This paper was converted on www.awesomepapers.org from LaTeX by an anonymous user.
Want to know more? Visit the Converter page.

Constraining energy-momentum-squared gravity by binary pulsar observations

Elham Nazari1 [email protected] (Corresponding Author)    Mahmood Roshan1,2 [email protected]    Ivan De Martino3 [email protected] 1Department of Physics, Faculty of Science, Ferdowsi University of Mashhad, P.O. Box 1436, Mashhad, Iran
2School of Astronomy, Institute for Research in Fundamental Sciences (IPM), P. O. Box 19395-5531, Tehran, Iran
3Universidad de Salamanca, Departamento de Fisica Fundamental, P. de la Merced, Salamanca, Spain
Abstract

In this paper, we introduce the post-Minkowskian approximation of energy-momentum-squared gravity (EMSG). This approximation is used to study the gravitational energy flux in the context of EMSG. As an application of our results, we investigate the EMSG effect on the first time derivative of the orbital period of the binary pulsars. Utilizing this post-Keplerian parameter, the free parameter of the EMSG theory, f0f_{0}^{\prime}, is estimated for six known binary pulsars. Taking the binaries that have the most accurate observations, it turns out that 6×1037ms2kg1<f0<+1036ms2kg1-6\times 10^{-37}\text{m}\,\text{s}^{2}\,\text{kg}^{-1}<f_{0}^{\prime}<+10^{-36}\text{m}\,\text{s}^{2}\,\text{kg}^{-1}. This bound is in agreement with the precedent studies.

I Introduction

There are several motivations behind attempts for generalizing the standard gravitational theory, namely the general theory of relativity (GR). These motivations come from both pure theoretical and also observational issues. For example, in the past decades, the dark energy enigma has been one of the main motivations to construct new gravity theories Clifton et al. (2012). An older motivation belongs to attempts for answering the dark matter problem without invoking any new particle Milgrom (1983); Salucci et al. (2021); de Martino et al. (2020). This story began by modifying the Newtonian dynamics. However, currently, there are covariant relativistic theories that in principle are significantly different from GR and claim at replacing dark matter by introducing corrections to GR, for example, see nonlocal gravity Hehl and Mashhoon (2009) and the scalar-tensor-vector-gravity theory Moffat (2006).

On the other hand, changing GR is not a simple task and there are serious restrictions on the deviations from GR. The recent detection of gravitational waves (GWs), already anticipated by GR, has provided a strong tool to rule out or constrain some modified gravity theories. It is necessary to mention that modified gravity theories mostly bring new gravitational fields in addition to the metric. This means that the dynamical/gravitational degrees of freedom is increased. Consequently, the equations governing the propagation of GWs are different, in principle, from GR. More importantly, the propagation speed of GWs can be different from that of the light speed. However, we know that the event GW170817 for GWs from a binary neutron star system Abbott et al. (2017a, b), proved that at least at redshift z0z\simeq 0, the fractional relative difference in propagation speeds of GWs (cWc_{W}) and light (cc) is less than 101510^{-15}. Therefore, modified theories that are incapable of satisfying cW=cc_{W}=c, are ruled out. For example, one may mention the covariant Galileon that has been ruled out by this implication Ezquiaga and Zumalacárregui (2017). There are other kinds of modified gravity theories which are still viable, e.g., see Boran et al. (2018).

Another pertinent test bed for modified theories of gravity is studying the post-Keplerian parameters associated with binary pulsars De Laurentis and De Martino (2013); De Laurentis and Capozziello (2011); De Laurentis and De Martino (2015); Jimenez et al. (2016). These parameters provide an indirect evidence of GW emission. Historically, the time derivative of the orbital period in the relativistic binary pulsar B1913+16 has been studied in Hulse and Taylor (1975). In this paper, we investigate the flux of energy due to the GW emissions from the binary systems, and consequently we obtain the first time derivative of the orbital period of several binary pulsars in the context of energy-momentum-squared gravity (EMSG). To do so, we introduce the post-Minkowskian (PM) approximation of this gravitational theory based on the Landau-Lifshitz formulation of the field equations. We apply the modern approach to the PM theory introduced in Will and Wiseman (1996); Pati and Will (2000, 2002)

The outline of the paper is as follows. First, in Sec. II, we briefly review EMSG and its current status among other modified gravity theories. In Sec. III, we clarify the strategy of our calculations. In this section, we introduce the Landau-Lifshitz formulation of the EMSG field equations and the general expression for the flux of energy in this theory. Then, by using this reformulation, the PM approximation of EMSG is comprehensively obtained in Sec. IV. The gravitational energy flux with EMSG correction is studied in Sec. V. As an application of our results, we next investigate the EMSG effect on the first time derivative of the orbital period of the binary pulsar in Sec. VI. We use this post-Keplerian parameter for six known binary pulsars to constrain one of the free parameters of the EMSG in this section. Finally, in Sec. VII, our results are discussed.

II Standard formulation of EMSG

EMSG has been introduced to resolve the big bang singularity Roshan and Shojai (2016); Katırcı and Kavuk (2014). The main idea is to allow the scalar 𝑻2=TαβTαβ{\bm{T}}^{2}=T^{\alpha\beta}T_{\alpha\beta} in the generic action of the theory, where TαβT_{\alpha\beta} is the energy-momentum tensor. The existence of this term induces some quadratic corrections to the Friedman equations that are reminiscent of the corrections reported in the context of loop quantum gravity, see Roshan and Shojai (2016) for more detail. It has been shown in Roshan and Shojai (2016) that EMSG has a bouncing solution preventing the early Universe singularity. However, recently in Barbar et al. (2020) the viability of this bouncing solution has been doubted. EMSG in the Palatini formulation has been investigated in Nazari et al. (2020). It has been shown that in this approach there are viable bouncing solutions. It is important to mention that interest in EMSG, has not been limited to the early Universe and bouncing solutions. For instance, this model has been used to manipulate the cosmic microwave background quadrupole temperature fluctuation Akarsu et al. (2020). Furthermore, this model explains the accelerated expansion of the Universe without the cosmological constant. In other words, the normal matter would be enough to speed up the cosmic expansion, see Akarsu et al. (2018a) and references therein. For the phase space view of EMSG, we refer the reader to Bahamonde et al. (2019). For some other papers on the cosmological and astrophysical issues in EMSG see Shahidi (2021); Moraes and Sahoo (2018); Faria et al. (2019); Sharif and Gul (2021). Although the original version of EMSG does not raise significant corrections to GR at low energy scales, the current versions are necessary to be consistent with the classical tests of gravity in the solar system Nazari (2022).

Now let us discuss the action and the corresponding field equations of EMSG. The general action of this theory is given by

S=g(12kR+f(𝑻2))d4x+SM,\displaystyle S=\int\sqrt{-g}\Big{(}\frac{1}{2k}R+f({\bm{T}}^{2})\Big{)}d^{4}x+S_{M}, (1)

where gg is the determinant of the metric gαβg^{\alpha\beta}, and k=8πG/c4k=8\pi G/c^{4}. Here, as usual, RR is the Ricci scalar, and SMS_{M} is the matter action. Of course, this is not the most general action of the theory. More specifically, one may take a function of RR, namely f(R)f(R). This branch of modified gravity theories has been widely investigated in the literature. On the other hand, our focus here is on the consequences of the scalar 𝑻2\bm{T}^{2}. Therefore, we take the standard linear contribution for the curvature part. In contrast, we take an arbitrary function for 𝑻2\bm{T}^{2}. We consider that f(𝑻2)f({\bm{T}}^{2}) is a Taylor expandable function in terms of 𝑻2\bm{T}^{2} and can then be written as

f(𝑻2)f(𝑻02)+f(𝑻02)(𝑻2𝑻02)+,\displaystyle f({\bm{T}}^{2})\simeq f({\bm{T}}_{0}^{2})+f^{\prime}({\bm{T}}_{0}^{2})\big{(}{\bm{T}}^{2}-{\bm{T}}_{0}^{2}\big{)}+\cdots, (2)

in which the prime stands for the differentiation with respect to 𝑻2{\bm{T}}^{2}. Here, the suffix “0” returns to the 𝑻2{\bm{T}}^{2} value in the background. On the other hand, since our focus is on the gravitational flux of energy in EMSG, we omit the dark energy contribution and assume that there is no matter field in the background. Therefore, the background is described by the flat-Minkowski metric. Then, we have 𝑻02=0{\bm{T}}_{0}^{2}=0 and consequently f(𝑻02)=0f({\bm{T}}_{0}^{2})=0. So, the above relation reduces to

f(𝑻2)f0𝑻2+.\displaystyle f({\bm{T}}^{2})\simeq f^{\prime}_{0}{\bm{T}}^{2}+\cdots. (3)

Here, f0=dfd𝑻2|𝑻2=0f^{\prime}_{0}=\frac{df}{d{\bm{T}}^{2}}\lvert_{{\bm{T}}^{2}=0} 111In this paper, f0f^{\prime}_{0} is equivalent to η/2k-\eta/2k in Roshan and Shojai (2016). and regarding Eq. (1) its SI unit is m s2 kg-1. Inserting Eq. (3) within the general form of the EMSG action (1), and varying each term with respect to the metric, one can obtain the field equations of EMSG as 222For a more detailed discussion, we refer the reader to Roshan and Shojai (2016).

Gμν=kTμνeff,\displaystyle G_{\mu\nu}=kT^{\text{eff}}_{\mu\nu}, (4)

where Gμν=Rμν12gμνRG_{\mu\nu}=R_{\mu\nu}-\frac{1}{2}g_{\mu\nu}R is the Einstein tensor and

Tμνeff=Tμν+f0(gμν𝑻24TμσTνσ4𝚿μν),\displaystyle T^{\text{eff}}_{\mu\nu}=T_{\mu\nu}+f^{\prime}_{0}\Big{(}g_{\mu\nu}{\bm{T}}^{2}-4T^{\sigma}_{\mu}T_{\nu\sigma}-4{\bm{\Psi}}_{\mu\nu}\Big{)}, (5)

is the effective conserved energy-momentum tensor:

μTeffμν=0.\displaystyle\nabla_{\mu}T_{\text{eff}}^{\mu\nu}=0. (6)

In the relation (5), the tensor 𝚿μν{\bm{\Psi}}_{\mu\nu} is given by

𝚿μν=Lm(Tμν12Tgμν)12TTμν2Tαβ2Lmgαβgμν,\displaystyle{\bm{\Psi}}_{\mu\nu}=-L_{m}\big{(}T_{\mu\nu}-\frac{1}{2}Tg_{\mu\nu}\big{)}-\frac{1}{2}TT_{\mu\nu}-2T^{\alpha\beta}\frac{\partial^{2}L_{m}}{\partial g^{\alpha\beta}\partial g^{\mu\nu}}, (7)

where LmL_{m} is the matter Lagrangian density and T=gαβTαβT=g^{\alpha\beta}T_{\alpha\beta}. To indicate the EMSG portion of the effective energy-momentum tensor and separate it from the standard part, we call the second part of Eq. (5)

TμνEMS=f0(gμν𝑻24TμσTνσ4𝚿μν).\displaystyle T_{\mu\nu}^{\text{\tiny EMS}}=f^{\prime}_{0}\Big{(}g_{\mu\nu}{\bm{T}}^{2}-4T^{\sigma}_{\mu}T_{\nu\sigma}-4{\bm{\Psi}}_{\mu\nu}\Big{)}. (8)

Given the definition of 𝚿μν{\bm{\Psi}}_{\mu\nu}, for the different Lagrangian densities describing a perfect fluid Schutz Jr. (1970); Brown (1993), TμνEMST_{\mu\nu}^{\text{\tiny EMS}} and consequently the field equations (4) would be different in this theory. In fact, using different Lagrangian densities for the perfect fluid produces different field equations which indeed describe two distinct theories in the EMSG framework. This is also the case in the f(R)f(R) theories of gravity Faraoni (2009); Bertolami et al. (2008). In the following calculations, in order to follow the literature on the EMSG theory, we use the Lagrangian density Lm=pL_{\text{m}}=p where pp is the pressure to describe a perfect fluid. We leave a supplementary study on the difference between Lagrangian densities in this theory for a future work.

We should mention that in addition to the effective energy-momentum conservation (6), we consider that the conservation of the rest-mass density ρ\rho is established in EMSG, i.e., α(ρuα)=0\nabla_{\alpha}\big{(}\rho u^{\alpha}\big{)}=0. Here, uα=γ(c,𝒗)u^{\alpha}=\gamma(c,\bm{v}) is the four-velocity field where 𝒗\bm{v} is the three-velocity field and γ=u0/c\gamma=u^{0}/c. This relation is simplified so that the rescaled mass density ρ=gγρ\rho^{*}=\sqrt{-g}\gamma\rho satisfies the following relation Poisson and Will (2014):

tρ+j(ρvj)=0.\displaystyle\partial_{t}\rho^{*}+\partial_{j}(\rho^{*}v^{j})=0. (9)

In fact, ρ\rho^{*} is the rescaled mass density that satisfies the continuity equation. In the following calculations, we use this useful definition of the mass density.

III THE STRATEGY OF CALCULATIONS

To solve the modified version of the Einstein field equations and study the gravitational flux of energy in EMSG, we apply the PM theory. In fact, this theory provides an excellent framework in which we can approximately study the GW signals up to the required degree of accuracy. In the following, we first introduce the PM theory in EMSG and next investigate the gravitational flux of energy in this alternative theory of gravity.

In the PM approximation, it is assumed that the gravitational field is weak. As we know, this weak field limit is equivalent to the slow-motion condition for the gravitationally bound system. Since our goal is to study the bound systems, we apply these two conditions throughout our calculation.

The modern approach to the PM approximation of the gravitational field is based on the Landau-Lifshitz formulation of the Einstein field equations. Here, we apply the modern approach and introduce the Landau-Lifshitz formulation of EMSG.

III.1 Landau-Lifshitz formulation of EMSG

To obtain the Landau-Lifshitz formulation of the EMSG field equations, we utilize the similar procedure introduced in Poisson and Will (2014). The following identity is the main relation in this approach:

μνHαμβν=2(g)Gαβ+16πGc4(g)tLLαβ,\displaystyle\partial_{\mu\nu}H^{\alpha\mu\beta\nu}=2(-g)G^{\alpha\beta}+\frac{16\pi G}{c^{4}}(-g)t_{\text{LL}}^{\alpha\beta}, (10)

where HαμβνH^{\alpha\mu\beta\nu} is the pseudotensor constructed from the gothic metric 𝔤αβ=ggαβ\mathfrak{g}^{\alpha\beta}=\sqrt{-g}g^{\alpha\beta} as follows

Hαμβν=𝔤αβ𝔤μν𝔤αν𝔤βμ,\displaystyle H^{\alpha\mu\beta\nu}=\mathfrak{g}^{\alpha\beta}\mathfrak{g}^{\mu\nu}-\mathfrak{g}^{\alpha\nu}\mathfrak{g}^{\beta\mu}, (11)

and it has the same symmetries as the Riemann tensor. In the above identity, (g)tLLαβ(-g)t_{\text{LL}}^{\alpha\beta} is the Landau-Lifshitz pseudotensor given by Eq. (6.5) of Poisson and Will (2014)333 In Appendix. B, for the sake of convenience, the definition of this pseudotensor is also given by Eq. (B).. It should be noted that the identity (10) is valid for every spacetime. Inserting the modified EMSG field equations, i.e., Eq. (4), within Eq. (10), we obtain

μνHαμβν=16πGc4(g)(Teffαβ+tLLαβ).\displaystyle\partial_{\mu\nu}H^{\alpha\mu\beta\nu}=\frac{16\pi G}{c^{4}}(-g)\Big{(}T_{\text{eff}}^{\alpha\beta}+t_{\text{LL}}^{\alpha\beta}\Big{)}. (12)

This relation is the nontensorial form of the EMSG field equations in the Landau-Lifshitz formalism. In the next step toward this derivation, we consider that 𝔤αβ=ηαβhαβ\mathfrak{g}^{\alpha\beta}=\eta^{\alpha\beta}-h^{\alpha\beta}. Here, hαβh^{\alpha\beta} is a gravitational potential and ηαβ\eta^{\alpha\beta} is the Minkowski metric. Furthermore, we use the harmonic gauge condition βhαβ=0\partial_{\beta}h^{\alpha\beta}=0. Applying this new definition of 𝔤αβ\mathfrak{g}^{\alpha\beta} and imposing the harmonic gauge condition in Eq. (12), after some manipulations, one can arrive at

hαβ=16πGc4τeffαβ,\displaystyle\square h^{\alpha\beta}=-\frac{16\pi G}{c^{4}}\tau^{\alpha\beta}_{\text{eff}}, (13)

where =ηαβαβ\square=\eta^{\alpha\beta}\partial_{\alpha\beta} is the Minkowski wave operator and

τeffαβ=(g)(Teffαβ+tLLαβ+tHαβ),\displaystyle\tau^{\alpha\beta}_{\text{eff}}=(-g)\Big{(}T^{\alpha\beta}_{\text{eff}}+t_{\text{LL}}^{\alpha\beta}+t_{\text{H}}^{\alpha\beta}\Big{)}, (14)

is the effective energy-momentum pseudotensor. Here, (g)tHαβ(-g)t_{\text{H}}^{\alpha\beta} is given by

(g)tHαβ=c416πG(μhαννhβμhμνμνhαβ).\displaystyle(-g)t_{\text{H}}^{\alpha\beta}=\frac{c^{4}}{16\pi G}\big{(}\partial_{\mu}h^{\alpha\nu}\partial_{\nu}h^{\beta\mu}-h^{\mu\nu}\partial_{\mu\nu}h^{\alpha\beta}\big{)}. (15)

The wave equation (13) is the cornerstone to derive the PM approximation to the EMSG field equations. By applying the systematic method in the PM theory, we can approximately solve the highly nonlinear wave equation (13) in the wave zone where the radiation effects are significant. As expected, by dropping TμνEMST_{\mu\nu}^{\text{\tiny EMS}} in this relation, the standard Landau-Lifshitz formulation of the Einstein field equations in GR is recovered, cf. Eq. (6.51) in Poisson and Will (2014). In this case, the general form of the solution of the wave equation is comprehensively introduced in chapter 6 in Poisson and Will (2014). Regarding the mathematical similarity of Eq. (13) and that of in GR, we can use the same general from of the solutions here. Therefore, we drop the relevant calculations. Instead, the general form of the solutions are presented in Appendix. B.

As the final point in this subsection, we should mention that the pseudotensor (g)tHαβ(-g)t_{\text{H}}^{\alpha\beta} satisfies the following identity: β((g)tHαβ)=0\partial_{\beta}\big{(}(-g)t_{\text{H}}^{\alpha\beta}\big{)}=0. Keeping this fact in mind and also using the harmonic gauge condition, we deduce from Eq. (13) that

μ((g)(Teffμν+tLLμν))=0.\displaystyle\partial_{\mu}\Big{(}(-g)(T^{\mu\nu}_{\text{eff}}+t_{\text{LL}}^{\mu\nu})\Big{)}=0. (16)

In fact, this is a statement of the conservation equations in this formalism. The wave equation (13) and the conservation equations (16) are the main relations to find the PM approximation to the EMSG field equations.

III.2 Flux of the energy

Let us introduce the energy-balance equation in the Landau-Lifshitz formalism of EMSG. As we know, by studying this equation, one can obtain the relation between the time dependent physical properties of the systems and the amount of energy carried away by the GW emissions. To do so, in a similar fashion to the method introduced in the Landau-Lifshitz formalism of GR, we first introduce the total four-vector momentum as

Pα[V]=1cV(g)(Teffα0+tLLα0)d3x.\displaystyle P^{\alpha}[V]=\frac{1}{c}\int_{V}(-g)\big{(}T^{\alpha 0}_{\text{eff}}+t_{\text{LL}}^{\alpha 0}\big{)}d^{3}x. (17)

Here, VV is the volume of the three-dimensional region where Pα[V]P^{\alpha}[V] is defined. The time and space components of this four-vector momentum represent the total energy P0[V]=c1E[V]P^{0}[V]=c^{-1}E[V] and three-vector momentum Pj[V]P^{j}[V] associated with VV, respectively. It is also considered that there is no matter field on the boundary of this region. In other words, VV is large enough so that the surface of VV, indicated by SS, does not intersect the matter distribution. Bearing this fact in mind and also using the conservation equations (16), one can arrive at

P˙α[V]=S(g)tLLαk𝑑Sk,\displaystyle\dot{P}^{\alpha}[V]=-\oint_{S}(-g)t_{\text{LL}}^{\alpha k}dS_{k}, (18)

for the conservation statement of the total four-vector momentum. Here, the overdot stands for the derivative with respect to time tt. At the first glance, this relation reveals that not only the standard energy-momentum tensor but also the EMSG portion TμνEMST_{\mu\nu}^{\text{\tiny EMS}} have no contribution in this conservation statement and the mathematical form of this equation is the same as in GR Poisson and Will (2014). However, it should be mentioned that the Landau-Lifshitz pseudotensor is not necessarily similar in these two theories. In the following section, we obtain this pseudotensor in EMSG and illustrate the differences.

