\gamma}_{ij}, and XiX_{i} satisfies the relation D^iXj+D^jXi(2/3)γ^mn(D^nXm)γ^ij=A^ij\hat{D}_{i}X_{j}+\hat{D}_{j}X_{i}-(2/3)\hat{\gamma}^{mn}(\hat{D}_{n}X_{m})\hat{\gamma}_{ij}=\hat{A}_{ij}. D^i\hat{D}_{i} is the covariant derivative associated with γ^ij\hat{\gamma}_{ij}, R^ij\hat{R}_{ij} is the Ricci tensor of γ^ij\hat{\gamma}^{ij}, and R^γ^ijR^ij\hat{R}\equiv\hat{\gamma}^{ij}\hat{R}_{ij}. We often assume γ^ij=δij\hat{\gamma}_{ij}=\delta_{ij} and K=0K=0. Then, we set a suitable boundary condition, and we solve Eqs. (7)–(8).

The Einstein equations are not satisfied by simply giving the dynamical variables (γij,Kij)(\gamma_{ij},K_{ij}) at the initial time. We have to give the gauge variables (α,βi)(\alpha,\beta^{i}) as appropriate values. For the lapse function α\alpha, we assume K=0K=0 and tK=0\partial_{t}K=0 in Eqs. (2)–(4), and we obtain

γ^ij(D^iD^jα)\displaystyle\hat{\gamma}^{ij}(\hat{D}_{i}\hat{D}_{j}\alpha) =2ψ1γ^ij(D^jψ)(D^iα)+4παψ4ρH\displaystyle=-2\psi^{-1}\hat{\gamma}^{ij}(\hat{D}_{j}\psi)(\hat{D}_{i}\alpha)+4\pi\alpha\psi^{4}\rho_{\text{H}}
+αψ8γ^miγ^jnA^ijA^mn+4πψ4αS.\displaystyle\quad+\alpha\psi^{-8}\hat{\gamma}^{mi}\hat{\gamma}^{jn}\hat{A}_{ij}\hat{A}_{mn}+4\pi\psi^{4}\alpha S. (9)

This is called the maximal slicing condition [9]. For the shift vector βi\beta^{i}, the minimal distortion gauge condition [7] is often used. We solve the nonlinear elliptic-type Eqs. (7)–(9), obtain (ψ,X^i,α)(\psi,\hat{X}_{i},\alpha), and then get (α,γij,Kij)(\alpha,\gamma_{ij},K_{ij}) at the initial time.

3.2 Evolution equations and constraint equations

Since it is well known that the numerical simulations using Eqs. (2)–(3) are unstable, we should reformulate the evolution equations. The BSSN formulation [10, 11] is one of the formulations most commonly used by numerical relativists. The dynamical variables are (φ,K,γ~ij,A~ij,Γ~i)(\varphi,K,\tilde{\gamma}_{ij},\tilde{A}_{ij},\tilde{\Gamma}^{i}) instead of (γij,Kij)(\gamma_{ij},K_{ij}), where φ=(1/12)log(det(γij))\varphi=(1/12)\log(\text{det}(\gamma_{ij})), γ~ij=e4φγij\tilde{\gamma}_{ij}=e^{-4\varphi}\gamma_{ij}, K=γijKijK=\gamma^{ij}K_{ij}, A~ij=e4φ(Kij(1/3)Kγij)\tilde{A}_{ij}=e^{-4\varphi}(K_{ij}-(1/3)K\gamma_{ij}), Γ~=Γ~γ~ijij\tilde{\Gamma}^{\ell}=\tilde{\Gamma}^{\ell}{}_{ij}\tilde{\gamma}^{ij}, γ~ij\tilde{\gamma}^{ij} is the inverse of γ~ij\tilde{\gamma}_{ij}, and Γ~ij\tilde{\Gamma}^{\ell}{}_{ij} is the connection coefficient of γ~ij\tilde{\gamma}_{ij}. The evolution equations are