As we aim to study the rate at which the energy is removed from the GW sources, we focus our attention on the time component of Eq. (18). Then for α=0\alpha=0, we have

E˙[V]=cS(g)tLL0k𝑑Sk.\displaystyle\dot{E}[V]=-c\oint_{S}(-g)t_{\text{LL}}^{0k}dS_{k}. (19)

Here,

E[V]=V(g)(Teff00+tLL00)d3x,\displaystyle E[V]=\int_{V}(-g)\big{(}T^{00}_{\text{eff}}+t^{00}_{\text{LL}}\big{)}d^{3}x, (20)

is the total energy of the system. Regarding Eq. (19), one can define the energy-balance equation in EMSG as

dEdt=𝒫,\displaystyle\frac{dE}{dt}=-\mathcal{P}, (21)

where

𝒫=cS(g)tLL0k𝑑Sk,\displaystyle\mathcal{P}=c\oint_{S}(-g)t_{\text{LL}}^{0k}dS_{k}, (22)

is the flux of energy across the surface SS.

The next step toward studying the energy-balance equation is to find the Landau-Lifshitz pseudotensor in terms of the gravitational potential hαβh^{\alpha\beta}. It is shown in the shortwave approximation where the characteristic wavelength of the GW signals λc\lambda_{c} is much smaller than the distance to the center of the mass of the GW system r=|𝐱|r=|\mathbf{x}|, i.e., where λc/r1\lambda_{c}/r\ll 1, one can simplify the definition (B) as 444 To see more detailed discussions on this issue, we refer the reader to Sec. 12.2.3 of Poisson and Will (2014).

(g)tLLαβ=c232πG(τhTTjkτhjkTT)kαkβ,\displaystyle(-g)t_{\text{LL}}^{\alpha\beta}=\frac{c^{2}}{32\pi G}\Big{(}\partial_{\tau}h_{\text{TT}}^{jk}\partial_{\tau}h^{\text{TT}}_{jk}\Big{)}k^{\alpha}k^{\beta}, (23)

where τ\partial_{\tau} shows the derivative with respect to retarded time τ=tr/c\tau=t-r/c and four vector kαk^{\alpha} is defined by kα=(1,𝒏)k^{\alpha}=(1,\bm{n}). Here hTTjk=(qljqmk12qjkqlm)hlmh^{jk}_{\text{TT}}=\Big{(}q_{l}^{j}q_{m}^{k}-\frac{1}{2}q^{jk}q_{lm}\big{)}h^{lm} represents the transverse-tracefree (T-T) portion of the gravitational potential hjkh^{jk} in which qjk=δjknjnkq_{jk}=\delta_{jk}-n_{j}n_{k} and nj=jrn_{j}=\partial_{j}r. As seen, the mathematical appearance of Eqs. (21) and (22) is similar to the GR one. However, hTTjkh_{\text{TT}}^{jk} can be basically different in EMSG. So, it is not trivial how GW systems will behave in the context of this modified theory of gravity.

To sum up, in order to obtain (g)tLLαβ(-g)t_{\text{LL}}^{\alpha\beta} and consequently the flux of energy in EMSG, we should find T-T part of the gravitational potential in this theory. So, we turn to solve the EMSG field equations (13). In the next section, we attempt to solve these equations by utilizing the PM approximation and obtain hTTjkh_{\text{TT}}^{jk} to the leading order in the EMSG theory. Those readers who are unfamiliar with the PM approximation, or have no interest in the detailed derivation, can directly skip to Sec. V. In this section, applying the results of Sec. IV, we study the flux of energy due to the GW emissions in EMSG.

III.3 Crude estimation

Before starting the main calculations, let us approximately obtain the GW field hTTjkh_{\text{TT}}^{jk} for a specific distribution of the matter in EMSG. We consider the famous quadrupole formula for hTTjkh_{\text{TT}}^{jk}, i.e., hTTjk=(2G/c4r)ττjkh_{\text{TT}}^{jk}=(2G/c^{4}r)\partial_{\tau\tau}\mathcal{I}^{jk}, in which

jk(τ)=c2τ00(τ,𝐱)xjxkd3x,\displaystyle\mathcal{I}^{jk}(\tau)=\int c^{-2}\tau^{00}(\tau,\mathbf{x}^{\prime})x^{\prime j}x^{\prime k}d^{3}x^{\prime}, (24)

is the quadrupole-moment tensor of the matter distribution. In the EMSG case, one may replace τ00\tau^{00} with τeff00\tau_{\text{eff}}^{00}. To find hTTjkh_{\text{TT}}^{jk}, we should then derive the time-time component of the effective energy-momentum pseudotensor (14). To do so, we choose a perfect fluid for describing the matter distribution in the Minkowski spacetime as Tαβ=(ρ+ϵ/c2+p/c2)uαuβ+pηαβT^{\alpha\beta}=\big{(}\rho+\epsilon/c^{2}+p/c^{2}\big{)}u^{\alpha}u^{\beta}+p\eta^{\alpha\beta}. Here, ϵ\epsilon is the proper internal energy density and pp is the pressure. We also consider that the velocity of the fluid elements is slow compared to the speed of light and the following set of conditions is established in this fluid system (v2/c21,p/ρc21,andϵ/ρc21v^{2}/c^{2}\ll 1,\,p/\rho c^{2}\ll 1,\,\text{and}\,\epsilon/\rho c^{2}\ll 1). With this in mind, regarding Eqs. (5), (B), and (15), one can show that τeff00\tau^{00}_{\text{eff}} up to the leading order is given by

τeff00=c2ρEMSeff+O(1),\displaystyle\tau^{00}_{\text{eff}}=c^{2}\rho_{\text{\tiny EMS}}^{\text{eff}}+O(1), (25)

where ρEMSeff=ρ(1+c2f0ρ)\rho_{\text{\tiny EMS}}^{\text{eff}}=\rho\left(1+c^{2}f_{0}^{\prime}\rho\right) represents the effective mass density in EMSG. So, we can conclude that finding the quadrupole moment

jk(τ)=ρEMSeff(τ,𝐱)xjxkd3x,\displaystyle\mathcal{I}^{jk}(\tau)=\int\rho_{\text{\tiny EMS}}^{\text{eff}}(\tau,\mathbf{x}^{\prime})x^{\prime j}x^{\prime k}d^{3}x^{\prime}, (26)

will be the main task toward deriving hTTjkh_{\text{TT}}^{jk} in EMSG. This crude estimation clearly shows that not only does ρ\rho play a role but ρ2\rho^{2} also has a contribution to the GW field hTTjkh_{\text{TT}}^{jk}. On the other hand, it should be emphasized that as this estimation is based on the behavior of the perfect fluid in the flat spacetime, the matter field indeed does not respond to gravity. In other words, enforcing Eq. (6) for the matter field in the Minkowski spacetime reveals that the matter is not subjected to the gravitational interaction in this estimation. Moreover, the Landau-Lifshitz and harmonic pseudotensors vanish here. Therefore, to incorporate the role of the gravity into the result, it is necessary to obtain τeff00\tau^{00}_{\text{eff}} more precisely. Toward this goal, in the next section, we introduce the PM expansion of the gravitational potentials in EMSG.

As it will be shown, we also need to indicate the order of magnitude of the free parameter of this theory. To do so, let us recall the time-time component of the metric up to the Newtonian order: g00=1+2U/c2g_{00}=-1+2U/c^{2} where UU is the gravitational potential and given by 2U=4πGρ\nabla^{2}U=-4\pi G\rho. One may deduce that this metric component will be g00=1+2UN/c2+2f0UEMSg_{00}=-1+2U_{\text{\tiny N}}/c^{2}+2f_{0}^{\prime}U_{\text{\tiny EMS}} after changing ρ\rho to the effective mass density ρEMSeff\rho_{\text{\tiny EMS}}^{\text{eff}}. Here, 2UN=4πGρ\nabla^{2}U_{\text{\tiny N}}=-4\pi G\rho and 2UEMS=4πGρ2\nabla^{2}U_{\text{\tiny EMS}}=-4\pi G\rho^{2} are the Poisson equations for the Newtonian and EMSG potentials UNU_{\text{\tiny N}} and UEMSU_{\text{\tiny EMS}}, respectively. Considering the weak field limit and comparing the first, second, and third terms in this component of the metric reveal that UN/c2U_{\text{\tiny N}}/c^{2} and f0UEMSf_{0}^{\prime}U_{\text{\tiny EMS}} should be very small, i.e., UN/c21U_{\text{\tiny N}}/c^{2}\ll 1 and f0UEMS1f_{0}^{\prime}U_{\text{\tiny EMS}}\ll 1. So, we consider that f0UEMSf_{0}^{\prime}U_{\text{\tiny EMS}} is at most of the order of UN/c2U_{\text{\tiny N}}/c^{2} 555In the following, for the sake of simplification, we drop the index “N ”..

IV PM approximation in EMSG

As mentioned earlier, in the context of the PM approximation, the system is restricted by two constraints: the slow-motion condition and weak-field limit, i.e., v2/c21v^{2}/c^{2}\ll 1 and U/c21U/c^{2}\ll 1, respectively. Regarding the last paragraph in the previous subsection, we would also have f0UEMS1f_{0}^{\prime}U_{\text{\tiny EMS}}\ll 1 in the weak-field limit. Given this point, hereafter, we treat each order of f0f_{0}^{\prime} as a correction of the order c2c^{-2}. In this approximate context, the spacetime deviates slightly from the flat spacetime. It is considered that its deviation, i.e., the gravitational potential hαβh^{\alpha\beta}, can be expanded in the power of the gravitational constant GG asymptotically Poisson and Will (2014). This is known as the PM expansion of the gravitational potentials. Moreover, in this framework, each order c2c^{-2} is considered as a post-Newtonian (PN) correction which indicates the order of the magnitude of each term. In the modern approach to the PM theory, using the PM expansion of the gravitational potentials and applying the iterative procedure, one can approximately solve the highly nonlinear field equations and obtain hαβh^{\alpha\beta} to the required PN order. The main point in the iterative procedure is that the source term of the wave equation (13) in the nnth iterated step is constructed in the previous step, i.e., (n1)(n-1)th iterated step. Then the wave equation will be linear and can be solved systematically. In the following, we take the advantages of this method to solve Eq. (13) in the wave zone.

The PN expansion of the spacetime metric is the main material required at least in the first steps of our derivation. To construct the PN expansion of the metric, we need to have information about the PN order of the gravitational potentials. For a survey of the PN order of hαβh^{\alpha\beta}, let us estimate the leading PN order of the first term in the PM expansion of the gravitational potentials, h(1)αβ=O(G)h^{\alpha\beta}_{(1)}=O(G), by using the following crude scheme. We will obtain the complete PN expansion of hαβh^{\alpha\beta} to the required degree of accuracy in the subsequent subsections.

Let us introduce the standard and EMSG portions of the energy-momentum tensors of a specific system. Here, we consider that the system is a perfect fluid. So, we have

Tαβ=(ρ+ϵc2+pc2)uαuβ+pgαβ,\displaystyle T^{\alpha\beta}=\big{(}\rho+\frac{\epsilon}{c^{2}}+\frac{p}{c^{2}}\big{)}u^{\alpha}u^{\beta}+pg^{\alpha\beta}, (27)

for the standard energy-momentum tensor. Moreover, utilizing the perfect fluid description, we find

TEMSαβ=f0(c4ρ2gαβ+2c2(ϵρgαβ+ρ2uαuβ)+(3p2\displaystyle T^{\alpha\beta}_{\text{\tiny EMS}}=f_{0}^{\prime}\Big{(}c^{4}\rho^{2}g^{\alpha\beta}+2c^{2}\big{(}\epsilon\rho g^{\alpha\beta}+\rho^{2}u^{\alpha}u^{\beta}\big{)}+\big{(}3p^{2}
+ϵ2)gαβ+(8pρ+4ϵρ+1c2(6p2+8pϵ+2ϵ2))uαuβ),\displaystyle+\epsilon^{2}\big{)}g^{\alpha\beta}+\big{(}8p\rho+4\epsilon\rho+\frac{1}{c^{2}}(6p^{2}+8p\epsilon+2\epsilon^{2})\big{)}u^{\alpha}u^{\beta}\Big{)}, (28)

for the EMSG part of energy-momentum tensor (8). To arrive at this relation, we use the normalization condition gαβuαuβ=c2g_{\alpha\beta}u^{\alpha}u^{\beta}=-c^{2} and assume that Lm=pL_{m}=p for a perfect fluid Schutz Jr. (1970). In the simplest case, we assume that the spacetime is described by the flat Minkowski metric ηαβ\eta^{\alpha\beta}. So, it is obvious that leading PN order of T00T^{00} is O(c2)O(c^{2}), T0jT^{0j} is O(c)O(c), and TjkT^{jk} is O(1)O(1). Also, TEMS00T^{00}_{\text{\tiny EMS}} is of the order c2c^{2}, TEMS0jT^{0j}_{\text{\tiny EMS}} is of the order cc, and TEMSjkT^{jk}_{\text{\tiny EMS}} is of the order c2c^{2} when j=kj=k and of the order c0c^{0} when jkj\neq k. Regarding the coefficient c4c^{-4} in Eq. (13), we then conclude that in EMSG, the leading PN correction of h00h^{00} is of the order c2c^{-2}, h0jh^{0j} is of the order c3c^{-3}, and hjkh^{jk} is of the order c2c^{-2} when j=kj=k and of the order c4c^{-4} when jkj\neq k. This crude estimation of the PN order of hαβh^{\alpha\beta}’s components illuminates our path toward finding the correct required degree of accuracy for the PN metric.

IV.1 Post-Minkowskian expansion of metric

Regarding the estimation of the PN order of the hαβh^{\alpha\beta} components stated before as well as utilizing Eq. (88), we find the PM expansion of the metric components in terms of the gravitational potentials as

g00=1+12h0038(h00)2+12hkk(112h00)\displaystyle g_{00}=-1+\frac{1}{2}h^{00}-\frac{3}{8}\big{(}h^{00}\big{)}^{2}+\frac{1}{2}h^{kk}\big{(}1-\frac{1}{2}h^{00}\big{)}
18(hkk)2+O(c6),\displaystyle-\frac{1}{8}\big{(}h^{kk}\big{)}^{2}+O(c^{-6}), (29a)
g0j=h0j+O(c5),\displaystyle g_{0j}=-h^{0j}+O(c^{-5}), (29b)
gij=δij(1+12h00)+hij12δijhkk+O(c4).\displaystyle g_{ij}=\delta_{ij}\Big{(}1+\frac{1}{2}h^{00}\Big{)}+h^{ij}-\frac{1}{2}\delta_{ij}h^{kk}+O(c^{-4}). (29c)

These equations provide sufficient PN corrections for the metric components that we need in the following computation. In an equivalent manner, using the general equation (89), we arrive at

(g)=1+h00hkk+O(c4),\displaystyle(-g)=1+h^{00}-h^{kk}+O(c^{-4}), (30)

for the PM expansion of gg containing the PN corrections to O(c4)O(c^{-4}) order. As expected from the high order of hkkh^{kk}, in this modified theory of gravity, the PM expansions of the metric and its determinant are more complicated than the GR ones.

IV.2 Gravitational potentials in the first iteration

After choosing the matter portion of the system, we are now in the position to solve the EMSG version of the field equations in the Landau-Lifshitz formalism. To do so, we utilize the iteration procedure. We recall that although our aim is to obtain hjkh^{jk} in the wave zone, enough information about the metric in the near zone, especially in the first iteration step is required. Let us mention that, in the PM theory, the near zone is restricted to a three-dimension sphere with the radius λc\mathcal{R}\approx\lambda_{\text{c}}. Beyond this region is called the wave zone. Given the position of the source point in the solution of the wave equations, the gravitational potential is separated into two parts. In a similar fashion to Poisson and Will (2014), we call these parts the near-zone and wave-zone portions of the gravitational potential when the source point is situated in the near and wave zones, respectively. Of course, the solution of the wave equations also depends on the position of the field point. In each case, we specify the field point position.

We now launch the iteration procedure. In the zeroth iterated step, we assume that hαβ(0)=0h_{\alpha\beta}^{(0)}=0 and gαβ(0)=ηαβg_{\alpha\beta}^{(0)}=\eta_{\alpha\beta}. It should be emphasized that the assumption hαβ(0)=0h_{\alpha\beta}^{(0)}=0 is equivalent to what we have considered to derive Eq. (3). In fact, here, it is assumed that there is no matter field in the background. Therefore, we have g(0)=1\sqrt{-g^{(0)}}=1 and γ=1+12v2c2+O(c4)\gamma=1+\frac{1}{2}\frac{v^{2}}{c^{2}}+O(c^{-4}). By considering the definition of rescaled mass density, one can simply deduce that ρ=(112v2c2+O(c4))ρ\rho=\big{(}1-\frac{1}{2}\frac{v^{2}}{c^{2}}+O(c^{-4})\big{)}\rho^{*} in the zeroth iteration. We then turn to find hαβ(1)h_{\alpha\beta}^{(1)} in the first iterated step. As we will see in the second iterated step, in order to extract the correct and required PN order for hαβ(2)h_{\alpha\beta}^{(2)}, we need to find h(1)00h_{(1)}^{00} to O(c2)O(c^{-2}), h(1)0jh_{(1)}^{0j} to O(c3)O(c^{-3}), and h(1)ijh_{(1)}^{ij} up to O(c4)O(c^{-4}) in the first iterated step. So, we should derive the sources of these gravitational potentials, i.e., the components of the effective energy-momentum tensor, as follows: τ(0)eff00\tau^{00}_{\text{(0)eff}} to O(c2)O(c^{2}), τ(0)eff0j\tau^{0j}_{\text{(0)eff}} to O(c)O(c), τ(0)eff ij\tau^{ij}_{\text{(0)eff }} up to O(1)O(1). In the following, we introduce each part of τ(0)effαβ\tau^{\alpha\beta}_{\text{(0)eff}} separately. For the usual energy-momentum tensor, T(0)αβT^{\alpha\beta}_{(0)}, we have

c2T(0)00=ρ+O(c2),\displaystyle c^{-2}T^{00}_{(0)}=\rho^{*}+O(c^{-2}), (31a)
c1T(0)0j=ρvj+O(c2),\displaystyle c^{-1}T^{0j}_{(0)}=\rho^{*}v^{j}+O(c^{-2}), (31b)
T(0)ij=O(1).\displaystyle T^{ij}_{(0)}=O(1). (31c)
Also, for the EMSG energy-momentum tensor (28) up to the similar PN order, we find that
c2T(0)EMS00=2c2f0ρ2+O(c2),\displaystyle c^{-2}T^{00}_{\text{\tiny(0)EMS}}=2c^{2}f_{0}^{\prime}{\rho^{*}}^{2}+O(c^{-2}), (32a)
c1T(0)EMS0j=2c2f0ρ2vj+O(c2),\displaystyle c^{-1}T^{0j}_{\text{\tiny(0)EMS}}=2c^{2}f_{0}^{\prime}{\rho^{*}}^{2}v^{j}+O(c^{-2}), (32b)
T(0)EMSij=c4f0ρ2δij+O(1).\displaystyle T^{ij}_{\text{\tiny(0)EMS}}=c^{4}f_{0}^{\prime}{\rho^{*}}^{2}\delta^{ij}+O(1). (32c)

Furthermore, since in the zeroth iterated step h(0)αβ=0h^{\alpha\beta}_{(0)}=0, we arrive at t(0)LLαβ=0=t(0)Hαβt_{(0)\text{LL}}^{\alpha\beta}=0=t_{(0)\text{H}}^{\alpha\beta}. Hence, we obtain the main materials desired to construct the gravitational potentials in the next iteration of the gravitational field equations. Now, we attempt to find the gravitational potentials where both the field and source points are situated in the near zone in the first iterated step, i.e., h(1)𝒩αβh_{(1)\mathcal{N}}^{\alpha\beta}. To do so, we insert Eqs. (31a)-(32c) into integral (90). For the time-time component of h(1)αβh^{\alpha\beta}_{(1)}, we have

h(1)𝒩00=4c2U+4f0UEMS+O(c3),\displaystyle h_{(1)\mathcal{N}}^{00}=\frac{4}{c^{2}}U+4f_{0}^{\prime}U_{\text{\tiny EMS}}+O(c^{-3}), (33)

in which UU is the Newtonian potential in terms of ρ\rho^{*} and UEMSU_{\text{\tiny EMS}} is the EMSG gravitational potential. The Poisson integrals of UU and UEMSU_{\text{\tiny EMS}} are given by

U=Gρ|𝒙𝒙|d3x,\displaystyle U=G\int_{\mathcal{M}}\frac{{\rho^{*}}^{\prime}}{\rvert{\bm{x}-\bm{x}^{\prime}}\rvert}d^{3}x^{\prime}, (34a)
UEMS=Gρ2|𝒙𝒙|d3x,\displaystyle U_{\text{\tiny EMS}}=G\int_{\mathcal{M}}\frac{{{\rho^{*}}^{\prime}}^{2}}{\rvert\bm{x}-\bm{x}^{\prime}\rvert}d^{3}x^{\prime}, (34b)

respectively. Here, \mathcal{M} represents the three-dimension region which in fact separates the near zone from the wave zone. Similarly, for the time-space components of h(1)αβh^{\alpha\beta}_{(1)} in the required order, we find that

h(1)𝒩0j=4c3Uj+8cf0UEMSj+O(c4),\displaystyle h^{0j}_{(1)\mathcal{N}}=\frac{4}{c^{3}}U^{j}+\frac{8}{c}f_{0}^{\prime}U^{j}_{\text{\tiny EMS}}+O(c^{-4}), (35)

where UjU^{j} is the well-known PN vector potential

Uj=Gρvj|𝒙𝒙|d3x,\displaystyle U^{j}=G\int_{\mathcal{M}}\frac{{\rho^{*}}^{\prime}v^{\prime j}}{\rvert{\bm{x}-\bm{x}^{\prime}}\rvert}d^{3}x^{\prime}, (36)

while UEMSjU^{j}_{\text{\tiny EMS}} is the new vector potential in the EMSG framework defined as

UEMSj=Gρ2vj|𝒙𝒙|d3x.\displaystyle U^{j}_{\text{\tiny EMS}}=G\int_{\mathcal{M}}\frac{{{\rho^{*}}^{\prime}}^{2}v^{\prime j}}{\rvert{\bm{x}-\bm{x}^{\prime}}\rvert}d^{3}x^{\prime}. (37a)

Finally, for the space-space components, we arrive at

h(1)𝒩ij=4f0δij(UEMSGcddt𝔐)+O(c4),\displaystyle h^{ij}_{(1)\mathcal{N}}=4f_{0}^{\prime}\delta^{ij}\Big{(}U_{\text{\tiny EMS}}-\frac{G}{c}\frac{d}{dt}\mathfrak{M}\Big{)}+O(c^{-4}), (38)

in which

𝔐=ρ2d3x,\displaystyle\mathfrak{M}=\int_{\mathcal{M}}{{\rho^{*}}^{\prime}}^{2}d^{3}x^{\prime}, (39)

is a new quantity in EMSG. It should be noted that all integrands in the above relations are a function of tt and 𝒙{\bm{x}^{\prime}}. So far, we have found the near-zone portion of the gravitational potential. To complete our derivation in this iterated step, we should also find the wave-zone part of the gravitational potential, i.e., h(1)𝒲αβh_{(1)\mathcal{W}}^{\alpha\beta} where the source point is in the wave zone and the field point is situated in the near zone. In this case, as mentioned before, the source term of the potential h(1)αβh_{(1)}^{\alpha\beta} is equal to T(0)effαβT_{(0)\text{eff}}^{\alpha\beta}; and t(0)LLαβt_{(0)\text{LL}}^{\alpha\beta} and t(0)Hαβt_{(0)\text{H}}^{\alpha\beta} have no portion. Therefore, the source term is completely constructed from the matter part in this step. On the other hand, the matter part of the system is completely restricted to the near zone when the slow-motion condition is established Poisson and Will (2014). As we consider a gravitationally bound system, this assumption is also true throughout our derivation. This fact reveals that the wave-zone part of the gravitational potential in the first iterated step is zero. Subsequently, we have h(1)𝒲αβ=0h_{(1)\mathcal{W}}^{\alpha\beta}=0 and h(1)αβ=h(1)𝒩αβh_{(1)}^{\alpha\beta}=h_{(1)\mathcal{N}}^{\alpha\beta}.

To sum up, we obtain the PN expansion of the EMSG potential’s components required to construct the near-zone metric in the first iterated step. Substituting Eqs. (33), (35), and (38) within Eqs. (29a), (29b),(29c), and (30), we finally arrive at

g00(1)=1+2Uc2+8f0UEMS+O(c3),\displaystyle g_{00}^{(1)}=-1+\frac{2U}{c^{2}}+8f_{0}^{\prime}U_{\text{\tiny EMS}}+O(c^{-3}), (40a)
g0j(1)=4Ujc38cf0UEMSj+O(c4),\displaystyle g_{0j}^{(1)}=-\frac{4U^{j}}{c^{3}}-\frac{8}{c}f_{0}^{\prime}U^{j}_{\text{\tiny EMS}}+O(c^{-4}), (40b)
gij(1)=(1+2Uc2)δij+O(c4),\displaystyle g_{ij}^{(1)}=\Big{(}1+\frac{2U}{c^{2}}\Big{)}\delta_{ij}+O(c^{-4}), (40c)
(g(1))=1+4Uc28f0UEMS+O(c3).\displaystyle(-g_{(1)})=1+\frac{4U}{c^{2}}-8f_{0}^{\prime}U_{\text{\tiny EMS}}+O(c^{-3}). (40d)

Here, we discard some extra PN orders.

As seen, the components and determinant of the near-zone metric are constructed from the usual potentials UU and UjU^{j} as well as the EMSG potentials UEMSU_{\text{\tiny EMS}} and UEMSjU^{j}_{\text{\tiny EMS}}. Notice that in order to describe a relativistic system to the first PN (1PN ) order, one should find the PN corrections of g00g^{00}, g0jg^{0j}, and gjkg^{jk} to O(c4)O(c^{-4}), O(c3)O(c^{-3}), and O(c2)O(c^{-2}), respectively. It is obvious from the above terms, in this iterated step, the required PN orders for the time-time metric component are not completely evaluated. It means that one should continue the journey toward the next iterated step and find gαβ(2)g^{(2)}_{\alpha\beta}. It is worth noting that the odd order c3c^{-3} that appears in the determinant and time-time component of the metric is entirely built of the EMSG term that is proportional to d𝔐/dtd\mathfrak{M}/dt. In Appendix. C, we simplify this term. However, because in this step, the required PN orders of the metric to describe a relativistic system are not built, we are not concerned about this odd-power order. In other words, after finding the metric components at least to the 1PN order, one can truly interpret the role of the odd PN orders and examine the time-reversal invariance of solutions.

IV.3 Gravitational potentials in the second iteration

In the following, we attempt to obtain the appropriate PN corrections for τ(1)effαβ\tau^{\alpha\beta}_{\text{(1)eff}} that are necessary to derive h(2)αβh^{\alpha\beta}_{(2)}. Regarding the relationship between the effective energy-momentum pseudotensor and gravitational potential components, we deduce that the source terms of the gravitational potential should be built to O(c2)O(c^{2}) for τ(1)eff00\tau^{00}_{\text{(1)eff}}, O(c)O(c) for τ(1)eff0j\tau^{0j}_{\text{(1)eff}}, and O(1)O(1) for τ (1)effjk\tau^{jk}_{\text{ (1)eff}}. This fact will be clarified in the following computations.

By inserting Eqs. (40a)-(40c) into the normalization condition gαβuαuβ=c2g_{\alpha\beta}u^{\alpha}u^{\beta}=-c^{2}, we find that γ(1)=1+4f0UEMS+1c2(12v2+U)+O(c3)\gamma^{(1)}=1+4f_{0}^{\prime}U_{\text{\tiny EMS}}+\frac{1}{c^{2}}\big{(}\frac{1}{2}v^{2}+U\big{)}+O(c^{-3}). Then, using γ(1)\gamma^{(1)} and g(1)g_{(1)}, we have ρ=[1+1c2(12v2+3U)]ρ+O(c4)\rho^{*}=\Big{[}1+\frac{1}{c^{2}}\big{(}\frac{1}{2}v^{2}+3U\big{)}\Big{]}\rho+O(c^{-4}) for the rescaled mass density. Now, by applying these parameters and the components of gαβ(1)g_{\alpha\beta}^{(1)} in Eq. (27), we arrive at

T(1)00=ρc2+O(1),\displaystyle T^{00}_{(1)}=\rho^{*}c^{2}+O(1), (41a)
T(1)0j=ρvjc+O(c1),\displaystyle T^{0j}_{(1)}=\rho^{*}v^{j}c+O(c^{-1}), (41b)
T(1)jk=pδjk+ρvjvk+O(c2),\displaystyle T^{jk}_{(1)}=p\delta^{jk}+\rho^{*}v^{j}v^{k}+O(c^{-2}), (41c)

for the contravariant components of the energy-momentum tensor in the first iterated step. We keep terms up to the desired PN order mentioned earlier. It is worth mentioning that in Eq. (41a), the O(1)O(1) term is entirely constructed from the EMSG term and it is given by ρc2f0UEMS\rho^{*}c^{2}f_{0}^{\prime}U_{\text{\tiny EMS}}.

We now obtain the EMSG part of the energy-momentum tensor T(1)EMSαβT^{\alpha\beta}_{\text{\tiny(1)EMS}}. According to the original definition of this tensor, i.e., Eq. (8), we first obtain 𝑻(1)2{\bm{T}}^{2}_{(1)} for the perfect fluid up to O(1)O(1). This is the appropriate PN order to find the required PN expansion of T(1)EMSαβT^{\alpha\beta}_{\text{\tiny(1)EMS}}’s components. In this step, one can deduce

𝑻(1)2=ρ2c4ρ2c2(v22Π+6U)+O(1).\displaystyle{\bm{T}}^{2}_{(1)}={\rho^{*}}^{2}c^{4}-{\rho^{*}}^{2}c^{2}\big{(}v^{2}-2\Pi+6U\big{)}+O(1). (42)

Here, Π=ϵ/ρ\Pi=\epsilon/\rho^{*}. Then using the above relation and the PN expansion of the metric and energy-momentum tensor components in the first iterated step, we arrive at

T(1)EMS00=ρ2c4f0+O(1),\displaystyle T^{00}_{\text{\tiny(1)EMS}}={\rho^{*}}^{2}c^{4}f_{0}^{\prime}+O(1), (43a)
T(1)EMS0j=2ρ2c3f0vj+O(c1),\displaystyle T^{0j}_{\text{\tiny(1)EMS}}=2{\rho^{*}}^{2}c^{3}f_{0}^{\prime}v^{j}+O(c^{-1}), (43b)
T(1)EMSjk=ρ2c4f0[δjk+1c2(2vjvk(v22Π\displaystyle T^{jk}_{\text{\tiny(1)EMS}}={\rho^{*}}^{2}c^{4}f_{0}^{\prime}\Big{[}\delta^{jk}+\frac{1}{c^{2}}\Big{(}2v^{j}v^{k}-\big{(}v^{2}-2\Pi
+8U)δjk)]+O(c2),\displaystyle+8U\big{)}\delta^{jk}\Big{)}\Big{]}+O(c^{-2}), (43c)

after some simplifications. Here, we again truncate the PN expansion of these components to the required accuracy. It should be mentioned that the c0c^{0} order in T(1)EMS00T^{00}_{\text{\tiny(1)EMS}} is built of the EMSG term that is proportional to ρ2c4f02UEMS{\rho^{*}}^{2}c^{4}{f_{0}^{\prime}}^{2}U_{\text{\tiny EMS}}.

The remaining source terms of the gravitational potential h(2)αβh_{(2)}^{\alpha\beta} are (g(1))t(1)LLαβ(-g^{(1)})t_{(1)\text{LL}}^{\alpha\beta} and (g(1))t(1)Hαβ(-g^{(1)})t_{(1)\text{H}}^{\alpha\beta}. As we have mentioned before, these pseudotensors themselves are constructed from the gravitational potential. In the first iterated step, they are built of h(1)αβh_{(1)}^{\alpha\beta}. We keep those PN orders in the expansion of h(1)αβh_{(1)}^{\alpha\beta} which construct the order c2c^{2} for (g(1))t(1)LL,H00(-g^{(1)})t_{(1)\text{LL,H}}^{00}, order c1c^{1} for (g(1))t(1)LL,H0j(-g^{(1)})t_{(1)\text{LL,H}}^{0j}, and order c0c^{0} for (g(1))t(1)LL,Hjk(-g^{(1)})t_{(1)\text{LL,H}}^{jk}. We start with the Landau-Lifshitz pseudotensor. After inserting Eqs. (33), (35), and (38) within the definition (B), we find

(g(1))t(1)LL00=O(1),\displaystyle(-g^{(1)})t_{(1)\text{LL}}^{00}=O(1), (44a)
(g(1))t(1)LL0j=O(c1),\displaystyle(-g^{(1)})t_{(1)\text{LL}}^{0j}=O(c^{-1}), (44b)
(g(1))t(1)LLjk=14πG[jUkU12nUnUδjk]\displaystyle(-g^{(1)})t_{(1)\text{LL}}^{jk}=\frac{1}{4\pi G}\bigg{[}\partial^{j}U\partial^{k}U-\frac{1}{2}\partial^{n}U\partial_{n}U\delta^{jk}\bigg{]} (44c)
+c4f0πG[f0(nUEMSnUEMSδjkjUEMSkUEMS)\displaystyle+\frac{c^{4}f_{0}^{\prime}}{\pi G}\bigg{[}f_{0}^{\prime}\Big{(}\partial^{n}U_{\text{\tiny EMS}}\partial_{n}U_{\text{\tiny EMS}}\delta^{jk}-\partial^{j}U_{\text{\tiny EMS}}\partial^{k}U_{\text{\tiny EMS}}\Big{)}
+1c2(2jUEMSkUnUEMSnUδjk)]+O(c1),\displaystyle+\frac{1}{c^{2}}\Big{(}2\partial^{j}U_{\text{\tiny EMS}}\partial^{k}U-\partial^{n}U_{\text{\tiny EMS}}\partial_{n}U\delta^{jk}\Big{)}\bigg{]}+O(c^{-1}),

for the PN expansion of the Landau-Lifshitz pseudotensor components. The last task here is to evaluate (g(1))t(1)Hαβ(-g^{(1)})t_{(1)\text{H}}^{\alpha\beta}. To do so, we substitute Eqs. (33), (35), and (38) into Eq. (15). After some simplifications, we deduce that

(g(1))t(1)H00=O(1),\displaystyle(-g^{(1)})t_{(1)\text{H}}^{00}=O(1), (45a)
(g(1))t(1)H0j=O(c1),\displaystyle(-g^{(1)})t_{(1)\text{H}}^{0j}=O(c^{-1}), (45b)
(g(1))t(1)Hjk=c4f02πG[jUEMSkUEMS\displaystyle(-g^{(1)})t_{(1)\text{H}}^{jk}=\frac{c^{4}f_{0}^{\prime 2}}{\pi G}\bigg{[}\partial^{j}U_{\text{\tiny EMS}}\partial^{k}U_{\text{\tiny EMS}} (45c)
UEMSnnUEMSδjk]+O(c1).\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}-U_{\text{\tiny EMS}}\partial_{n}\partial^{n}U_{\text{\tiny EMS}}\delta^{jk}\bigg{]}+O(c^{-1}).

Gathering together Eqs. (41a)-(41c), and (43a)-(45c), one can construct the components of the EMSG effective pseudotensor as follows:

c2τ(1)eff00=ρ+c2f0ρ2+O(c2),\displaystyle c^{-2}\tau^{00}_{(1)\text{eff}}=\rho^{*}+c^{2}f_{0}^{\prime}{\rho^{*}}^{2}+O(c^{-2}), (46a)
c1τ(1)eff0j=ρvj+2c2f0ρ2vj+O(c2),\displaystyle c^{-1}\tau^{0j}_{(1)\text{eff}}=\rho^{*}v^{j}+2c^{2}f_{0}^{\prime}{\rho^{*}}^{2}v^{j}+O(c^{-2}), (46b)
τ(1)effjk=ρvjvk+pδjk+14πG[jUkU12nUnUδjk]\displaystyle\tau^{jk}_{(1)\text{eff}}=\rho^{*}v^{j}v^{k}+p\delta^{jk}+\frac{1}{4\pi G}\bigg{[}\partial^{j}U\partial^{k}U-\frac{1}{2}\partial_{n}U\partial^{n}U\delta^{jk}\bigg{]}
+c4f0[ρ2δjk+1c2(ρ2δjk(2Πv24U)+2ρ2vjvk\displaystyle+c^{4}f_{0}^{\prime}\bigg{[}{\rho^{*}}^{2}\delta^{jk}+\frac{1}{c^{2}}\Big{(}{\rho^{*}}^{2}\delta^{jk}\big{(}2\Pi-v^{2}-4U\big{)}+2{\rho^{*}}^{2}v^{j}v^{k}
+1πG(2jUEMSkUnUEMSnUδjk))\displaystyle+\frac{1}{\pi G}\big{(}2\partial^{j}U_{\text{\tiny EMS}}\partial^{k}U-\partial_{n}U_{\text{\tiny EMS}}\partial^{n}U\delta^{jk}\big{)}\Big{)} (46c)
+f0δjk(1πGnUEMSnUEMS4ρ2UEMS)]+O(c1).\displaystyle+f_{0}^{\prime}\delta^{jk}\Big{(}\frac{1}{\pi G}\partial_{n}U_{\text{\tiny EMS}}\partial^{n}U_{\text{\tiny EMS}}-4{\rho^{*}}^{2}U_{\text{\tiny EMS}}\Big{)}\bigg{]}+O(c^{-1}).

Here, to simplify the last component, we utilize the Poisson equation 2UEMS=4πGρ2\nabla^{2}U_{\text{\tiny EMS}}=-4\pi G{\rho^{*}}^{2}. As seen, except for the space-space component, the standard and EMSG parts of τ(1)eff00\tau^{00}_{(1)\text{eff}} and those of τ(1)eff0j\tau^{0j}_{(1)\text{eff}} have the same order of the magnitude. Only the term c4f0ρ2c^{4}f_{0}^{\prime}{\rho^{*}}^{2} in τ(1)effjk\tau^{jk}_{(1)\text{eff}} has an unusual PN order, O(c2)O(c^{2}), compared to the standard terms in this component. In the following computations, we investigate the possible role of this term in the final result.

So far, we have found some source terms which we need to build the gravitational potential tensor in the second iterated step. This tensor in fact has two portions. One part comes from the near-zone solution of the wave equation (13) and another one is the wave-zone solution of this equation. The general form of these solutions is given in Appendix. B.

1. Near-zone portion

Here, we choose the field point within the wave zone and the source point within the near zone. For this case, the general solution form of h𝒩αβh_{\mathcal{N}}^{\alpha\beta} is given in (91). We should also recall that according to what was mentioned in Sec. III.2, we finally aim to obtain tLL0kt_{\text{LL}}^{0k}, which appears in the energy-balance equation. Therefore, we just need to find the space-space component of h(2)αβh_{(2)}^{\alpha\beta}, cf. Eq. (23). Rewriting Eq. (91) for h(2)𝒩jkh_{(2)\mathcal{N}}^{jk}, we have

h(2)𝒩jk(t,𝒙)=\displaystyle h_{(2)\mathcal{N}}^{jk}(t,\bm{x})= 4Gc4l=0(1)ll!\displaystyle\frac{4G}{c^{4}}\sum_{l=0}^{\infty}\frac{(-1)^{l}}{l!} (47)
×j1j2jl[1rτeffjk(τ,𝒙)xj1j2jld3x].\displaystyle\times\partial_{j_{1}j_{2}\cdots j_{l}}\bigg{[}\frac{1}{r}\int_{\mathcal{M}}\tau^{jk}_{\text{eff}}(\tau,\bm{x}^{\prime})x^{\prime j_{1}j_{2}\cdots j_{l}}d^{3}x^{\prime}\bigg{]}.