tφ\displaystyle\partial_{t}\varphi =16αK+16(iβi)+βi(iφ),\displaystyle=-\frac{1}{6}\alpha K+\frac{1}{6}(\partial_{i}\beta^{i})+\beta^{i}(\partial_{i}\varphi), (10)
tK\displaystyle\partial_{t}K =(DiDjα)e4φγ~ij+13αK2+4παS\displaystyle=-(D_{i}D_{j}\alpha)e^{-4\varphi}\tilde{\gamma}^{ij}+\frac{1}{3}\alpha K^{2}+4\pi\alpha S
+αA~ijA~mnγ~imγ~jn+4παρH+βi(iK),\displaystyle\quad+\alpha\tilde{A}_{ij}\tilde{A}_{mn}\tilde{\gamma}^{im}\tilde{\gamma}^{jn}+4\pi\alpha\rho_{\text{H}}+\beta^{i}(\partial_{i}K), (11)
tγ~ij\displaystyle\partial_{t}\tilde{\gamma}_{ij} =2αA~ij23(β)γ~ij+(iβ)γ~j+(jβ)γ~i\displaystyle=-2\alpha\tilde{A}_{ij}-\frac{2}{3}(\partial_{\ell}\beta^{\ell})\tilde{\gamma}_{ij}+(\partial_{i}\beta^{\ell})\tilde{\gamma}_{\ell j}+(\partial_{j}\beta^{\ell})\tilde{\gamma}_{\ell i}
+β(γij),\displaystyle\quad+\beta^{\ell}(\partial_{\ell}\gamma_{ij}), (12)
tA~ij\displaystyle\partial_{t}\tilde{A}_{ij} =(DiDjα)TFe4φ2αA~imA~jnγ~mn+αKA~ij\displaystyle=-(D_{i}D_{j}\alpha)^{\rm TF}e^{-4\varphi}-2\alpha\tilde{A}_{im}\tilde{A}_{jn}\tilde{\gamma}^{mn}+\alpha K\tilde{A}_{ij}
+αe4φRijTF8παe4φSijTF23(β)A~ij\displaystyle\quad+\alpha e^{-4\varphi}R^{\rm TF}_{ij}-8\pi\alpha e^{-4\varphi}S_{ij}^{\rm TF}-\dfrac{2}{3}(\partial_{\ell}\beta^{\ell})\tilde{A}_{ij}
+(iβ)A~j+(jβ)A~i+β(A~ij),\displaystyle\quad+(\partial_{i}\beta^{\ell})\tilde{A}_{\ell j}+(\partial_{j}\beta^{\ell})\tilde{A}_{\ell i}+\beta^{\ell}(\partial_{\ell}\tilde{A}_{ij}), (13)
tΓ~\displaystyle\partial_{t}\tilde{\Gamma}^{\ell} =2(iα)A~mjγ~ijγ~m+2αΓ~A~ijmnγ~miγ~nj\displaystyle=-2(\partial_{i}\alpha)\tilde{A}_{mj}\tilde{\gamma}^{ij}\tilde{\gamma}^{m\ell}+2\alpha\tilde{\Gamma}^{\ell}{}_{mn}\tilde{A}_{ij}\tilde{\gamma}^{mi}\tilde{\gamma}^{nj}
+12α(iφ)A~i43αγ~i(iK)16παγ~iJi\displaystyle\quad+12\alpha(\partial_{i}\varphi)\tilde{A}^{i\ell}-\dfrac{4}{3}\alpha\tilde{\gamma}^{\ell i}(\partial_{i}K)-16\pi\alpha\tilde{\gamma}^{i\ell}J_{i}
+13(ijβj)γ~i+(ijβ)γ~ij+23(iβi)Γ~\displaystyle\quad+\dfrac{1}{3}(\partial_{i}\partial_{j}\beta^{j})\tilde{\gamma}^{\ell i}+(\partial_{i}\partial_{j}\beta^{\ell})\tilde{\gamma}^{ij}+\dfrac{2}{3}(\partial_{i}\beta^{i})\tilde{\Gamma}^{\ell}
(iβ)Γ~i+βi(iΓ~),\displaystyle\quad-(\partial_{i}\beta^{\ell})\tilde{\Gamma}^{i}+\beta^{i}(\partial_{i}\tilde{\Gamma}^{\ell}), (14)