As this step is the very last iterated step of this derivation, we can now apply the gauge condition βh(2)αβ=0\partial_{\beta}h^{\alpha\beta}_{(2)}=0 or equivalently the conservation equation βτ(1)effαβ=0\partial_{\beta}\tau^{\alpha\beta}_{\text{(1)eff}}=0 in order to simplify the general solution (47). In fact, in the final step where the metric truly describes the spacetime with sufficient PN corrections, we enforce the gauge condition/conservation equation to investigate the dynamical behavior of the system Poisson and Will (2014). Utilizing βτ(1)effαβ=0\partial_{\beta}\tau^{\alpha\beta}_{\text{(1)eff}}=0, one can then show that 666The GR versions of the identities (48a) and (48b) are introduced in chapter 7 of Poisson and Will (2014).

τ(1)effjk=1200(τ (1)eff00xjxk)+12q(2τ (1)effq(jxk)\displaystyle\tau^{jk}_{\text{(1)eff}}=\frac{1}{2}\partial_{00}\big{(}\tau^{00}_{\text{ (1)eff}}x^{j}x^{k}\big{)}+\frac{1}{2}\partial_{q}\big{(}2\tau^{q(j}_{\text{ (1)eff}}x^{k)}
pτ(1)effqpxjxk),\displaystyle-\partial_{p}\tau^{qp}_{\text{(1)eff}}x^{j}x^{k}\big{)}, (48a)
τ(1)effjkxp=120(2τ (1)eff0(jxk)xpτ(1)eff0pxjxk)\displaystyle\tau^{jk}_{\text{(1)eff}}x^{p}=\frac{1}{2}\partial_{0}\Big{(}2\tau^{0(j}_{\text{ (1)eff}}x^{k)}x^{p}-\tau^{0p}_{\text{(1)eff}}x^{j}x^{k}\Big{)}
+12n(2τ(1)effn(jxk)xpτ (1)effpnxjxk).\displaystyle+\frac{1}{2}\partial_{n}\Big{(}2\tau^{n(j}_{\text{(1)eff}}x^{k)}x^{p}-\tau^{pn}_{\text{ (1)eff}}x^{j}x^{k}\Big{)}. (48b)

Now, we return to Eq. (47). For the case l=0l=0, after replacing the integrand in Eq. (47) with Eq. (48a), we arrive at

4Gc4\displaystyle\frac{4G}{c^{4}} 1rτ (1)effjk(τ,𝒙)d3x=\displaystyle\frac{1}{r}\int_{\mathcal{M}}\tau^{jk}_{\text{ (1)eff}}(\tau,\bm{x}^{\prime})d^{3}x^{\prime}= (49)
2Gc41rttc2τ (1)eff00xjxkd3x\displaystyle\frac{2G}{c^{4}}\frac{1}{r}\partial_{tt}\int_{\mathcal{M}}c^{-2}\tau^{00}_{\text{ (1)eff}}x^{\prime j}x^{\prime k}d^{3}x^{\prime}
+2Gc41r(2τ (1)effq(jxk)pτ (1)effqpxjxk)𝑑Sq,\displaystyle+\frac{2G}{c^{4}}\frac{1}{r}\oint_{\partial\mathcal{M}}\Big{(}2\tau^{q(j}_{\text{ (1)eff}}x^{\prime k)}-\partial_{p}\tau^{qp}_{\text{ (1)eff}}x^{\prime j}x^{\prime k}\Big{)}dS_{q},

where the Gauss divergence theorem has been used. We first focus our attention on the surface integrals. As mentioned before, the matter portion of our system is completely restricted to the near zone, and consequently TαβT^{\alpha\beta} and TEMSαβT^{\alpha\beta}_{\text{\tiny EMS}} are zero on the boundary between the near and wave zones, i.e., the surface \partial\mathcal{M}. So, the surface integrals in the above relation reduce to

(2τ (1)effq(j[F]xk)pτ(1)effqp[F]xjxk)𝑑Sq,\displaystyle\oint_{\partial\mathcal{M}}\Big{(}2\tau^{q(j}_{\text{ (1)eff}}[\text{F}]x^{\prime k)}-\partial_{p}\tau^{qp}_{\text{(1)eff}}[\text{F}]x^{\prime j}x^{\prime k}\Big{)}dS_{q}, (50)

where τeffjk[F]\tau^{jk}_{\text{eff}}[\text{F}] representing the field portion of the effective energy-momentum tensor is given by

τ(1)effjk[F]=14πG[jUkU12nUnUδjk]\displaystyle\tau^{jk}_{\text{(1)eff}}[F]=\frac{1}{4\pi G}\bigg{[}\partial^{j}U\partial^{k}U-\frac{1}{2}\partial_{n}U\partial^{n}U\delta^{jk}\bigg{]}
+c4f0πG[1c2(2jUEMSkUnUEMSnUδjk)\displaystyle+\frac{c^{4}f_{0}^{\prime}}{\pi G}\bigg{[}\frac{1}{c^{2}}\Big{(}2\partial^{j}U_{\text{\tiny EMS}}\partial^{k}U-\partial_{n}U_{\text{\tiny EMS}}\partial^{n}U\delta^{jk}\Big{)} (51)
+f0(nUEMSnUEMSUEMSnnUEMS)δjk]+O(c1).\displaystyle+f_{0}^{\prime}\Big{(}\partial_{n}U_{\text{\tiny EMS}}\partial^{n}U_{\text{\tiny EMS}}-U_{\text{\tiny EMS}}\partial_{n}\partial^{n}U_{\text{\tiny EMS}}\Big{)}\delta^{jk}\bigg{]}+O(c^{-1}).

In fact, this pseudotensor is entirely constructed from (g(1))t(1)LLjk(-g^{(1)})t_{(1)\text{LL}}^{jk} and (g(1))t(1)Hjk(-g^{(1)})t_{(1)\text{H}}^{jk} which can exist beyond the near zone, cf. Eqs. (44c) and (45c). As seen, the Newtonian gravitational potential UU and the EMSG gravitational potential UEMSU_{\text{\tiny EMS}} appear in this source term. So, to derive the surface integral, let us estimate the order of magnitude of UU and UEMSU_{\text{\tiny EMS}} on the surface region \partial\mathcal{M}. In Appendix. D, by applying the N-body description of the fluid system, we find two expansions (102) and (106) in terms of the distance to the field point for UU and UEMSU_{\text{\tiny EMS}}, respectively. In fact, using these relations, one can approximately evaluate the Newtonian and EMSG gravitational potentials of NN separated bodies at a considerable distance from each body. Taking advantage of this description and using Eq. (102), we deduce that U=O(1)+O(3)+U=O(\mathcal{R}^{-1})+O(\mathcal{R}^{-3})+\cdots and jU=O(2)+O(4)+\partial_{j}U=O(\mathcal{R}^{-2})+O(\mathcal{R}^{-4})+\cdots on the surface \partial\mathcal{M}. For the EMSG potential, using Eq. (106), we also find that UEMS=O(1)+O(3)+U_{\text{\tiny EMS}}=O(\mathcal{R}^{-1})+O(\mathcal{R}^{-3})+\cdots and jUEMS=O(2)+O(4)+\partial_{j}U_{\text{\tiny EMS}}=O(\mathcal{R}^{-2})+O(\mathcal{R}^{-4})+\cdots on the surface \partial\mathcal{M}.

Keeping this fact in mind and substituting the first term of Eq. (IV.3) into the first part of the surface integral (50), we have

12πG\displaystyle\frac{1}{2\pi G} (qU(jUxk))𝑑Sq=2G3qU(jUnk)nq\displaystyle\oint_{\partial\mathcal{M}}\Big{(}\partial^{q}U\partial^{(j}Ux^{\prime k)}\Big{)}dS_{q}=\frac{2}{G}\mathcal{R}^{3}\langle\partial^{q}U\partial^{(j}Un^{k)}n_{q}\rangle
=2G1n(jnk)+O(m),\displaystyle=\frac{2}{G}\mathcal{R}^{-1}\langle n^{(j}n^{k)}\rangle+O(\mathcal{R}^{-m}), (52)

in which m>1m>1. Here, we use that dSq=2nqdΩdS_{q}=\mathcal{R}^{2}n_{q}d\Omega and xk=nkx^{k}=\mathcal{R}n^{k} on the surface \partial\mathcal{M}. We also use this fact that nqnq=1n^{q}n_{q}=1. In the above relation, the angular bracket denotes an average over the surface of a sphere, i.e., =(4π)1()𝑑Ω\langle\cdots\rangle=(4\pi)^{-1}\int(\cdots)d\Omega. As seen, this term is a function of \mathcal{R}. It is argued that the \mathcal{R}-dependent terms in the gravitational potential should be omitted from the main results Poisson and Will (2014). In fact, \mathcal{R}-dependent terms in the near-zone portion of hαβh^{\alpha\beta} are finally canceled by those in the wave-zone portion of hαβh^{\alpha\beta}. Therefore, we implement this scheme in our calculation and freely discard this term from our results. We use the same analysis for the other terms in Eq. (IV.3). It should be mentioned that here, we use the fact that the angular average of the odd number of 𝒏\bm{n}s is zero. Furthermore, as we aim to obtain the T-T part of the gravitational potential hjkh^{jk}, we can freely drop terms that are proportional to δjk\delta^{jk}. Finally we find that the surface integrals in Eq. (49) all are a function of \mathcal{R} and consequently have no contribution to the case l=0l=0 in the expansion of the gravitational potential h(2)𝒩jk(t,𝒙)h_{(2)\mathcal{N}}^{jk}(t,\bm{x}). We leave deriving the volume integral in Eq. (49) here and turn to find the next case l=1l=1.

To examine the next term in the expansion of h(2)𝒩jkh_{(2)\mathcal{N}}^{jk}, we set l=1l=1 in Eq. (47). For this term, we have

4Gc4p[1rτ (1)effjk(τ,𝒙)xpd3x]=\displaystyle-\frac{4G}{c^{4}}\partial_{p}\bigg{[}\frac{1}{r}\int_{\mathcal{M}}\tau^{jk}_{\text{ (1)eff}}(\tau,\bm{x}^{\prime})x^{\prime p}d^{3}x^{\prime}\bigg{]}=
2Gc4p[1rt(2c1τ (1)eff0(jxk)xpc1τ (1)eff0pxjxk)d3x\displaystyle-\frac{2G}{c^{4}}\partial_{p}\bigg{[}\frac{1}{r}\partial_{t}\int_{\mathcal{M}}\big{(}2c^{-1}\tau^{0(j}_{\text{ (1)eff}}x^{\prime k)}x^{\prime p}-c^{-1}\tau^{0p}_{\text{ (1)eff}}x^{\prime j}x^{\prime k}\big{)}d^{3}x^{\prime}
+1r(2τ (1)effn(jxk)xpτ(1)effpnxjxk)dSn].\displaystyle+\frac{1}{r}\oint_{\partial\mathcal{M}}\Big{(}2\tau^{n(j}_{\text{ (1)eff}}x^{\prime k)}x^{\prime p}-\tau^{pn}_{\text{(1)eff}}x^{\prime j}x^{\prime k}\Big{)}dS_{n}\bigg{]}. (53)

Now, we try to obtain the first volume integral in the above relation. As mentioned earlier, our goal is to find h(2)𝒩jk(t,𝒙)h_{(2)\mathcal{N}}^{jk}(t,\bm{x}) to the leading PN order. So, the PN expansion of c1τ(1)eff0jc^{-1}\tau^{0j}_{\text{(1)eff}} is limited to O(c2)O(c^{-2}). This component is obtained to the required order in Eq. (46b). We start our calculation in this part by finding the order of magnitude of the first term in the above relation. In this case, after inserting ρvj\rho^{*}v^{j} into the volume integral of Eq. (IV.3), one can easily grasp that this volume integral is proportional to Ijkp=(2ρv(jxk)xpρvpxjxk)d3xI^{jkp}=\int\big{(}2\rho^{*}v^{(j}x^{k)}x^{p}-\rho^{*}v^{p}x^{j}x^{k}\big{)}d^{3}x. Regarding this relation, we deduce that IjkpI^{jkp} is of the order O(mcvcrc2)O(m_{c}v_{c}r_{c}^{2}). Here, the quantities mcm_{c} and rcr_{c} represent the characteristic mass and length scale of the system, respectively. Moreover, vcv_{c} is the characteristic velocity of the system. So, we deduce that the time derivation of this term is of the order I˙jkp=O(mcvcrc2tc)\dot{I}^{jkp}=O(\frac{m_{c}v_{c}r_{c}^{2}}{t_{c}}) in which tct_{c} is the characteristic time scale during which the source changes. In the other words, tc=rc/vct_{c}=r_{c}/v_{c}. We should recall that IjkpI^{jkp} is a function of the retarded time τ\tau. Therefore, the first term in Eq. (IV.3) becomes

2Gc4p(1rI˙jkp)=2Gc4(1crI¨jkpnp+1r2I˙jkpnp)\displaystyle-\frac{2G}{c^{4}}\partial_{p}(\frac{1}{r}\dot{I}^{jkp})=\frac{2G}{c^{4}}\Big{(}\frac{1}{cr}\ddot{I}^{jkp}n_{p}+\frac{1}{r^{2}}\dot{I}^{jkp}n_{p}\Big{)} (54)
=O(Gc5mcvcrc2rtc2(1+λcr))O(Gc5mcvcrc2rtc2).\displaystyle=O\Big{(}\frac{G}{c^{5}}\frac{m_{c}v_{c}r_{c}^{2}}{rt_{c}^{2}}\big{(}1+\frac{\lambda_{c}}{r}\big{)}\Big{)}\simeq O\Big{(}\frac{G}{c^{5}}\frac{m_{c}v_{c}r_{c}^{2}}{rt_{c}^{2}}\Big{)}. (55)

To simplify the above relation, we use τ/xp=c1np\partial\tau/\partial x^{p}=-c^{-1}n_{p} and also consider that λcr\lambda_{c}\ll r where λc=ctc\lambda_{c}=c\,t_{c} is the characteristic wavelength of the radiation. This condition reveals that the field point is situated in the wave zone. In fact, as we aim to study the gravitational potential in the wave zone, the assumption λcr\lambda_{c}\ll r is completely suitable here. Now, we compare this term with the volume integral in the case l=0l=0. By substituting the leading term of Eq. (46a) within the volume integral of Eq. (49), we evaluate the order of magnitude of this term as

4Gc41rttρxjxkd3x=O(Gc4mcrc2rtc2).\displaystyle\frac{4G}{c^{4}}\frac{1}{r}\partial_{tt}\int_{\mathcal{M}}{\rho^{*}}^{\prime}x^{\prime j}x^{\prime k}d^{3}x^{\prime}=O\Big{(}\frac{G}{c^{4}}\frac{m_{c}r_{c}^{2}}{rt_{c}^{2}}\Big{)}. (56)

From these estimations, one can easily grasp that the volume integral in the l=1l=1 case compared to the leading term in the l=0l=0 case is of the order O(vc/c)O(v_{c}/c). By applying a similar analysis, we find that the second term in Eq. (46b) compared to Eq. (56) is also of the order O(vc/c)O(v_{c}/c). Therefore, this term in total will add a 0.50.5PN correction to the PN expansion of the gravitational potential. On the other hands, if the leading term of the l=0l=0 case is considered as the 11PN correction, the biggest contribution of the l=1l=1 case to Eq. (47) will be of the 1.51.5PN order.

As the final part of our calculation in this subsection, it is important to obtain the surface integral in the l=1l=1 case, cf. Eq. (IV.3). To do so, we again restrict the source of this surface integral to the field portion of the effective energy-momentum tensor introduced in Eq. (IV.3). So, we have

(2τ(1)effn(j[F]xk)xpτ (1)effpn[F]xjxk)𝑑Sn,\displaystyle\oint_{\partial\mathcal{M}}\Big{(}2\tau^{n(j}_{\text{(1)eff}}[F]x^{\prime k)}x^{\prime p}-\tau^{pn}_{\text{ (1)eff}}[F]x^{\prime j}x^{\prime k}\Big{)}dS_{n}, (57)

for this surface integral. By applying a similar analysis mentioned above, one can show that this integral is simplified to the angular average of the odd number of 𝒏\bm{n}s times the \mathcal{R}-dependent terms. So, this surface integral eventually vanishes and has no contribution to h(2)𝒩jkh_{(2)\mathcal{N}}^{jk}. It should be emphasized that the unusual high-order term appearing in the space-space component of τ(1)effαβ\tau_{(1)\text{eff}}^{\alpha\beta} just contributes to the surface integrals. Completely depending to the matter part of the system, this term then has no role up to the leading order. To sum up, we deduce that each ll-pole term in Eq. (47) will be the (l/2)(l/2)PN correction in the PN expansion of the near-zone gravitational potential.

Considering the above discussion, we finally deduce that the PN expansion of the near-zone gravitational potential (47) is simplified as

h(2)𝒩jk=2Gc4¨(2)jk(τ)r+O(c5),\displaystyle h_{(2)\mathcal{N}}^{jk}=\frac{2G}{c^{4}}\frac{\ddot{\mathcal{I}}^{jk}_{(2)}(\tau)}{r}+O(c^{-5}), (58)

where

(2)jk=c2τ (1)eff00(τ,𝒙)xjxkd3x.\displaystyle\mathcal{I}^{jk}_{(2)}=\int_{\mathcal{M}}c^{-2}\tau^{00}_{\text{ (1)eff}}(\tau,\bm{x}^{\prime})x^{\prime j}x^{\prime k}d^{3}x^{\prime}. (59)

To find the leading PN order of Eq. (58) and consequently the leading term in the energy-balance equation, we should only insert the order c2c^{2} of τ(1)eff00\tau^{00}_{\text{(1)eff}} into the definition (59). This order is derived in the previous part. As seen, in comparison with the GR system, for two cases f0>0f_{0}^{\prime}>0 or f0<0f_{0}^{\prime}<0, the gravitational potential can be stronger or weaker in EMSG, respectively. So far, we have derived the near-zone portion of h(2)jkh_{(2)}^{jk} described by Eqs. (58). To complete our calculation, we obtain the wave-zone portion of the gravitational potential in the rest of this section.

2. Wave-zone portion

In order to find the wave-zone portion of the total gravitational potential, h(2)𝒲jkh^{jk}_{(2)\mathcal{W}}, enough information about the source terms, cf. Eq. (14), is required. It means we should obtain the effective energy-momentum pseudotensor τ(1)effαβ\tau^{\alpha\beta}_{\text{(1)eff}} in the wave zone. We recall that in the previous part, we obtained this pseudotensor in the near zone. To construct τ(1)effαβ\tau^{\alpha\beta}_{\text{(1)eff}} existing in the wave zone, we first calculate its foundations, i.e., h(1)αβh_{(1)}^{\alpha\beta} in which the field point is situated in the wave zone. By using relations mentioned in Appendix. B, we find h(1)αβh_{(1)}^{\alpha\beta} where |𝒙||\bm{x}|\geq\mathcal{R} as follows. After substituting Eqs. (31a) and (32a) within Eq. (91), we have

h(1)𝒩00=4Gc21r(M0(τ)+c2f0𝔐(τ))+O(c3),\displaystyle h_{(1)\mathcal{N}}^{00}=\frac{4G}{c^{2}}\frac{1}{r}\Big{(}M_{0}(\tau)+c^{2}f_{0}^{\prime}\mathfrak{M}(\tau)\Big{)}+O(c^{-3}), (60)

for the time-time component of the gravitational potential in the first iteration of the wave equation. Here,

M0=ρd3x,\displaystyle M_{0}=\int_{\mathcal{M}}{\rho^{*}}d^{3}x^{\prime}, (61)

in principle, represents the total matter inside the near zone. As before, we consider that f0f_{0}^{\prime} is a constant. In the above relation, one can show that O(c3)O(c^{-3}) comes from l=1l=1 terms in the expansion (91). In a similar way, for the time-space component of the potential, we arrive at

h(1)𝒩0j=4Gc31r(P0j(τ)+2c2f0𝔓j(τ))+O(c4),\displaystyle h_{(1)\mathcal{N}}^{0j}=\frac{4G}{c^{3}}\frac{1}{r}\Big{(}P_{0}^{j}(\tau)+2c^{2}f_{0}^{\prime}\,\mathfrak{P}^{j}(\tau)\Big{)}+O(c^{-4}), (62)

where

P0j=ρvjd3x,\displaystyle P_{0}^{j}=\int_{\mathcal{M}}{\rho^{*}}v^{j}d^{3}x^{\prime}, (63)

and

𝔓j=ρ2vjd3x.\displaystyle\mathfrak{P}^{j}=\int_{\mathcal{M}}{{\rho^{*}}^{\prime}}^{2}v^{\prime j}d^{3}x^{\prime}. (64)

In this component, l=1l=1 terms contribute at O(c4)O(c^{-4}) and its O(c3)O(c^{-3}) term is purely built of the l=0l=0 pole. Finally, for the space-space component, we obtain

h(1)𝒩jk=4Gf0r𝔐δjk+O(c3).\displaystyle h_{(1)\mathcal{N}}^{jk}=4G\frac{f_{0}^{\prime}}{r}\mathfrak{M}\,\delta^{jk}+O(c^{-3}). (65)

Notice M0M_{0}, P0jP_{0}^{j}, 𝔐\mathfrak{M}, and 𝔓j\mathfrak{P}^{j} all are functions of the retarded time τ\tau here. In this component, the c3c^{-3} order is also constructed from l=1l=1 terms of the expansion (91). In general, one can show that each ll-pole term in this expansion adds an l/2l/2PN contribution to hαβh^{\alpha\beta}. Until now, we derive the near-zone portion of the gravitational potential, i.e., h(1)𝒩αβh_{(1)\mathcal{N}}^{\alpha\beta}. To complete the gravitational potential, we should also find h(1)𝒲αβh_{(1)\mathcal{W}}^{\alpha\beta} where both the field and source points are in the wave zone. On the other hand, regarding Eqs. (31a)-(32c), one can easily conclude that h(1)𝒲αβh_{(1)\mathcal{W}}^{\alpha\beta} vanishes and then h(1)αβ=h(1)𝒩αβh_{(1)}^{\alpha\beta}=h_{(1)\mathcal{N}}^{\alpha\beta}. As seen in this part of the derivation, in the EMSG theory, the gravitational potential can exist in the wave zone even at the first iteration step. At the first glance, it shows that one can study the energy-balance equation with the information derived in the first iteration. However, considering the coefficient δjk\delta^{jk} in Eq. (65), this potential in fact has no T-T portion to construct the Landau-Lifshitz pseudotensor at this order, cf. Eqs. (22) and (23). From this point, we continue our computation until the second iteration.

Now, applying the components of h(1)𝒩αβh_{(1)\mathcal{N}}^{\alpha\beta}, we can find τ(1)effαβ\tau_{\text{(1)eff}}^{\alpha\beta} in the wave zone. We first turn to find the Landau-Lifshitz pseudotensor (g(1))t(1)LLαβ(-g^{(1)})t_{(1)\text{LL}}^{\alpha\beta}. To do so, we insert Eqs. (60), (62), and (65) into definition (B). After some simplifications, we arrive at

(g(1))t(1)LL00=Gπr4(78M02+c4f0𝔐(f0𝔐\displaystyle(-g^{(1)})t_{(1)\text{LL}}^{00}=-\frac{G}{\pi r^{4}}\Big{(}\frac{7}{8}M_{0}^{2}+c^{4}f_{0}^{\prime}\mathfrak{M}\big{(}f_{0}^{\prime}\mathfrak{M}
+1c2M0))+O(c1),\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}+\frac{1}{c^{2}}M_{0}\big{)}\Big{)}+O(c^{-1}), (66a)
(g(1))t(1)LL0j=O(c1),\displaystyle(-g^{(1)})t_{(1)\text{LL}}^{0j}=O(c^{-1}), (66b)
(g(1))t(1)LLjk=Gπr4[(14M02c4f0𝔐(f0𝔐\displaystyle(-g^{(1)})t_{(1)\text{LL}}^{jk}=\frac{G}{\pi r^{4}}\bigg{[}\Big{(}\frac{1}{4}M^{2}_{0}-c^{4}f_{0}^{\prime}\mathfrak{M}\big{(}f_{0}^{\prime}\mathfrak{M} (66c)
2c2M0))(njnk12δjk)+12c4f02𝔐2δjk]+O(c1).\displaystyle-\frac{2}{c^{2}}M_{0}\big{)}\Big{)}\Big{(}n^{j}n^{k}-\frac{1}{2}\delta^{jk}\Big{)}+\frac{1}{2}c^{4}{f_{0}^{\prime}}^{2}\mathfrak{M}^{2}\delta^{jk}\bigg{]}+O(c^{-1}).

We will see that the PN order of the space-space component is indeed sufficient to calculate the h(2)𝒲jkh_{(2)\mathcal{W}}^{jk} to the leading order. Here, we use this fact that jτ=1/cnj\partial_{j}\tau=-1/c\,n^{j}. We also use that jF(τ)=1/cnjτF\partial_{j}F(\tau)=-1/c\,n^{j}\partial_{\tau}F where FF is an arbitrary function of the retarded time. Moreover, due to Eq. (9), one can conclude that dM0/dt=0dM_{0}/dt=0. To find the harmonic portion, we substitute the components of h(1)𝒩αβh_{(1)\mathcal{N}}^{\alpha\beta} within the definition (15). So, we have

(g(1))t(1)H00=2Gπr4c4f0𝔐(f0𝔐+1c2M0)\displaystyle(-g^{(1)})t_{(1)\text{H}}^{00}=-\frac{2G}{\pi r^{4}}c^{4}f_{0}^{\prime}\mathfrak{M}\big{(}f_{0}^{\prime}\mathfrak{M}+\frac{1}{c^{2}}M_{0}\big{)}
+O(c1),\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}+O(c^{-1}), (67a)
(g(1))t(1)H0j=O(c1),\displaystyle(-g^{(1)})t_{(1)\text{H}}^{0j}=O(c^{-1}), (67b)
(g(1))t(1)Hjk=Gπr4c4f02𝔐2(njnk2δjk)\displaystyle(-g^{(1)})t_{(1)\text{H}}^{jk}=\frac{G}{\pi r^{4}}c^{4}{f_{0}^{\prime}}^{2}\mathfrak{M}^{2}\big{(}n^{j}n^{k}-2\delta^{jk}\big{)}
+O(c1).\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}+O(c^{-1}). (67c)

Here, we use that jnk=1r(δjknjnk)\partial_{j}n_{k}=\frac{1}{r}\big{(}\delta_{jk}-n_{j}n_{k}\big{)}. On the other hand, since the matter part of the system cannot exist in the wave zone, the entire energy-momentum pseudotensor τ(1)effαβ\tau_{\text{(1)eff}}^{\alpha\beta} in the wave zone is constructed from (g(1))t(1)LLαβ(-g^{(1)})t_{(1)\text{LL}}^{\alpha\beta} and (g(1))t(1)Hαβ(-g^{(1)})t_{(1)\text{H}}^{\alpha\beta}. Regarding this point and gathering together Eqs. (66a)-(67c), we finally arrive at

τ(1)eff00=Gπr4(78M02+3c4f0𝔐(f0𝔐+1c2M0))\displaystyle\tau_{\text{(1)eff}}^{00}=-\frac{G}{\pi r^{4}}\Big{(}\frac{7}{8}M_{0}^{2}+3c^{4}f_{0}^{\prime}\mathfrak{M}\big{(}f_{0}^{\prime}\mathfrak{M}+\frac{1}{c^{2}}M_{0}\big{)}\Big{)}
+O(c1),\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}+O(c^{-1}), (68a)
τ(1)eff0j=O(c1),\displaystyle\tau_{\text{(1)eff}}^{0j}=O(c^{-1}), (68b)
τ(1)effjk=Gπr4[(14M02+2c2f0𝔐M0)(njnk12δjk)\displaystyle\tau_{\text{(1)eff}}^{jk}=\frac{G}{\pi r^{4}}\Big{[}\big{(}\frac{1}{4}M^{2}_{0}+2c^{2}f_{0}^{\prime}\mathfrak{M}M_{0}\big{)}\big{(}n^{j}n^{k}-\frac{1}{2}\delta^{jk}\big{)}
c4f02𝔐2δjk]+O(c1).\displaystyle~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}~{}-c^{4}{f_{0}^{\prime}}^{2}\mathfrak{M}^{2}\delta^{jk}\Big{]}+O(c^{-1}). (68c)

It should be mentioned that, here, we only need to obtain the space-space component of τ(1)effαβ\tau_{\text{(1)eff}}^{\alpha\beta}. However, for the sake of completeness, we have found the other components as well.

Before deriving h(2)𝒲jkh_{(2)\mathcal{W}}^{jk}, let us simplify the source term of this potential, i.e, τ(1)effjk\tau_{\text{(1)eff}}^{jk} so that the symmetric trace-free tensors appear in it. To do so, we rewrite Eq. (68c) as follows:

τ(1)effjk=Gπr4[(14M02+2c2f0𝔐M0)(n<jk>16δjk)\displaystyle\tau_{\text{(1)eff}}^{jk}=\frac{G}{\pi r^{4}}\Big{[}\big{(}\frac{1}{4}M^{2}_{0}+2c^{2}f_{0}^{\prime}\mathfrak{M}M_{0}\big{)}\big{(}n^{<jk>}-\frac{1}{6}\delta^{jk}\big{)}
c4f02𝔐2δjk]+O(c1),\displaystyle-c^{4}{f_{0}^{\prime}}^{2}\mathfrak{M}^{2}\delta^{jk}\Big{]}+O(c^{-1}), (69)

in which n<jk>=njnk1/3δjkn^{<jk>}=n^{j}n^{k}-1/3\delta^{jk} is a symmetric trace-free tensor. Now, by comparing this relation with Eq. (92), we can simply deduce that in this case, the source of the gravitational potential h(2)𝒲jkh_{(2)\mathcal{W}}^{jk} is a function of rnr^{-n} with n=4n=4 and

fl=0jk=G6δjk(M02+8c4f0𝔐(3f0𝔐+1c2M0)),\displaystyle f_{l=0}^{jk}=-\frac{G}{6}\delta^{jk}\Big{(}M_{0}^{2}+8c^{4}f_{0}^{\prime}\mathfrak{M}\big{(}3f_{0}^{\prime}\,\mathfrak{M}+\frac{1}{c^{2}}M_{0}\big{)}\Big{)}, (70a)
fl=2jk=GM0(M0+8c2f0𝔐).\displaystyle f_{l=2}^{jk}=GM_{0}\big{(}M_{0}+8c^{2}f_{0}^{\prime}\mathfrak{M}\big{)}. (70b)

Up to this point, we have achieved adequate materials to calculate the integral (B). Considering n=4n=4 and applying Eqs. (70a)-(70b) for l=0l=0 and l=2l=2 respectively, after some simplifications, we eventually arrive at

h(2)𝒲jk=\displaystyle h_{(2)\mathcal{W}}^{jk}= G2c4r2{(M02+8c2f0𝔐M0)njnk\displaystyle\frac{G^{2}}{c^{4}r^{2}}\bigg{\{}\Big{(}M_{0}^{2}+8c^{2}f_{0}^{\prime}\mathfrak{M}M_{0}\Big{)}n^{j}n^{k}
+8c4f02𝔐2δjk},\displaystyle+8c^{4}{f_{0}^{\prime}}^{2}\mathfrak{M}^{2}\delta^{jk}\bigg{\}}, (71)

for the space-space component of the gravitational potential in the wave zone. Note that as already mentioned, we drop the \mathcal{R}-dependent terms. It is obvious from this relation that the wave-zone contribution of the gravitational potential is proportional to the inverse squared rr. However, because we aim to find the flux of the energy in the far-away wave zone, in comparison to h(2)𝒩jkh_{(2)\mathcal{N}}^{jk} which falls as r1r^{-1}, we may discard this contribution to hjkh^{jk}. Furthermore, this part is 0.5PN order higher than the leading term in Eq. (58). To show this fact, regarding Eqs. (58) and (IV.3), we deduce that h(2)𝒲jk/h(2)𝒩jk=O(GMtc2/rrc2)h_{(2)\mathcal{W}}^{jk}/h_{(2)\mathcal{N}}^{jk}=O(GMt^{2}_{\text{c}}/rr^{2}_{\text{c}}). Considering the Newtonian acceleration, one can show that GMGM is of the rc3/tc2r^{3}_{\text{c}}/t^{2}_{\text{c}} order. By applying this order for GMGM and also setting rλc=ctcr\sim\lambda_{\text{c}}=c\,t_{\text{c}}, one can conclude that h(2)𝒲jk/h(2)𝒩jk=O(vc/c)h_{(2)\mathcal{W}}^{jk}/h_{(2)\mathcal{N}}^{jk}=O(v_{\text{c}}/c). Therefore, this portion of the potential adds a 0.5PN correction to h(2)jkh_{(2)}^{jk}, i.e., h(2)𝒲jkh_{(2)\mathcal{W}}^{jk} is actually of the 1.5 PN order. To sum up, with regard to both former and latter facts, we can ignore this part in our calculation. So, we have h(2)jk=h(2)𝒩jkh_{(2)}^{jk}=h_{(2)\mathcal{N}}^{jk}.

V Gravitational energy flux in EMSG

It is comprehensively shown that the leading order of the gravitational potential in the EMSG theory is described by Eq. (58) and the only difference with the GR case comes from the definition of quadrupole-moment tensor jk\mathcal{I}^{jk} in this theory. Rewriting Eq. (59) up to the leading order, we have

jk=(ρ+c2f0ρ2)xjxkd3x.\displaystyle\mathcal{I}^{jk}=\int_{\mathcal{M}}\big{(}\rho+c^{2}f_{0}^{\prime}\rho^{2}\big{)}x^{j}x^{k}d^{3}x. (72)

As seen in addition to the usual term ρ\rho, a new quadratic term ρ2\rho^{2} plays a role in this order. Since we focus on the leading order, hereafter, we drop “*” and exhibit the density with ρ\rho. Therefore, one can straightforwardly deduce that the EMSG version of the instantaneous gravitational energy flux is given by

𝒫=G5c5˙˙˙<jk>˙˙˙<jk>,\displaystyle\mathcal{P}=\frac{G}{5c^{5}}\dddot{\mathcal{I}}^{<jk>}\dddot{\mathcal{I}}_{<jk>}, (73)

in which <jk>=jk1/3δjkqq\mathcal{I}^{<jk>}=\mathcal{I}^{jk}-1/3\,\delta^{jk}\,\mathcal{I}^{qq} is the symmetric-tracefree sector of jk\mathcal{I}^{jk}. It should be mentioned that to derive 𝒫\mathcal{P}, the angular average of the radial vectors 𝒏\bm{n}s is used here. The difference with GR is that instead of the Newtonian mass quadrupole moment IjkI^{jk}, we insert jk\mathcal{I}^{jk}. It is obvious that, like in GR (cf. Will (2018)), the monopole and dipole terms vanish here and in this PN order, the quadrupole term contributes to the flux of energy.

In order to clarify the role of the EMSG correction in this relation practically, we investigate 𝒫\mathcal{P} for a binary system containing two compact bodies with mass mAm_{A} where the index “AA ” stands for the body AA and A=1,2A=1,2. As usual, we choose the barycenter coordinate system to study the binary system. In this coordinate system, the position of each body 𝒓A(t)\bm{r}_{A}(t) is given with respect to the system’s barycenter. We also have

𝒓1=m2m𝒓,𝒓2=m1m𝒓,\displaystyle\bm{r}_{1}=\frac{m_{2}}{m}\bm{r},~{}~{}~{}~{}~{}~{}~{}~{}\bm{r}_{2}=-\frac{m_{1}}{m}\bm{r}, (74a)
𝒗1=m2m𝒗,𝒗2=m1m𝒗,\displaystyle\bm{v}_{1}=\frac{m_{2}}{m}\bm{v},~{}~{}~{}~{}~{}~{}~{}~{}\bm{v}_{2}=-\frac{m_{1}}{m}\bm{v}, (74b)

where m=m1+m2m=m_{1}+m_{2} is total mass of the system. Here, 𝒓=𝒓1𝒓2\bm{r}=\bm{r}_{1}-\bm{r}_{2} is the separation vector of the bodies and 𝒗=d𝒓/dt\bm{v}=d\bm{r}/dt is their relative velocity. It should be noted, because of the presence of the quadratic term ρ2\rho^{2} in the integral jk\mathcal{I}^{jk}, we cannot simply utilize the point-mass description and take the advantage of the delta function δ(𝒙)\delta(\bm{x}) to solve this integral. In this case, the integral (72) diverges. Therefore, to carry out our calculation, we consider compact bodies that are well separated. In the framework of this description, we have ρ=AρA\rho=\sum_{A}\rho_{A} in which ρA\rho_{A} is the density of the body AA and vanishes outside the volume VAV_{A} occupied by this body. We also introduce the vector 𝒙¯=𝒙𝒓A\bar{\bm{x}}=\bm{x}-\bm{r}_{A} that shows the fluid element position with respect to the center of mass of the body AA. This description is also mentioned in Appendix. D. Applying these definitions, for the second term of Eq. (72), we have

ρ2xjxkd3x\displaystyle\int_{\mathcal{M}}\rho^{2}x^{j}x^{k}d^{3}x 1ρ12(x¯j+r1j)(x¯k+r1k)d3x¯\displaystyle\simeq\int_{\mathcal{M}_{1}}\rho^{2}_{1}\big{(}\bar{x}^{j}+r_{1}^{j}\big{)}\big{(}\bar{x}^{k}+r_{1}^{k}\big{)}d^{3}\bar{x}
+2ρ22(x¯j+r2j)(x¯k+r2k)d3x¯.\displaystyle+\int_{\mathcal{M}_{2}}\rho^{2}_{2}\big{(}\bar{x}^{j}+r_{2}^{j}\big{)}\big{(}\bar{x}^{k}+r_{2}^{k}\big{)}d^{3}\bar{x}. (75)

In the above relation, the domain of the first integral is a sphere centered at the binary system’s center of mass with a radius |𝒙|<|\bm{x}|<\mathcal{R}. One can approximately simplify this integral in terms of the new domain A\mathcal{M}_{A} which this time is a sphere with a radius |𝒙¯|<|\bar{\bm{x}}|<\mathcal{R} and its center corresponds to the body AA’s center of mass. As the integrands are completely related to the matter sector, these domains are eventually restricted to the volumes occupied by these bodies. Therefore, we arrive at

ρ2xjxkd3x𝔐1r1jr1k\displaystyle\int_{\mathcal{M}}\rho^{2}x^{j}x^{k}d^{3}x\simeq\mathfrak{M}_{1}r_{1}^{j}r_{1}^{k} +𝔐2r2jr2k\displaystyle+\mathfrak{M}_{2}r_{2}^{j}r_{2}^{k}
+jk[cm1]+jk[cm2],\displaystyle+\mathfrak{I}^{jk}[\text{cm}_{1}]+\mathfrak{I}^{jk}[\text{cm}_{2}], (76)

where 𝔐A\mathfrak{M}_{A} and jk[cmA]\mathfrak{I}^{jk}[\text{cm}_{A}] are given by Eqs. (105a) and (105b). Here, “cmA\text{cm}_{A}” shows that the mentioned quantity is obtained with respect to the center of mass of the body AA. To simplify this relation, we consider the symmetry ρ(t,𝒓A𝒙¯)=ρ(t,𝒓A+𝒙¯)\rho(t,\bm{r}_{A}-\bar{\bm{x}})=\rho(t,\bm{r}_{A}+\bar{\bm{x}}). Following a similar computation for the first term in Eq. (72), we have

ρxjxkd3xm1r1jr1k\displaystyle\int_{\mathcal{M}}\rho\,x^{j}x^{k}d^{3}x\simeq m_{1}r_{1}^{j}r_{1}^{k} +m2r2jr2k\displaystyle+m_{2}r_{2}^{j}r_{2}^{k}
+Ijk[cm1]+Ijk[cm2],\displaystyle+I^{jk}[\text{cm}_{1}]+I^{jk}[\text{cm}_{2}], (77)

in which Ijk[cmA]=AρAx¯jx¯kd3x¯I^{jk}[\text{cm}_{A}]=\int_{A}\rho_{A}\bar{x}^{j}\bar{x}^{k}d^{3}\bar{x} is the quadrupole-moment tensor relative to the center of mass of the body AA. Gathering together the above results and applying Eq. (74a), we obtain jk\mathcal{I}^{jk} for the binary system as

jk\displaystyle\mathcal{I}^{jk} =(ηm+c2f01m2(𝔐1m22+𝔐2m12))rjrk\displaystyle=\Big{(}\eta m+c^{2}f_{0}^{\prime}\frac{1}{m^{2}}\big{(}\mathfrak{M}_{1}m_{2}^{2}+\mathfrak{M}_{2}m_{1}^{2}\big{)}\Big{)}r^{j}r^{k} (78)
+Ijk[cm1]+Ijk[cm2]+c2f0(jk[cm1]+jk[cm2]),\displaystyle+I^{jk}[\text{cm}_{1}]+I^{jk}[\text{cm}_{2}]+c^{2}f_{0}^{\prime}\big{(}\mathfrak{I}^{jk}[\text{cm}_{1}]+\mathfrak{I}^{jk}[\text{cm}_{2}]\big{)},

where η=m1m2/m2\eta=m_{1}m_{2}/m^{2}.