where RijR_{ij} in the above is defined as

Rij\displaystyle R_{ij} 12γ~m(mγ~ij)+12γ~mi(jΓ~m)+12γ~mj(iΓ~m)\displaystyle\equiv-\frac{1}{2}\tilde{\gamma}^{\ell m}(\partial_{\ell}\partial_{m}\tilde{\gamma}_{ij})+\dfrac{1}{2}\tilde{\gamma}_{mi}(\partial_{j}\tilde{\Gamma}^{m})+\dfrac{1}{2}\tilde{\gamma}_{mj}(\partial_{i}\tilde{\Gamma}^{m})
+12γ~iΓ~Γ~mjm+12γ~jΓ~Γ~mim+γ~mnγ~kΓ~Γ~knjmi\displaystyle\quad+\dfrac{1}{2}\tilde{\gamma}_{i\ell}\tilde{\Gamma}^{\ell}{}_{jm}\tilde{\Gamma}^{m}+\dfrac{1}{2}\tilde{\gamma}_{j\ell}\tilde{\Gamma}^{\ell}{}_{im}\tilde{\Gamma}^{m}+\tilde{\gamma}^{mn}\tilde{\gamma}_{\ell k}\tilde{\Gamma}^{\ell}{}_{nj}\tilde{\Gamma}^{k}{}_{mi}
+γ~mnγ~kjΓ~Γ~kni+mγ~mnγ~kiΓ~Γ~knjm\displaystyle\quad+\tilde{\gamma}^{mn}\tilde{\gamma}_{kj}\tilde{\Gamma}^{\ell}{}_{ni}\tilde{\Gamma}^{k}{}_{\ell m}+\tilde{\gamma}^{mn}\tilde{\gamma}_{ki}\tilde{\Gamma}^{\ell}{}_{nj}\tilde{\Gamma}^{k}{}_{\ell m}
2(D~jD~iφ)2γ~mn(D~mD~nφ)γ~ij+4(D~iφ)(D~jφ)\displaystyle\quad-2(\tilde{D}_{j}\tilde{D}_{i}\varphi)-2\tilde{\gamma}^{mn}(\tilde{D}_{m}\tilde{D}_{n}\varphi)\tilde{\gamma}_{ij}+4(\tilde{D}_{i}\varphi)(\tilde{D}_{j}\varphi)
4γ~mn(D~mφ)(D~nφ)γ~ij.\displaystyle\quad-4\tilde{\gamma}^{mn}(\tilde{D}_{m}\varphi)(\tilde{D}_{n}\varphi)\tilde{\gamma}_{ij}. (15)

The symbol TF means the trace-free part of the value, and D~i\tilde{D}_{i} is the covariant derivative associated with γ~ij\tilde{\gamma}_{ij}. The constraint equations are

~\displaystyle\tilde{\mathcal{H}} R+23K2A~ijA~mnγ~imγ~jn16πρH0,\displaystyle\equiv R+\frac{2}{3}K^{2}-\tilde{A}_{ij}\tilde{A}_{mn}\tilde{\gamma}^{im}\tilde{\gamma}^{jn}-16\pi\rho_{\text{H}}\approx 0, (16)
~i\displaystyle\tilde{\mathcal{M}}_{i} γ~jn(D~jA~ni)+6(D~jφ)γ~jnA~ni23D~iK\displaystyle\equiv\tilde{\gamma}^{jn}(\tilde{D}_{j}\tilde{A}_{ni})+6(\tilde{D}_{j}\varphi)\tilde{\gamma}^{jn}\tilde{A}_{ni}-\frac{2}{3}\tilde{D}_{i}K
8πJi0,\displaystyle\quad-8\pi J_{i}\approx 0, (17)
𝒮~\displaystyle\tilde{\mathcal{S}} det(γ~ij)10,\displaystyle\equiv\text{det}(\tilde{\gamma}_{ij})-1\approx 0, (18)
𝒜~\displaystyle\tilde{\mathcal{A}} γ~ijA~ij0,\displaystyle\equiv\tilde{\gamma}^{ij}\tilde{A}_{ij}\approx 0, (19)
𝒢~\displaystyle\tilde{\mathcal{G}}^{\ell} Γ~Γ~γ~ijij0.\displaystyle\equiv\tilde{\Gamma}^{\ell}-\tilde{\Gamma}^{\ell}{}_{ij}\tilde{\gamma}^{ij}\approx 0. (20)

Recently, other formulations have also been used [12, 13] by numerical relativists.