The next step toward finding 𝒫\mathcal{P} is to compute the time derivative of this quadrupole-moment tensor. To do so, we consider that the temporal variations of the internal tensors Ijk[cmA]I^{jk}[\text{cm}_{A}] and jk[cmA]\mathfrak{I}^{jk}[\text{cm}_{A}] are insignificant compared to those related to the orbital motion. Consequently, we set I˙jk[cmA]=0=˙jk[cmA]\dot{I}^{jk}[\text{cm}_{A}]=0=\dot{\mathfrak{I}}^{jk}[\text{cm}_{A}]. For the sake of simplification, we also assume that the density inside each body is uniform so that ρA=0\bm{\nabla}\rho_{A}=0. Under this condition, given the result of Appendix. C, we find that d𝔐A/dt=0d\mathfrak{M}_{A}/dt=0. Moreover, one can simplify the second term in Eq. (78) as (𝔐1m22+𝔐2m12)/m2=η(ρ1m2+ρ2m1)\big{(}\mathfrak{M}_{1}m_{2}^{2}+\mathfrak{M}_{2}m_{1}^{2}\big{)}/m^{2}=\eta\big{(}\rho_{1}m_{2}+\rho_{2}m_{1}\big{)}. Therefore, to complete our derivation, we only need to compute d3(rjrk)/dt3d^{3}(r^{j}r^{k})/dt^{3}. Since, we aim to obtain 𝒫\mathcal{P} to the leading order, we can use the Keplerian equations to describe the motion of the binary system. We consider that the orbit is in the (x,y)(x,y) plane. Consequently, we have

d3dt3(rjrk)\displaystyle\frac{d^{3}}{dt^{3}}\big{(}r^{j}r^{k}\big{)} =2(Gm)32l52(1+ecosφ)2[esinφnjnk\displaystyle=-2\frac{(Gm)^{\frac{3}{2}}}{l^{\frac{5}{2}}}\big{(}1+e\cos\varphi\big{)}^{2}\Big{[}e\sin\varphi\,n^{j}n^{k}
+2(1+ecosφ)(njλk+λjnk)],\displaystyle+2\big{(}1+e\cos\varphi\big{)}\big{(}n^{j}\lambda^{k}+\lambda^{j}n^{k}\big{)}\Big{]}, (79)

in which ll and ee are the semilatus rectum and eccentricity of the orbit, respectively. Here, 𝒏\bm{n} and 𝝀\bm{\lambda} are the orbital plane’s unit vectors of the binary system that are given by 𝒏=[cosφ,sinφ,0]\bm{n}=\big{[}\cos\varphi,\sin\varphi,0\big{]} and 𝝀=[sinφ,cosφ,0]\bm{\lambda}=\big{[}-\sin\varphi,\cos\varphi,0\big{]} where φ\varphi is the true anomaly. Inserting these results within Eq. (73), after some manipulations, we finally arrive at

𝒫=325η2G(Gmcl)5(1+2α)\displaystyle\mathcal{P}=\frac{32}{5}\frac{\eta^{2}}{G}\Big{(}\frac{G\,m}{c\,l}\Big{)}^{5}\Big{(}1+2\alpha\Big{)} (80)
×(1+ecosφ)4[1+2ecosφ+112e2(1+11cos2φ)],\displaystyle\times\big{(}1+e\cos\varphi\big{)}^{4}\Big{[}1+2e\cos\varphi+\frac{1}{12}e^{2}\big{(}1+11\cos^{2}\varphi\big{)}\Big{]},

in which

α=c2f0m(ρ1m2+ρ2m1).\displaystyle\alpha=\frac{c^{2}f_{0}^{\prime}}{m}\big{(}\rho_{1}m_{2}+\rho_{2}m_{1}\big{)}. (81)

Notice that given the EMSG correction α\alpha is a small parameter, |α|1|\alpha|\ll 1, we have expanded our results in powers of α\alpha, kept only linear terms in α\alpha, and then obtained Eq. (80). This relation describes the flux of energy in the EMSG theory. Obviously, dropping the EMSG correction α\alpha, the relation (80) reduces to the GR version. It should be emphasized that when the density inside each body is not uniform, this relation would dramatically change. In fact, in a more realistic case where ρ\rho is not constant, d𝔐A/dtd\mathfrak{M}_{A}/dt should be considered in calculating the EMSG energy flux.

In order to visualize the effect of the EMSG correction on 𝒫\mathcal{P}, we display Eq. (80) in Fig. 1. To do so, we choose a specific case e=0.7e=0.7 and then numerically solve φ˙=(Gm/l3)1/2(1+ecosφ)2\dot{\varphi}=\big{(}Gm/l^{3}\big{)}^{1/2}(1+e\cos\varphi)^{2} in terms of the retarded time. Here, we also assume that the density of the two bodies in the binary system is of the same order and it is constant. We set ρ1=ρ2=ρ\rho_{1}=\rho_{2}=\rho. Under this assumption, the EMSG correction (81) reduces to α=c2f0ρ\alpha=c^{2}f_{0}^{\prime}\rho. As seen from this figure, even for the small value of α\alpha, the flux of energy near the pericenter of the orbit dramatically changes comparing with the GR one. Therefore, one may conclude that studying this relation could strongly restrict the free parameter of this theory f0f_{0}^{\prime}. In the following section, by studying the post-Keplerian parameter, the time derivative of the orbital period P˙\dot{P}, 777Notice that hereafter, the symbol PP stands for the orbital period and almost the same symbol 𝒫\mathcal{P} represents the flux of energy. of several binary pulsars, we attempt to find a bound on f0f_{0}^{\prime}.

Refer to caption
Figure 1: The scaled flux of energy 𝒫(5/32)(G/η2)(cl/Gm)5\mathcal{P}(5/32)(G/\eta^{2})(c\,l/G\,m)^{5} in terms of the scaled retarded time τ/P\tau/P where PP is the orbital period. Here, we assume that e=0.7e=0.7. In this figure, α\alpha shows the EMSG correction. We see that near the pericenter, even for a rather small value of α\alpha, the flux of energy changes considerably comparing with the GR case with α=0\alpha=0.

As a final point in this section, let us return to the energy flux derived in Eq. (80). As shown, in the EMSG theory, this relation depends on the densities of each component of the binary system in addition to their masses. So, for dense systems like double-neutron star binaries, the EMSG correction will be considerable. On the other hand, it means that the gravitational radiation in this theory may implicitly be affected by the internal structure of each component. Now the question is whether it can be a consequence of the violation of the Strong Equivalence Principle (SEP) in this theory. To demonstrate the latter state, we consider the near-zone metric obtained in Sec. IV.2, cf. Eqs. (40a)-(40c). According to the relations represented in Appendix. D, one can show that in the framework of the N-body description, for instance, the time-time component of the spacetime metric outside a single sphere with mass mm and constant density ρ\rho is given by g00=1+2Gm/(rc2)(1+4c2f0ρ)g_{00}=-1+2G\,m/(rc^{2})\big{(}1+4c^{2}f_{0}^{\prime}\rho\big{)}. It illustrates that two compact stars with the same rest mass mm but different densities would induce different spacetimes. In other words, not only their mass but also their density could affect the trajectory of a test particle Nazari (2022). This reveals that the interior of the bodies could play a role here. Therefore, we conclude that SEP is indeed violated in this theory. This is expected in the sense that the standard conservation equation for TμνT_{\mu\nu} does not hold in EMSG. This means that particles do not necessarily move on geodesics. More specifically, the internal properties of the massive bodies appear at the right-hand side of the conservation equation. It should be mentioned that to examine the bodies’ internal structure on the near-zone spacetime completely, one should at least find the metric up to the second iteration where the required PN order is faithfully constructed.

VI Application to the binary pulsars

Table 1: The binary pulsars and their characteristics
System PP ee mpm_{\text{p}} mcm_{\text{c}} P˙obs\dot{P}_{\text{obs}} ±δ\pm\delta P˙GR\dot{P}_{\text{GR}} References
(d)(\text{d}) (M)(M_{\odot}) (M)(M_{\odot}) (×1012)(\times 10^{-12}) (×1012)(\times 10^{-12}) (×1012)(\times 10^{-12})
J2129+1210C 0.335 282 0490.335\,282\,049 0.681 3950.681\,395 1.358 1.354 3.96-3.96 0.05 3.94-3.94 Jacoby et al. (2006)
J1915+1606 0.322 997 4490.322\,997\,449 0.617 13340.617\,1334 1.4398 1.3886 2.423-2.423 0.001 2.403-2.403 Hulse and Taylor (1975); Weisberg et al. (2010)
J0737-3039A 0.102 251 5620.102\,251\,562 0.087 77750.087\,7775 1.3381 1.2489 1.252-1.252 0.017 1.248-1.248 Kramer et al. (2006)
J1537+1155 0.420 737 2990.420\,737\,299 0.273 67670.273\,6767 1.3332 1.3452 0.138-0.138 0.0001 0.192-0.192 Stairs et al. (2002)
J1141-6545 0.197 650 9590.197\,650\,959 0.171 8840.171\,884 1.27 1.02 0.403-0.403 0.025 0.387-0.387 Bhat et al. (2008)
J1738+0333 0.354 790 73990.354\,790\,7399 3.4×1073.4\times 10^{-7} 1.46 0.181 0.017-0.017 0.0031 0.0277-0.0277 Freire et al. (2012)

As an application of our derivation, we investigate the EMSG effect on the time average of the power radiated due to GWs of the binary system. Then, applying this relation, we study the EMSG version of the post-Keplerian parameter P˙\dot{P}. As the orbital period variation is the best-observed parameter, we choose this post-Keplerian parameter to find a reasonable restriction on the free parameter of the EMSG theory. Of course, to examine the EMSG relativistic effects comprehensively, the other post-Keplerian parameters should also be studied. Moreover, studying all post-Keplerian parameters, one can check the self-consistency of the theory. e.g., in the case of the tensor-scalar theories of gravity, see Bhat et al. (2008); Freire et al. (2012); Damour and Esposito-Farese (1996). We next find P˙EMSG\dot{P}_{\text{\tiny EMSG}} of several known binary pulsars; and by comparing our result with their observed orbital period variation P˙obs\dot{P}_{\text{obs}}, we try to set a bound on f0f_{0}^{\prime}.

Regarding Eq. (80), we obtain the orbital average of the flux of energy, <𝒫>\big{<}\mathcal{P}\big{>}, and then according to the energy-balance equation (21), we arrive at

<dEdt>=325η2G(Gmcl)5(1+2α)\displaystyle\Big{<}\frac{dE}{dt}\Big{>}=-\frac{32}{5}\frac{\eta^{2}}{G}\Big{(}\frac{G\,m}{c\,l}\Big{)}^{5}\Big{(}1+2\alpha\Big{)}
×(1e2)32[1+7324e2+3796e4],\displaystyle\times\big{(}1-e^{2})^{\frac{3}{2}}\Big{[}1+\frac{73}{24}e^{2}+\frac{37}{96}e^{4}\Big{]}, (82)

for the time average of the radiated power. Inserting the orbital energy and the Kepler third law into the above relation yields

P˙EMSG=192π5(GMc32πP)53(1+2α)\displaystyle\dot{P}_{\text{\tiny EMSG}}=-\frac{192\pi}{5}\Big{(}\frac{GM}{c^{3}}\frac{2\pi}{P}\Big{)}^{\frac{5}{3}}\Big{(}1+2\alpha\Big{)}
×(1e2)72[1+7324e2+3796e4],\displaystyle\times\big{(}1-e^{2})^{-\frac{7}{2}}\Big{[}1+\frac{73}{24}e^{2}+\frac{37}{96}e^{4}\Big{]}, (83)

for the first time derivative of the orbital period PP. Here, M=η3/5mM=\eta^{3/5}m is the chirp mass. As seen, the quadrupolar gravitational radiation in the EMSG theory is obviously dictated in this post-Keplerian parameter. Therefore, this relativistic parameter can be a sound test bed for this theory.

Given the sign of f0f_{0}^{\prime}, P˙EMSG\dot{P}_{\text{\tiny EMSG}} can be smaller or larger than the GR case P˙GR\dot{P}_{\text{GR}}. Here, we assume that the free parameter of the theory can take both positive and negative values. In Akarsu et al. (2018b), by studying the masses and radii of neutron stars, a bound on the EMSG parameter is fixed. It is shown that 1037ms2kg1<f0<+1036ms2kg1-10^{-37}\,\text{m}\,\text{s}^{2}\,\text{kg}^{-1}<f_{0}^{\prime}<+10^{-36}\,\text{m}\,\text{s}^{2}\,\text{kg}^{-1}. This limitation is also consistent with what is provided in Nari and Roshan (2018). Applying this bound, we examine the time derivative of the orbital period for the well-known Hulse-Taylor binary pulsar, J1915+1606, in EMSG. To do so, we consider that the density of both the pulsar and the companion is of the order of the neutron star density 1017kgm3\sim 10^{17}\,\text{kg}\,\text{m}^{-3}. In this case, we find that 2.447×1012<P˙EMSG<2.399×1012-2.447\times 10^{-12}<\dot{P}_{\text{\tiny EMSG}}<-2.399\times 10^{-12}. On the other hand, the observed orbital period variation of this system is of the order P˙obs=2.423×1012\dot{P}_{\text{obs}}=-2.423\times 10^{-12} Hulse and Taylor (1975); Weisberg et al. (2010). So, one can conclude that, at least this specific binary system does not rule out EMSG.

We apply the method described in De Laurentis and De Martino (2013) to restrict the EMSG parameter. We consider that the EMSG orbital period variation could fully justify the observed one, i.e., we set P˙EMSG=P˙obs\dot{P}_{\text{\tiny EMSG}}=\dot{P}_{\text{obs}} or equivalently P˙GR(1+2α)=P˙obs\dot{P}_{\text{GR}}\big{(}1+2\alpha\big{)}=\dot{P}_{\text{obs}}. So, the free parameter f0f_{0}^{\prime} is restricted as

f0=12c2m(ρ1m2+ρ2m1)[(P˙obsP˙GR)1].\displaystyle{f_{0}^{\prime}}=\frac{1}{2c^{2}}\frac{m}{\big{(}\rho_{1}m_{2}+\rho_{2}m_{1}\big{)}}\Big{[}\Big{(}\frac{\dot{P}_{\text{obs}}}{\dot{P}_{\text{GR}}}\Big{)}-1\Big{]}. (84)

Moreover, we assume that uncertainty on f0f_{0}^{\prime} is given by

f0±δ=12c2m(ρ1m2+ρ2m1)[(P˙obs±δP˙GR)1],\displaystyle{f_{0}^{\prime}}_{\pm\delta}=\frac{1}{2c^{2}}\frac{m}{\big{(}\rho_{1}m_{2}+\rho_{2}m_{1}\big{)}}\Big{[}\Big{(}\frac{\dot{P}_{\text{obs}}\pm\delta}{\dot{P}_{\text{GR}}}\Big{)}-1\Big{]}, (85)

where δ\delta shows the experimental error on P˙obs\dot{P}_{\text{obs}}. Here, we do not add the contributions resulting from the Galactic and kinematic/Shklovskii accelerations, P˙Gal\dot{P}_{\text{Gal}} and P˙kin\dot{P}_{\text{kin}} Damour and Taylor (1991), to the orbital decay. After these values are provided in the literature, the ratio P˙obs/P˙GR\dot{P}_{\text{obs}}/\dot{P}_{\text{GR}} in Eq. (84) should be changed to (P˙obsP˙GalP˙kin)/P˙GR\big{(}\dot{P}_{\text{obs}}-\dot{P}_{\text{Gal}}-\dot{P}_{\text{kin}}\big{)}/\dot{P}_{\text{GR}}. We select the binary pulsars whose characteristics like the mass of pulsar mpm_{\text{p}} and mass of companion mcm_{\text{c}}, orbital eccentricity ee, orbital period PP, and observed orbital period deviation are introduced with a good precision in the literature. In Table 1, the J-name of these binary pulsars and their characteristics needed during our calculations are shown. For the first relativistic binary pulsar, J2129+1210C, we exhibit our method in Fig. 2. As seen in this figure, the function P˙EMSG\dot{P}_{\text{\tiny EMSG}} intersects the horizontal line of P˙obs\dot{P}_{\text{obs}}. This point is indicated with the green arrow. Therefore, for this value of f0f_{0}^{\prime}, this theory can justify the observed orbital period variation. Here, we assume that the density of both neutron stars in this binary pulsar is of the order 1017kgm310^{17}\,\text{kg}\,\text{m}^{-3}. Moreover, the upper and lower limits of this parameter are obtained according to Eq. (85). These are also displayed with the blue arrows. Furthermore, one can see that for the value f0=0f_{0}^{\prime}=0, our result reduces to the GR case. We display this with f0GR=0{f_{0}^{\prime}}_{\text{GR}}=0 in this figure.

Refer to caption
Figure 2: The orbital period variation of the double neutron star binary pulsar J2129+1210C. In this figure, the green dot-dashed line shows P˙EMSG\dot{P}_{\text{\tiny EMSG}} in terms of f0f_{0}^{\prime}. cf. Eq. (VI). We also insert P˙GR\dot{P}_{\text{GR}} and P˙obs\dot{P}_{\text{obs}} in this plot. Where the P˙EMSG\dot{P}_{\text{\tiny EMSG}} line intersects the blue solid and red dashed lines indicates f0f_{0}^{\prime} and f0GR{f_{0}^{\prime}}_{\text{GR}}, respectively. Moreover, the upper and lower limits of f0f_{0}^{\prime} are obtained from the intersection of the green dot-dashed and blue dotted lines. The numerical values of these are given in Table 2.

A similar interpretation is applied for the rest of the binary pulsars. The results are summarized in Table 2. In this table, for each system, we obtain a numerical value for f0f_{0}^{\prime} which satisfies the observed results. For the double neutron star binary pulsars, we set ρ1=ρ2=1017kgm3\rho_{1}=\rho_{2}=10^{17}\,\text{kg}\,\text{m}^{-3}; and for the last two systems in this table, which are the pulsar-white-dwarf binaries, we consider that the density of pulsar and companion is of the order 101710^{17} and 109kgm310^{9}\,\text{kg}\,\text{m}^{-3}, respectively. Also, we introduce the interval f0\triangle f_{0}^{\prime} as |f0+δf0δ|/2|{f_{0}^{\prime}}_{+\delta}-{f_{0}^{\prime}}_{-\delta}|/2. In fact, twice this interval shows where P˙EMSG\dot{P}_{\text{\tiny EMSG}} would intersect the observed case.

The first three systems reveal that the f0f_{0}^{\prime} value of the order 1037ms2kg110^{-37}\,\text{m}\,\text{s}^{2}\,\text{kg}^{-1} improves the theoretical predictions. In fact, in these cases, the same order of the EMSG parameter can fill the gap between the observed results and the GR predictions. On the other hand, the next double neutron star binary pulsar, J1537+1155, behaves differently. For this relativistic system, we find that f0{f_{0}^{\prime}} is negative and its value is different from that of the previous double neutron star binary pulsars. However, it is necessary to emphasize that for this system, the percent error |(P˙obsP˙GR)/P˙GR|×100|(\dot{P}_{\text{obs}}-\dot{P}_{\text{GR}})/\dot{P}_{\text{GR}}|\times 100 is about 28%28\%, while the percent error of the previous systems is less than 1%1\%, making it of less interest and reliability in this investigation. Modifying Eq. (84) by inserting P˙Gal=(0.037±0.011)×1012\dot{P}_{\text{Gal}}=(0.037\pm 0.011)\times 10^{-12} Stairs et al. (2002) for J1537+1155 improves the results and increases f0{f_{0}^{\prime}} up to 2.46×1036ms2kg1-2.46\times 10^{-36}\,\text{m}\,\text{s}^{2}\text{kg}^{-1}. Moreover, we simply assume that the density of the components is constant with the order 1017kgm310^{17}\,\text{kg}\,\text{m}^{-3}. For the higher density range, f0{f_{0}^{\prime}} deduced from J1537+1155 may also enter the mentioned bound.