3.3 Evolution equations of matter fields

For the perfect fluid, the evolution equations of matter fields [14] are given by the space–time decomposition of μ(ρuμ)=0\nabla_{\mu}(\rho u^{\mu})=0 and gμλ(μTλν)=0g^{\mu\lambda}(\nabla_{\mu}T_{\lambda\nu})=0 as

tρ\displaystyle\partial_{t}\rho_{*} =i(ρvi),\displaystyle=-\partial_{i}(\rho_{*}v^{i}), (21)
te\displaystyle\partial_{t}e_{*} =i(evi),\displaystyle=-\partial_{i}(e_{*}v^{i}), (22)
t(ρu^i)\displaystyle\partial_{t}(\rho_{*}\hat{u}_{i}) =j(ρu^ivj)αe6φ(ip)ρ(iα)hw\displaystyle=-\partial_{j}\left(\rho_{*}\hat{u}_{i}v^{j}\right)-\alpha e^{6\varphi}(\partial_{i}p)-\rho_{*}(\partial_{i}\alpha)hw
+ρ(iβn)u^n12hwραe4φ(iγ~mn)u^mu^n\displaystyle\quad+\rho_{*}(\partial_{i}\beta^{n})\hat{u}_{n}-\frac{1}{2hw}\rho_{*}\alpha e^{-4\varphi}(\partial_{i}\tilde{\gamma}^{mn})\hat{u}_{m}\hat{u}_{n}
+2h(w21)w1ρα(iφ),\displaystyle\quad+2h(w^{2}-1)w^{-1}\rho_{*}\alpha(\partial_{i}\varphi), (23)

where ρρwe6φ\rho_{*}\equiv\rho we^{6\varphi}, wαu0w\equiv\alpha u^{0}, e(ρϵ)1/Γe6φwe_{*}\equiv(\rho\epsilon)^{1/\Gamma}e^{6\varphi}w, viui/u0v^{i}\equiv u^{i}/u^{0}, h1+ϵ+p/ρh\equiv 1+\epsilon+p/\rho, u^ihe4φγ~ij(u0βj+uj)\hat{u}_{i}\equiv he^{-4\varphi}\tilde{\gamma}_{ij}(u^{0}\beta^{j}+u^{j}), and Γ\Gamma is a constant. In addition, we assume p=(Γ1)ρϵp=(\Gamma-1)\rho\epsilon. The relations between (ρH,Ji,Sij)(\rho_{\text{H}},J_{i},S_{ij}) and (ρ,e,u^i)(\rho_{*},e_{*},\hat{u}_{i}) are

ρH\displaystyle\rho_{\text{H}} =e6φhρwp,\displaystyle=e^{-6\varphi}h\rho_{*}w-p, (24)
Ji\displaystyle J_{i} =ρu^ie6φ,\displaystyle=\rho_{*}\hat{u}_{i}e^{-6\varphi}, (25)
Sij\displaystyle S_{ij} =e6φw1h1ρu^iu^j+pe4φγ~ij.\displaystyle=e^{-6\varphi}w^{-1}h^{-1}\rho_{*}\hat{u}_{i}\hat{u}_{j}+pe^{4\varphi}\tilde{\gamma}_{ij}. (26)

Since the four velocity uμu^{\mu} is satisfied in the relation uμuμ=1u^{\mu}u_{\mu}=-1, ww is given as w=1+h2e4φγ~iju^iu^jw=\sqrt{1+h^{-2}e^{-4\varphi}\tilde{\gamma}^{ij}\hat{u}_{i}\hat{u}_{j}}. In addition, for p=(Γ1)ρϵp=(\Gamma-1)\rho\epsilon, hh is given as h=1+Γeρ1(ew1e6φ)Γ1h=1+\Gamma e_{*}\rho_{*}^{-1}(e_{*}w^{-1}e^{-6\varphi})^{\Gamma-1}.

4 Numerical simulations

In the dust case, we solve the Einstein equations and the matter evolution equations. With reference to [14], we set the initial data as follows.

ρ=a(1+exp(r2r02δr2))1,\displaystyle\rho_{*}=a\left(1+\exp\left(\dfrac{r^{2}-r_{0}^{2}}{\delta r^{2}}\right)\right)^{-1}, (27)

where aa is the gravitational mass Mg=d3x(ρHψ5+(1/16π)ψ7A^ijA^mnγ^imγ^jn)M_{g}=\int d^{3}x(\rho_{\text{H}}\psi^{5}+(1/16\pi)\psi^{-7}\hat{A}_{ij}\hat{A}_{mn}\hat{\gamma}^{im}\hat{\gamma}^{jn}) as the unit at the initial time and r=x2+y2+z2r=\sqrt{x^{2}+y^{2}+z^{2}}. This time, we set a=4.129×103a=4.129\times 10^{-3}, δr2=0.18Mg2\delta r^{2}=0.18M_{g}^{2}, and r0=4.0Mgr_{0}=4.0M_{g}. The numerical ranges are 9x,y,z9-9\leq x,y,z\leq 9. This case is static at the initial time, so we set Xi=A^ij=Ji=βi=ui=0X_{i}=\hat{A}_{ij}=J_{i}=\beta^{i}=u^{i}=0. In the dust case, we set the inner energy as ϵ=0\epsilon=0 and the pressure p=0p=0. We assume γ^ij=δij\hat{\gamma}_{ij}=\delta_{ij} and K=0K=0. Then, the extrinsic curvature Kij=0K_{ij}=0 and R^=0\hat{R}=0. We obtain the initial data (α,γij)(\alpha,\gamma_{ij}) with the above conditions by solving Eqs. (7) and (9). With reference to the Schwarzschild metric, the initial step values of ψ\psi and α\alpha are set as 1+1/(1+6r)1+1/(1+6r) and 11/(3/2+r)1-1/(3/2+r), respectively.

Recently, the maximal slicing condition, Eq. (9), and the minimal distortion gauge condition are almost never used in the evolution because the numerical costs are high. The evolution equation of α\alpha often uses the 1+log1+\log slicing condition [15],

tα=2αK.\displaystyle\partial_{t}\alpha=-2\alpha K. (28)

Since this condition has the characteristic of singularity avoidance, it is widely used in the simulations for the gravitational collapse models. We choose βi=0\beta^{i}=0. For the rotating models of neutron stars and/or black holes, the Gamma-driver condition [16] is often used in the evolution equations of βi\beta^{i}.

This time, we select the grid as Δx=Δy=Δz=1/60\Delta x=\Delta y=\Delta z=1/60, Δt=1/240\Delta t=1/240, and the boundary condition as the approximate asymptotic flat boundary. We use the fourth-order Runge–Kutta scheme with mainly the second-order centered space difference. However, for only the advection term, which is the first term on the right-hand side in each of Eqs. (21)–(23), we use the second-order upwind scheme. The direction is defined by the signature of the velocity viv^{i}.

Refer to caption
Figure 1: ρ\rho_{*} of x=y=0.45x=y=-0.45 obtained by solving Eqs. (10)–(14), Eqs. (21)–(23), and Eq. (28). The horizontal line is zz, the vertical line is ρ\rho_{*}. The line of t=12t=12 satisfies ρ0\rho_{*}\geq 0. On the other hand, we see that ρ<0\rho_{*}<0 in 2<z<2-2<z<2 at t=13t=13.

Fig. 1 shows the weighted rest mass ρ\rho_{*} at t=12t=12 and t=13t=13 obtained by solving Eqs. (10)–(14), Eqs. (21)–(23), and Eq. (28). We see that ρ<0\rho_{*}<0 at t=13t=13 in the 2<z<2-2<z<2 range. We check ρ0\rho_{*}\geq 0 during 0t120\leq t\leq 12 in all the simulation ranges. Since ρ0\rho_{*}\geq 0 is a necessary condition for successful simulations, this simulation fails after t=13t=13.

For more stable simulations, we modify Eq. (23) as

t(ρu^i)\displaystyle\partial_{t}(\rho_{*}\hat{u}_{i}) =[Original terms]+κργ~mn(mn~i),\displaystyle=[\text{Original terms}]+\kappa\rho_{*}\tilde{\gamma}^{mn}(\partial_{m}\partial_{n}\tilde{\mathcal{M}}_{i}), (29)

where κ\kappa is a damping parameter. This modification is based on the following ideas. By using this modification, we obtain the following: (i) the positive rest mass condition ρ0\rho_{*}\geq 0 is satisfied, (ii) the constraints, Eqs. (16)–(20), are conserved, and (iii) the total weighted rest mass