For the last two pulsar-white-dwarf binaries, J1141-6545 and J1738+0333, we assume that the white dwarf density is of the order 109kgm310^{9}\,\text{kg}\,\text{m}^{-3}. For these two cases, one can see that the value of f0{f_{0}^{\prime}} is not of the order of the first three cases. It can be a result of the effect of the Galactic and kinematic accelerations, the constant density assumption, or the magnitude of the density inside these systems. To clarify the latter fact, we study Eq. (84) for the different range of f0f_{0}^{\prime} and ρ\rho in Fig. 3. It should be mentioned in the case of white-dwarf-pulsar binaries, we assume that the density of the companion is of the order 109kgm310^{9}\,\text{kg}\,\text{m}^{-3}, and we consider that the density of the pulsar can change between 10178×1017kgm310^{17}-8\times 10^{17}\,\text{kg}\,\text{m}^{-3}. For Four binary pulsars J2129+1210C, J1915+1606, J0737-3039A, and J1141-6545, we obtain reliable values for f0f_{0}^{\prime} in terms of ρ\rho. As seen, the value of f0f_{0}^{\prime} is completely sensitive to the density, and at the high-density regime, it decreases to 11 order of magnitude. We also find that the binary pulsars J1537+1155 and J1738+0333 have no solution in the range shown in this figure. It should be emphasized that for these systems, the percent error |(P˙obsP˙GR)/P˙GR|×100|(\dot{P}_{\text{obs}}-\dot{P}_{\text{GR}})/\dot{P}_{\text{GR}}|\times 100 is more than 25%25\%. Because of this high percent error, we ignore these two systems in the following analysis and focus our attention on the rest systems in Table 2 where the percent error is less than 5%5\%.

Table 2: The value of the EMSG parameter and its uncertainty by analyzing the orbital decay of the specific binary pulsars. In SI units, the dimension of this parameter is ms2kg1\text{m}\,\text{s}^{2}\text{kg}^{-1}. It should be mentioned, the best previous constraint on f0f_{0}^{\prime} is introduced in Akarsu et al. (2018b) which is in the range 1037ms2kg1<f0<+1036ms2kg1-10^{-37}\text{m}\,\text{s}^{2}\text{kg}^{-1}<f_{0}^{\prime}<+10^{-36}\text{m}\,\text{s}^{2}\text{kg}^{-1}.
System f0{f_{0}^{\prime}} f0+δ{f_{0}^{\prime}}_{+\delta} f0δ{f_{0}^{\prime}}_{-\delta} f0\triangle{f_{0}^{\prime}}
(×1037)(\times 10^{-37}) (×1037)(\times 10^{-37}) (×1037)(\times 10^{-37}) (×1037)(\times 10^{-37})
J2129+1210C 2.82 4.24-4.24 9.89 7.06
J1915+1606 4.49 4.25 4.72 0.23
J0737-3039A 1.64 5.94-5.94 9.23 7.58
J1537+1155 157.54-157.54 157.83-157.83 157.25-157.25 0.29
J1141-6545 52.02 28.69-28.69 132.73 80.71
J1738+0333 1922.75-1922.75 2491.89-2491.89 1353.62-1353.62 569.13
Refer to caption
Figure 3: The free parameter of the EMSG theory in terms of the density of the neutron star. Here, we consider that the density can change in the interval (10178×1017)kgm3(10^{17}-8\times 10^{17})\,\text{kg}\,\text{m}^{-3}. Here, f0{f_{0}^{\prime}} is displayed for the introduced relativistic binary pulsars. The colored solid and dashed curves represent the solutions (84) and (85), respectively. Here, we show the range of f0f_{0}^{\prime} where most of the systems behave similarly. We find that the binary pulsars J1537+1155 and J1738+0333 have no solution in this range. Also, the dashed curves belonging to J1141-6545 do not enter this range.

VII Conclusion

Refer to caption
Figure 4: The absolute value of the free parameter of the EMSG theory in terms of the percent error |(P˙obsP˙GR)/P˙GR|×100|(\dot{P}_{\text{obs}}-\dot{P}_{\text{GR}})/\dot{P}_{\text{GR}}|\times 100. For the sake of convenience, the horizontal axis is scaled logarithmically. Here, except for J1141-6545\text{J}1141\text{-}6545*, we consider that the density of the neutron star is of the order 1017kgm310^{17}\text{kg}\,\text{m}^{-3}. For J1141-6545\text{J}1141\text{-}6545*, we assume that the density of the pulsar is of the order 6×1017kgm36\times 10^{17}\text{kg}\,\text{m}^{-3}. The horizontal lines, from top to bottom, represent the percent error 5%5\% and 1%1\%, respectively. Moreover, the colored area shows the allowed region for f0f_{0}^{\prime} introduced in Akarsu et al. (2018b). Four cases J0737-3039A, J2129+1210C, J1915+1606, and J1141-6545\text{J}1141\text{-}6545* are well located in this region. These systems are displayed by the black circle. The rest systems where the percent error is more than 5%5\% are indicated by the red square.

In this paper, we have introduced the PM approximation of EMSG. Utilizing this approximation, the gravitational energy flux has been studied in this theory. As an application of our derivation, we have investigated the EMSG effect on the post-Keplerian parameter P˙\dot{P}. Comparing P˙EMSG\dot{P}_{\text{EMSG}} with P˙obs\dot{P}_{\text{obs}} of six binary pulsars categorized in Table 1, the free parameter of the EMSG theory has been fixed. The results are summarized in Table 2.

It has been shown that for the first three binary pulsars in this table, the parameter f0f_{0}^{\prime} is of the order of 1037ms2kg110^{-37}\,\text{m}\,\text{s}^{2}\text{kg}^{-1}. In other words, for this value of the EMSG parameter, the gap between the observed results and the GR predictions can be filled. However, the order of magnitude of f0f_{0}^{\prime} is quite different for the next three binary pulsars. This discrepancy is visualized in Fig. 4. In this figure, the absolute value of f0f_{0}^{\prime}s in terms of |(P˙obsP˙GR)/P˙GR|×100|(\dot{P}_{\text{obs}}-\dot{P}_{\text{GR}})/\dot{P}_{\text{GR}}|\times 100 for the six binary pulsars is displayed.

Some assumptions taken during our derivation can be the origin of this discrepancy. As mentioned, we have considered that the density of the binary components is constant, and for the neutron star, we set ρ=1017kgm3\rho=10^{17}\,\text{kg}\,\text{m}^{-3}. On the other hand, determining the EMSG parameter strongly depends on the density of the subject system. We have shown that increasing the density to 8×1017kgm38\times 10^{17}\,\text{kg}\,\text{m}^{-3}, the value of f0f_{0}^{\prime} can change about 1 order of magnitude. In Figs. 3 and 4, it is exhibited that at the higher density range, the binary pulsar J1141-6545 may also behave like the first three so that f0f_{0}^{\prime} enters the range <1036ms2kg1<10^{-36}\,\text{m}\,\text{s}^{2}\text{kg}^{-1}. This case is displayed by an asterisk in the J-name of this binary pulsar in Fig. 4.

In addition, another reason for this discrepancy may be the mass dependence of f0f_{0}^{\prime}. In Eq. (84), we have illustrated that the mass-dependent terms exist in the definition of f0f_{0}^{\prime}. Notice that some part of this dependency lies in P˙GR\dot{P}_{\text{GR}}. So, in an accurate analysis to determine f0f_{0}^{\prime}, one needs to study the mass of the binary components in the EMSG framework. To do so, one should obtain the other post-Keplerian parameters in EMSG. In this paper, as the first step to estimate the order of the free parameter in this theory by studying P˙\dot{P}, we have utilized the masses derived in the GR context. We leave the complete analysis for future work.

More importantly, other causes may come from the considerable contributions of the Galactic and kinematic/Shklovskii accelerations to the orbital decay Damour and Taylor (1991). In this case, the ratio P˙obs/P˙EMSG\dot{P}_{\text{obs}}/\dot{P}_{\text{EMSG}} can dramatically change and affect the value of f0f_{0}^{\prime}. We have argued that by adding the Galactic acceleration, the value of f0f_{0}^{\prime} obtained from the system J1537+1155 is improved so that it approaches that of the first three systems. So, to estimate the free parameter of EMSG truly, besides obtaining the mass and density of the binary components more accurately, we need to consider the role of the Galactic and kinematic/Shklovskii accelerations. So, to estimate the value of f0f_{0}^{\prime}, we ignore systems with high percent error and focus our attention on the rest systems where the percent error is less than 5%5\%.

Refer to caption
Figure 5: The value of f0f_{0}^{\prime} and its error bar for the systems with percent error <5%<5\%. The dashed lines show the estimated bound for f0f_{0}^{\prime}. Here, we choose the worse error to estimate this bound. The blue dashed lines represent the region deduced from the four systems and the red ones exhibit the bound found from the binary pulsars J2129+1210C, J1915+1606, and J0737-3039A.

Figure. 5 represents the value of f0f_{0}^{\prime} and its error bar for the systems with percent error <5%<5\%. As seen from this figure, for the binary pulsars J2129+1210C, J1915+1606, and J0737-3039A with the percent error less than 1%1\%, for f0<1036f_{0}^{\prime}<10^{-36}, one can fill the gap between the observed results and the GR predictions. Considering the error bars, we conclude that 6×1037ms2kg1<f0<+1036ms2kg1-6\times 10^{-37}\text{m}\,\text{s}^{2}\text{kg}^{-1}<f_{0}^{\prime}<+10^{-36}\text{m}\,\text{s}^{2}\text{kg}^{-1} from these binary pulsars. This constraint on f0f_{0}^{\prime} is in agreement with the specified range 1037ms2kg1<f0<+1036ms2kg1-10^{-37}\text{m}\,\text{s}^{2}\text{kg}^{-1}<f_{0}^{\prime}<+10^{-36}\text{m}\,\text{s}^{2}\text{kg}^{-1} introduced in Akarsu et al. (2018b). On the other hand, adding J1141-6545, one can estimate 2.8×1036ms2kg1f0+1.3×1035ms2kg1-2.8\times 10^{-36}\text{m}\,\text{s}^{2}\text{kg}^{-1}\leq f_{0}^{\prime}\leq+1.3\times 10^{-35}\text{m}\,\text{s}^{2}\text{kg}^{-1} for the range of the free parameter of theory. Although, because of the different nature of this white-dwarf-pulsar binary from the first three systems, more effects like the mass transfer in the binary system and the accurate density of the components should be considered. In conclusion, the first three binary pulsars in Table 2 do not rule out the theory, and by analyzing these system, we estimate that the bound 6×1037ms2kg1<f0<+1036ms2kg1-6\times 10^{-37}\text{m}\,\text{s}^{2}\text{kg}^{-1}<f_{0}^{\prime}<+10^{-36}\text{m}\,\text{s}^{2}\text{kg}^{-1} for the free parameter of EMSG. However, for the last three binaries where the percent error is high, further study on the density, the mass of the binary pulsar components, (in the case of white-dwarf-pulsar binaries) the hydrodynamics effects due to the mass transfer, and the contributions of the Galactic and kinematic/Shklovskii accelerations to the orbital decay are required to improve the free parameter estimation.

ACKNOWLEDGMENTS

We thank the anonymous referees for their useful and constructive comments and for introducing related references. This work is supported by Ferdowsi University of Mashhad under Grant No. 1/53355 (09/10/1399). I.D.M acknowledges support from MICINN (Spain) under de project IJCI2018-036198-I. I.D.M is also supported by Junta de Castilla y León (SA096P20), and Spanish Ministerio de Ciencia, Innovación y Universidades and FEDER (PGC2018-096038-B-I00).

References

  • Clifton et al. (2012) T. Clifton, P. G. Ferreira, A. Padilla,  and C. Skordis, Phys. Rept. 513, 1 (2012).
  • Milgrom (1983) M. Milgrom, ApJ 270, 365 (1983).
  • Salucci et al. (2021) P. Salucci, G. Esposito, G. Lambiase, E. Battista, M. Benetti, D. Bini, L. Boco, G. Sharma, V. Bozza, L. Buoninfante, et al., Front. Phys. 8, 579 (2021).
  • de Martino et al. (2020) I. de Martino, S. S. Chakrabarty, V. Cesare, A. Gallo, L. Ostorero,  and A. Diaferio, Universe 6, 107 (2020).
  • Hehl and Mashhoon (2009) F. W. Hehl and B. Mashhoon, Phys. Lett. B 673, 279 (2009).
  • Moffat (2006) J. W. Moffat, JCAP 2006, 004 (2006).
  • Abbott et al. (2017a) B. Abbott, R. Abbott, T. Abbott, F. Acernese, C. Adams, T. Adams, P. Addesso, R. Adhikari, V. Adya, C. Affeldt, et al., ApJL 848, L12 (2017a).
  • Abbott et al. (2017b) B. P. Abbott, R. Abbott, T. Abbott, F. Acernese, K. Ackley, C. Adams, T. Adams, P. Addesso, R. Adhikari, V. Adya, et al., PhRvL 119, 161101 (2017b).
  • Ezquiaga and Zumalacárregui (2017) J. M. Ezquiaga and M. Zumalacárregui, PhRvL 119, 251304 (2017).
  • Boran et al. (2018) S. Boran, S. Desai, E. Kahya,  and R. Woodard, PhRvD 97, 041501 (2018).
  • De Laurentis and De Martino (2013) M. De Laurentis and I. De Martino, MNRAS 431, 741 (2013).
  • De Laurentis and Capozziello (2011) M. De Laurentis and S. Capozziello, Astropart. Phys. 35, 257 (2011).
  • De Laurentis and De Martino (2015) M. De Laurentis and I. De Martino, Int. J. Geom. Meth. Mod. Phys. 12, 1550040 (2015).
  • Jimenez et al. (2016) J. B. Jimenez, F. Piazza,  and H. Velten, PhRvL 116, 061101 (2016).
  • Hulse and Taylor (1975) R. A. Hulse and J. H. Taylor, ApJ 195, L51 (1975).
  • Will and Wiseman (1996) C. M. Will and A. G. Wiseman, PhRvD 54, 4813 (1996).
  • Pati and Will (2000) M. E. Pati and C. M. Will, PhRvD 62, 124015 (2000).
  • Pati and Will (2002) M. E. Pati and C. M. Will, PhRvD 65, 104008 (2002).
  • Roshan and Shojai (2016) M. Roshan and F. Shojai, PhRvD 94, 044002 (2016).
  • Katırcı and Kavuk (2014) N. Katırcı and M. Kavuk, Eur. Phys. J. Plus 129, 1 (2014).
  • Barbar et al. (2020) A. H. Barbar, A. M. Awad,  and M. T. AlFiky, PhRvD 101, 044058 (2020).
  • Nazari et al. (2020) E. Nazari, F. Sarvi,  and M. Roshan, PhRvD 102, 064016 (2020).
  • Akarsu et al. (2020) Ö. Akarsu, J. D. Barrow,  and N. M. Uzun, PhRvD 102, 124059 (2020).
  • Akarsu et al. (2018a) Ö. Akarsu, N. Katırcı,  and S. Kumar, PhRvD 97, 024011 (2018a).
  • Bahamonde et al. (2019) S. Bahamonde, M. Marciu,  and P. Rudra, PhRvD 100, 083511 (2019).
  • Shahidi (2021) S. Shahidi, Eur. Phys. J. C 81, 1 (2021).
  • Moraes and Sahoo (2018) P. Moraes and P. Sahoo, PhRvD 97, 024007 (2018).
  • Faria et al. (2019) M. Faria, C. Martins, F. Chiti,  and B. Silva, A&A 625, A127 (2019).
  • Sharif and Gul (2021) M. Sharif and M. Z. Gul, Eur. Phys. J. Plus 136, 1 (2021).
  • Nazari (2022) E. Nazari, “The bending of light and gravitational microlensing in energy-momentum-squared gravity,” work in preparation (2022).
  • Schutz Jr. (1970) B. F. Schutz Jr., PhRvD 2, 2762 (1970).
  • Brown (1993) J. D. Brown, CQG 10, 1579 (1993).
  • Faraoni (2009) V. Faraoni, PhRvD 80, 124040 (2009).
  • Bertolami et al. (2008) O. Bertolami, F. S. Lobo,  and J. Páramos, PhRvD 78, 064036 (2008).
  • Poisson and Will (2014) E. Poisson and C. M. Will, Gravity: Newtonian, Post-Newtonian, Relativistic (Cambridge University Press, 2014).
  • Will (2018) C. M. Will, Theory and experiment in gravitational physics (Cambridge university press, 2018).
  • Jacoby et al. (2006) B. A. Jacoby, P. Cameron, F. Jenet, S. Anderson, R. Murty,  and S. Kulkarni, ApJL 644, L113 (2006).
  • Weisberg et al. (2010) J. M. Weisberg, D. J. Nice,  and J. H. Taylor, ApJ 722, 1030 (2010).
  • Kramer et al. (2006) M. Kramer, I. H. Stairs, R. Manchester, M. McLaughlin, A. Lyne, R. Ferdman, M. Burgay, D. Lorimer, A. Possenti, N. D’Amico, et al., Sci 314, 97 (2006).
  • Stairs et al. (2002) I. Stairs, S. Thorsett, J. Taylor,  and A. Wolszczan, ApJ 581, 501 (2002).
  • Bhat et al. (2008) N. R. Bhat, M. Bailes,  and J. P. Verbiest, PhRvD 77, 124017 (2008).
  • Freire et al. (2012) P. C. Freire, N. Wex, G. Esposito-Farèse, J. P. Verbiest, M. Bailes, B. A. Jacoby, M. Kramer, I. H. Stairs, J. Antoniadis,  and G. H. Janssen, MNRAS 423, 3328 (2012).
  • Damour and Esposito-Farese (1996) T. Damour and G. Esposito-Farese, PhRvD 54, 1474 (1996).
  • Akarsu et al. (2018b) Ö. Akarsu, J. D. Barrow, S. Çıkıntoğlu, K. Y. Ekşi,  and N. Katırcı, PhRvD 97, 124017 (2018b).
  • Nari and Roshan (2018) N. Nari and M. Roshan, PhRvD 98, 024031 (2018).
  • Damour and Taylor (1991) T. Damour and J. H. Taylor, ApJ 366, 501 (1991).

Appendix A Symbols and Acronyms

In this appendix, for the convenience of the reader, symbols and acronyms are summarized in Tables. 3 and 4.

Table 3: List of abbreviations frequently used in the paper.
Acronyms Extended name
GR General theory of relativity
GW Gravitational wave
EMSG Energy-momentum-squared gravity
PM Post-Minkowskian
T-T Transverse-tracefree
PN Post-Newtonian
cmA\text{cm}_{A} Center of mass of the body AA
SEP Strong equivalence principle
Table 4: List of symbols used in the paper.
Symbols Explanation
𝑻2{\bm{T}}^{2} TαβTαβT^{\alpha\beta}T_{\alpha\beta}
TeffμνT_{\text{eff}}^{\mu\nu} Effective energy-momentum tensor
𝔤μν\mathfrak{g}^{\mu\nu} Gothic metric defined by ggμν\sqrt{-g}g^{\mu\nu}
hμνh^{\mu\nu} Gravitational potential
τeffμν\tau^{\mu\nu}_{\text{eff}} Effective energy-momentum pseudotensor
(g)tLLμν(-g)t_{\text{LL}}^{\mu\nu} Landau-Lifshitz pseudotensor
(g)tHμν(-g)t_{\text{H}}^{\mu\nu} Harmonic pseudotensor
PαP^{\alpha} Total four-vector momentum
f0f^{\prime}_{0} Free parameter of the EMSG theory
𝒫\mathcal{P} Flux of energy
PP Orbital period of binary system
λc\lambda_{c} Characteristic wavelength of the GW signals
τ\tau Retarded time
ρ\rho Mass density
ρ\rho^{*} Rescaled mass density
ϵ\epsilon Proper internal energy density
pp Pressure
Π\Pi Fluid’s internal energy per unit mass
cc Speed of light
UU Newtonian potential
UEMSU_{\text{\tiny EMS}} EMSG potential defined in Eq. (34b)
\mathcal{M} Three-dimension sphere separating
the near zone from the wave zone
\mathcal{R} Radius of \mathcal{M}
\partial\mathcal{M} Boundary of \mathcal{M}
𝒩\mathcal{N} Near zone
𝒲\mathcal{W} Wave zone
𝔐\mathfrak{M} New quantity in EMSG defined in Eq. (39)
M0M_{0} Total matter inside the near zone
𝔓j\mathfrak{P}^{j} New quantity in EMSG defined in Eq. (64)
P0jP_{0}^{j} Near-zone momentum
MM Chirp mass
ll Semilatus rectum of the orbit
ee Orbital eccentricity

Appendix B Essential Relations

In this Appendix, we introduce the essential relations required to study the balance-energy equation in the context of the EMSG theory. The first one is the definition of the Landau-Lifshitz pseudotensor (g)tLLαβ(-g)t_{\text{LL}}^{\alpha\beta}. Its general definition in terms of the gothic metric 𝔤αβ\mathfrak{g}^{\alpha\beta} is given by

(g)tLLαβ=\displaystyle(-g)t_{\text{LL}}^{\alpha\beta}= c416πG{λ𝔤αβμ𝔤λμλ𝔤αλμ𝔤βμ+12gαβgλμρ𝔤λνν𝔤μρgαλgμνρ𝔤βνλ𝔤μρgβλgμνρ𝔤ανλ𝔤μρ\displaystyle\frac{c^{4}}{16\pi G}\bigg{\{}\partial_{\lambda}\mathfrak{g}^{\alpha\beta}\partial_{\mu}\mathfrak{g}^{\lambda\mu}-\partial_{\lambda}\mathfrak{g}^{\alpha\lambda}\partial_{\mu}\mathfrak{g}^{\beta\mu}+\frac{1}{2}g^{\alpha\beta}g_{\lambda\mu}\partial_{\rho}\mathfrak{g}^{\lambda\nu}\partial_{\nu}\mathfrak{g}^{\mu\rho}-g^{\alpha\lambda}g_{\mu\nu}\partial_{\rho}\mathfrak{g}^{\beta\nu}\partial_{\lambda}\mathfrak{g}^{\mu\rho}-g^{\beta\lambda}g_{\mu\nu}\partial_{\rho}\mathfrak{g}^{\alpha\nu}\partial_{\lambda}\mathfrak{g}^{\mu\rho}
+gλμgνρν𝔤αλρ𝔤βμ+18(2gαλgβμgαβgλμ)(2gνρgστgρσgντ)λ𝔤ντμ𝔤ρσ}.\displaystyle+g_{\lambda\mu}g^{\nu\rho}\partial_{\nu}\mathfrak{g}^{\alpha\lambda}\partial_{\rho}\mathfrak{g}^{\beta\mu}+\frac{1}{8}\big{(}2g^{\alpha\lambda}g^{\beta\mu}-g^{\alpha\beta}g^{\lambda\mu}\big{)}\big{(}2g_{\nu\rho}g_{\sigma\tau}-g_{\rho\sigma}g_{\nu\tau}\big{)}\partial_{\lambda}\mathfrak{g}^{\nu\tau}\partial_{\mu}\mathfrak{g}^{\rho\sigma}\bigg{\}}. (86)

By defining the gravitational potential hαβ=ηαβ𝔤αβh^{\alpha\beta}=\eta^{\alpha\beta}-\mathfrak{g}^{\alpha\beta} and imposing the harmonic gauge condition βhαβ=0\partial_{\beta}h^{\alpha\beta}=0, one can simplify the above definition as

(g)tLLαβ=c416πG{12ηαβηλμρhλννhμρηαλημνρhβν\displaystyle(-g)t_{\text{LL}}^{\alpha\beta}=\frac{c^{4}}{16\pi G}\bigg{\{}\frac{1}{2}\eta^{\alpha\beta}\eta_{\lambda\mu}\partial_{\rho}h^{\lambda\nu}\partial_{\nu}h^{\mu\rho}-\eta^{\alpha\lambda}\eta_{\mu\nu}\partial_{\rho}h^{\beta\nu}
×λhμρηβλημνρhανλhμρ+ηλμηνρνhαλρhβμ\displaystyle\times\partial_{\lambda}h^{\mu\rho}-\eta^{\beta\lambda}\eta_{\mu\nu}\partial_{\rho}h^{\alpha\nu}\partial_{\lambda}h^{\mu\rho}+\eta_{\lambda\mu}\eta^{\nu\rho}\partial_{\nu}h^{\alpha\lambda}\partial_{\rho}h^{\beta\mu}
+18(2ηαληβμηαβηλμ)(2ηνρηστηρσηντ)λhντμhρσ}.\displaystyle+\frac{1}{8}\big{(}2\eta^{\alpha\lambda}\eta^{\beta\mu}-\eta^{\alpha\beta}\eta^{\lambda\mu}\big{)}\big{(}2\eta_{\nu\rho}\eta_{\sigma\tau}-\eta_{\rho\sigma}\eta_{\nu\tau}\big{)}\partial_{\lambda}h^{\nu\tau}\partial_{\mu}h^{\rho\sigma}\bigg{\}}. (87)

The second set of the important relations we need during our calculation is the PM expansion of the metric and its determinant in terms of the gravitational potentials. In Poisson and Will (2014), by utilizing the Landau-Lifshitz formalism and introducing the modern approach to the PM theory, it is shown that these PM expansions are given by the following general forms:

gαβ=ηαβ+hαβ12hηαβ+hαμhβμ12hhαβ\displaystyle g_{\alpha\beta}=\eta_{\alpha\beta}+h_{\alpha\beta}-\frac{1}{2}h\eta_{\alpha\beta}+h_{\alpha\mu}h^{\mu}_{\beta}-\frac{1}{2}hh_{\alpha\beta}
+(18h214hμνhμν)ηαβ+O(G3),\displaystyle~{}~{}~{}~{}~{}~{}+\big{(}\frac{1}{8}h^{2}-\frac{1}{4}h^{\mu\nu}h_{\mu\nu}\big{)}\eta_{\alpha\beta}+O(G^{3}), (88)
(g)=1h+12h212hμνhμν+O(G3),\displaystyle(-g)=1-h+\frac{1}{2}h^{2}-\frac{1}{2}h^{\mu\nu}h_{\mu\nu}+O(G^{3}), (89)

in which h=ηαβhαβ=h00+hkkh=\eta_{\alpha\beta}h^{\alpha\beta}=-h^{00}+h^{kk}. It should be noted that to derive these relations, according to the PM expansion of hαβh_{\alpha\beta}, it is considered that the gravitational potentials are at least of the order O(G)O(G). We use this general relation to find the near-zone metric in Sec. IV.1.

The third set of the essential relations is the solutions of the wave equation (13). All general forms of these solutions with respect to the position of the field and source points are completely derived and classified in Poisson and Will (2014). Here, we rewrite the solutions that we use in our calculation. The general solution of the wave equation when the source and field points both are situated within the near zone is given by

h𝒩αβ(t,𝒙)=\displaystyle h_{\mathcal{N}}^{\alpha\beta}{(t,\bm{x})}= 4Gc4l=0(1)ll!cl\displaystyle\frac{4G}{c^{4}}\sum_{l=0}^{\infty}\frac{(-1)^{l}}{l!c^{l}}
×(t)lτeffαβ(t,𝒙)|𝒙𝒙|l1d3x\displaystyle\times\Big{(}\frac{\partial}{\partial t}\Big{)}^{l}\int_{\mathcal{M}}\tau^{\alpha\beta}_{\text{eff}}{(t,\bm{x}^{\prime})}\rvert{\bm{x}-\bm{x}^{\prime}}\rvert^{l-1}d^{3}x^{\prime} (90)

Here, \mathcal{M} represents the three-dimension region which in fact separates the near zone from the wave zone. The length scale and surface of this boundary are displayed by \mathcal{R} and \partial\mathcal{M}, respectively. We should recall that in the primary stage of the iterated method, we are not allowed to impose the harmonic gauge conditions, αhαβ=0\partial_{\alpha}h^{\alpha\beta}=0, or equivalently the conservation equations, ατeffαβ=0\partial_{\alpha}\tau^{\alpha\beta}_{\text{eff}}=0. In fact, we postpone this condition until the last step of the iterative procedure, cf. Poisson and Will (2014). So, in our calculation, if we are in the primary stage of the iterated method, we use Eq. (90) to find the near-zone portion of the potential in the near zone; and if we are in the very last iterated step, we can freely use ατeffαβ=0\partial_{\alpha}\tau^{\alpha\beta}_{\text{eff}}=0 to simplify this integral and find the potential.

The next solution we need to complete our derivation is the near-zone solution of the wave equation where the field point is in the wave zone and the source point is situated in the near zone. In this case, unlike the previous near-zone solution, the field point is located in the wave zone. The general form of this solution is given by

h𝒩αβ(t,𝒙)=\displaystyle h_{\mathcal{N}}^{\alpha\beta}(t,\bm{x})= 4Gc4l=0(1)ll!\displaystyle\frac{4G}{c^{4}}\sum_{l=0}^{\infty}\frac{(-1)^{l}}{l!} (91)
×j1j2jl[1rτeffαβ(τ,𝒙)xj1j2jld3x].\displaystyle\times\partial_{j_{1}j_{2}\cdots j_{l}}\bigg{[}\frac{1}{r}\int_{\mathcal{M}}\tau^{\alpha\beta}_{\text{eff}}(\tau,\bm{x}^{\prime})x^{\prime j_{1}j_{2}\cdots j_{l}}d^{3}x^{\prime}\bigg{]}.

Here xj1j2jlx^{j_{1}j_{2}\cdots j_{l}} stands for xj1xj2xjlx^{j_{1}}x^{j_{2}}\cdots x^{j_{l}} and j1j2jl\partial_{j_{1}j_{2}\cdots j_{l}} shows j1j2jl\partial_{j_{1}}\partial_{j_{2}}\cdots\partial_{j_{l}}. We recall that τ=tr/c\tau=t-r/c is the retarded time and the integrand in this integral unlike the previous solution is a function of τ\tau.

Another solution that we will encounter during our calculation, is the wave-zone solution where the field and source points both are situated in the wave zone. In this case, considering the source of the wave-zone portion of the gravitational potential as

τEMSαβ=14πfαβ(τ)rnn<j1j2jl>,\displaystyle\tau^{\alpha\beta}_{\text{\tiny EMS}}=\frac{1}{4\pi}\frac{f^{\alpha\beta}(\tau)}{r^{n}}n^{<j_{1}j_{2}\cdots j_{l}>}, (92)

the wave-zone portion of the gravitational potential is given in the following form

h𝒲αβ(t,𝒙)\displaystyle h^{\alpha\beta}_{\mathcal{W}}(t,\bm{x}) =4Gc4n<j1j2jl>r{0fαβ(τ2s/c)A(s,r)ds\displaystyle=\frac{4G}{c^{4}}\frac{n^{<j_{1}j_{2}\cdots j_{l}>}}{r}\bigg{\{}\int_{0}^{\mathcal{R}}f^{\alpha\beta}(\tau-2s/c)A(s,r)ds
+fαβ(τ2s/c)B(s,r)ds},\displaystyle+\int_{\mathcal{R}}^{\infty}f^{\alpha\beta}(\tau-2s/c)B(s,r)ds\bigg{\}}, (93)

in which A(s,r)=r+sPl(ζ)p1n𝑑pA(s,r)=\int_{\mathcal{R}}^{r+s}P_{l}(\zeta)p^{1-n}dp and B(s,r)=sr+sPl(ζ)p1n𝑑pB(s,r)=\int_{s}^{r+s}P_{l}(\zeta)p^{1-n}dp. Here, Pl(ζ)P_{l}(\zeta) is a Legendre polynomial, ζ=(r+2s)/r2s(r+s)/(rp)\zeta=(r+2s)/r-2s(r+s)/(rp), and n<j1j2jl>n^{<j_{1}j_{2}\cdots j_{l}>} is an angular symmetric trace-free tensor introduced in Eq. (1.154) of Poisson and Will (2014).

Appendix C On the time derivative of 𝔐\mathfrak{M}

During our calculations in Sec. IV, we have encountered the new EMSG parameter 𝔐\mathfrak{M} introduced by Eq. (39). We have then shown that the time derivative of this parameter is entered in several PN corrections. Here, we try to simplify d𝔐/dtd\mathfrak{M}/dt. Given Eq. (39), we have

d𝔐dt=tρ2(t,𝒙)d3x.\displaystyle\frac{d\mathfrak{M}}{dt}=\int_{\mathcal{M}}\frac{\partial}{\partial t}{\rho^{*}}^{2}(t,\bm{x})d^{3}x. (94)

Utilizing the conservation of the rest-mass density (9), we find that

d𝔐dt=2ρj(ρvj)d3x.\displaystyle\frac{d\mathfrak{M}}{dt}=-2\int_{\mathcal{M}}\rho^{*}\partial_{j}\big{(}\rho^{*}v^{j}\big{)}d^{3}x. (95)

One can simply show that this relation can be written as

d𝔐dt=2ρ2vj𝑑Sj+2jρ(ρvj)d3x,\displaystyle\frac{d\mathfrak{M}}{dt}=-2\oint_{\partial\mathcal{M}}{\rho^{*}}^{2}v^{j}dS_{j}+2\int_{\mathcal{M}}\partial_{j}\rho^{*}\big{(}\rho^{*}v^{j}\big{)}d^{3}x, (96)

after applying the Gauss divergence theorem. Noting that the matter part vanishes on the boundary of \mathcal{M}, the first surface integral is zero. So, this term is reduced to

d𝔐dt=2ρvjjρd3x\displaystyle\frac{d\mathfrak{M}}{dt}=2\int_{\mathcal{M}}\rho^{*}v^{j}\partial_{j}\rho^{*}d^{3}x (97)

As seen, d𝔐/dtd\mathfrak{M}/dt is finally proportional to the integration of ρvjjρ\rho^{*}v^{j}\partial_{j}\rho^{*} and does not necessarily vanish.

Appendix D N-body description of the gravitational potentials

As we have seen in Sec. IV.3, it is important to know the order of the magnitude of the Newtonian and EMSG potentials UU and UEMSU_{\text{\tiny EMS}} on the boundary between the near and wave zones. We have called it \partial\mathcal{M}. For this purpose, in this Appendix, we benefit from the N-body description of the fluid system to derive an appropriate relation which can approximately define these gravitational potentials on the surface \partial\mathcal{M}.

To do so, we consider that the fluid is constructed from NN well-separated bodies. In this description, we can rewrite the gravitational potential as

U(t,𝒙)=A=1NGAρ(t,𝒙)|𝒙𝒙|d3x,\displaystyle U(t,\bm{x})=\sum_{A=1}^{N}G\int_{A}\frac{\rho^{*}(t,\bm{x}^{\prime})}{|\bm{x}-\bm{x}^{\prime}|}d^{3}x^{\prime}, (98)

where the index “AA” stands for the body AA and A=1,2,,NA=1,2,...,N. We assume that the body AA occupies the volume VAV_{A} in space with length scale RAR_{A}. To simplify this integral, we change the variable as 𝒙=𝒙¯+𝒓A\bm{x}^{\prime}=\bm{\bar{x}}^{\prime}+\bm{r}_{A}. Here, 𝒓A(t)\bm{r}_{A}(t) is the position of the center of mass of the body AA and the vector 𝒙¯\bm{\bar{x}} is the distance between a fluid element and 𝒓A(t)\bm{r}_{A}(t). So, we have

U(t,𝒙)=A=1NGAρ(t,𝒓A+𝒙¯)|𝒔A𝒙¯|d3x,\displaystyle U(t,\bm{x})=\sum_{A=1}^{N}G\int_{A}\frac{\rho^{*}(t,\bm{r}_{A}+\bm{\bar{x}}^{\prime})}{|\bm{s}_{A}-\bm{\bar{x}}^{\prime}|}d^{3}x^{\prime}, (99)

in which sA=|𝒙𝒓A|s_{A}=|\bm{x}-\bm{r}_{A}| is the position of the field point relative to the center of mass of the body AA. Now, we assume that this distance is much larger than the dimension of the body AA, i.e., we have RAsAR_{A}\ll s_{A}. Using this condition, we can expand |𝒔A𝒙¯|1|\bm{s}_{A}-\bm{\bar{x}}^{\prime}|^{-1} in powers of 𝒙¯\bm{\bar{x}}^{\prime}. Regarding this fact, one can simplify Eq. (99) to

U=A=1N(GmAsA+12IAjkjk1sA+),\displaystyle U=\sum_{A=1}^{N}\Big{(}\frac{Gm_{A}}{s_{A}}+\frac{1}{2}I_{A}^{jk}\partial_{jk}\frac{1}{s_{A}}+\cdots\Big{)}, (100)

where

mA=Aρd3x¯,\displaystyle m_{A}=\int_{A}{\rho^{*}}^{\prime}d^{3}\bar{x}^{\prime}, (101a)
IAjk=Aρx¯jx¯kd3x¯,\displaystyle I_{A}^{jk}=\int_{A}{\rho^{*}}^{\prime}\bar{x}^{\prime j}\bar{x}^{\prime k}d^{3}\bar{x}^{\prime}, (101b)

are the material mass and quadrupole moment of the body AA, respectively. This derivation is comprehensively introduced in chapter 9 of Poisson and Will (2014). Now, we assume that each compact body is located in the near zone, i.e., rAr_{A}\ll\mathcal{R}. Bearing this assumption in mind, one can deduce that Eq. (100) reduces to

U=AGmAr+O(r3),\displaystyle U=\sum_{A}\frac{Gm_{A}}{r}+O(r^{-3}), (102)

when we want to study the gravitational potential in the wave zone, i.e., |𝒙||\bm{x}|\geq\mathcal{R}. Here, we set sA|𝒙|=rs_{A}\simeq|\bm{x}|=r. In Sec. IV.3, we use this potential as a source of the surface integrals. We then set r=r=\mathcal{R} in that derivation.

In order to obtain the EMSG potential, the other source term of the surface integrals, we apply the same strategy introduced above. In the N-body description, for Eq. (34b), we have

UEMS(t,𝒙)=AGAρ2(t,𝒙)|𝒙𝒙|d3x.\displaystyle U_{\text{\tiny EMS}}(t,\bm{x})=\sum_{A}G\int_{A}\frac{{\rho^{*}}^{2}(t,\bm{x}^{\prime})}{|\bm{x}-\bm{x}^{\prime}|}d^{3}x^{\prime}. (103)

Changing the integration variable like before and using the Taylor expansion of |𝒔A𝒙¯|1|\bm{s}_{A}-\bm{\bar{x}}^{\prime}|^{-1}, we arrive at

UEMS=A(G𝔐AsA+12Ajkjk1sA+),\displaystyle U_{\text{\tiny EMS}}=\sum_{A}\Big{(}\frac{G\mathfrak{M}_{A}}{s_{A}}+\frac{1}{2}\mathfrak{I}_{A}^{jk}\partial_{jk}\frac{1}{s_{A}}+\cdots\Big{)}, (104)

where

𝔐A=Aρ2d3x¯,\displaystyle\mathfrak{M}_{A}=\int_{A}{\rho^{*}}^{\prime 2}d^{3}\bar{x}^{\prime}, (105a)
Ajk=Aρ2x¯jx¯kd3x¯.\displaystyle\mathfrak{I}_{A}^{jk}=\int_{A}{\rho^{*}}^{\prime 2}\bar{x}^{\prime j}\bar{x}^{\prime k}d^{3}\bar{x}^{\prime}. (105b)

It should be mentioned that to simplify this relation, we consider the following symmetry for the matter density ρ(t,𝒓A𝒙¯)=ρ(t,𝒓A+𝒙¯)\rho^{*}(t,\bm{r}_{A}-\bm{\bar{x}})=\rho^{*}(t,\bm{r}_{A}+\bm{\bar{x}}) and deduce that the integral Aρ2x¯jd3x¯\int_{A}{\rho^{*}}^{\prime 2}\bar{x}^{\prime j}d^{3}\bar{x}^{\prime} vanishes. The same scheme is also applied in the previous case. One can easily show that this relation is simplified to

UEMS=AG𝔐Ar+O(r3),\displaystyle U_{\text{\tiny EMS}}=\sum_{A}\frac{G\mathfrak{M}_{A}}{r}+O(r^{-3}), (106)

when |𝒙||𝒓A||\bm{x}|\gg|\bm{r}_{A}|.