I=ρd3x\displaystyle I=\int\rho_{*}d^{3}x (30)

is conserved. The negative sign of κ\kappa makes the simulations stable because the dynamical equations of ~i\tilde{\mathcal{M}}_{i} become

t~i\displaystyle\partial_{t}\tilde{\mathcal{M}}_{i} =[Original terms]8πκρe6φwγ~mn(mn~i)\displaystyle=[\text{Original terms}]-\dfrac{8\pi\kappa\rho_{*}}{e^{6\varphi}w}\tilde{\gamma}^{mn}(\partial_{m}\partial_{n}\tilde{\mathcal{M}}_{i}) (31)

because of the adjusted terms of Eq. (29). The adjusted term of Eq. (31) has the dissipation effect if κ<0\kappa<0 because ρ/(e6φw)0\rho_{*}/(e^{6\varphi}w)\geq 0. The set of Eqs. (10)–(14), Eqs. (21)–(22), Eq. (28), and Eq. (29) is called as the modified system hereafter.

Refer to caption
Figure 2: ρ\rho_{*} of x=y=0.45x=y=-0.45 with Eq. (29) and the other conditions are the same as those in Fig. 1. We set the damping parameter of Eq. (29) as κ=0.1\kappa=-0.1. The solid line for t=17t=17 satisfies ρ0\rho_{*}\geq 0. On the other hand, we see ρ<0\rho_{*}<0 in 2<z<2-2<z<2 at t=18t=18.

We show the numerical results of ρ\rho_{*} obtained using the modified system in Fig. 2. The numerical settings are consistent with those in Fig. 1 without the evolution equation of ρu^i\rho_{*}\hat{u}_{i} and we set κ=0.1\kappa=-0.1. For this simulation, we check ρ0\rho_{*}\geq 0 during 0t170\leq t\leq 17 in all simulation ranges. In Fig. 3, we show the L2 norm of the following values:

𝒞2=~2+γ~ij~i~j+γ~ij𝒢~i𝒢~j+𝒮~2+𝒜~2.\displaystyle\mathcal{C}^{2}=\tilde{\mathcal{H}}^{2}+\tilde{\gamma}^{ij}\tilde{\mathcal{M}}_{i}\tilde{\mathcal{M}}_{j}+\tilde{\gamma}_{ij}\tilde{\mathcal{G}}^{i}\tilde{\mathcal{G}}^{j}+\tilde{\mathcal{S}}^{2}+\tilde{\mathcal{A}}^{2}. (32)

We see that the norm of the constraints 𝒞2\mathcal{C}^{2} with κ=0.1\kappa=-0.1 is less than those in other cases until 0t170\leq t\leq 17. On the other hand, the norm with κ=0.1\kappa=0.1 is larger than those in other cases. Thus, these results are consistent with the analytical results using Eq. (31). Fig. 4 shows the relative errors against the initial values of the total weighted mass II in Eq. (30). They are not markedly different between the cases of κ=0.0\kappa=0.0 and κ=0.1\kappa=-0.1.

Refer to caption
Figure 3: The lines show the constraint errors in the cases of κ=0.0\kappa=0.0, 0.1-0.1, and 0.10.1. The horizontal axis is time, and the vertical axis is the logarithm of the L2 norm of 𝒞2\mathcal{C}^{2}, Eq. (32).
Refer to caption
Figure 4: The lines show the relative errors of the total weighted rest mass II in Eq. (30) against the initial values I(0)I(0) for the cases of κ=0.0\kappa=0.0, 0.1-0.1, and 0.10.1. The horizontal axis is time, and the vertical axis is the logarithm of |(I(0)I(t))/I(0)||(I(0)-I(t))/I(0)|.

5 Summary

We reviewed the equations for construction of the initial values, the dynamical equations of the Einstein equations called the BSSN formulation, and the dynamical equations of the matter fields in the perfect fluid. With these equations, we performed the simulations in the dust case. We modified the system by modifying the evolution equations of the matter field, investigated the stability analytically, and performed the simulations with the modified system to confirm the consistency of the analytical results. In addition, the lifetime of the simulations was extended from t=12t=12 to t=17t=17 with the modification.

Acknowledgments

T.T. was partially supported by JSPS KAKENHI Grant Number 21K03354 and a Grant for Basic Science Research Projects from The Sumitomo Foundation. G.Y. and T.T. were partially supported by JSPS KAKENHI Grant Number 20K03740. G.Y. was partially supported by a Waseda University Grant for Special Research Projects 2021C-138.

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