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Neutron star mass formula with nuclear saturation parameters

Hajime Sotani [email protected] Astrophysical Big Bang Laboratory, RIKEN, Saitama 351-0198, Japan Interdisciplinary Theoretical & Mathematical Science Program (iTHEMS), RIKEN, Saitama 351-0198, Japan    Hajime Togashi Department of Physics, Tohoku University, Sendai 980-8578, Japan
Abstract

We derive the empirical formulas for the neutron star mass and gravitational redshift as a function of the central density and specific combination of the nuclear saturation parameters, which are applicable to the stellar models constructed with the central density up to threefold nuclear saturation density. Combining the both empirical formulas, one also estimates the neutron star radius. In practice, we find that the neutron star mass (radius) can be estimated within 10%\sim 10\% (a few percent) accuracy by comparing the mass and radius evaluated with our empirical formulas to those determined with the specific equation of state. Since our empirical formulas directly connect the neutron star mass and radius to the nuclear saturation parameters, one can discuss the neutron star properties with the specific values of nuclear saturation parameters constrained via nuclear experiments.

pacs:
04.40.Dg, 26.60.+c, 21.65.Ef

I Introduction

A neutron star is produced as a compact remnant through a supernova explosion, which occurs at the last moment of a massive star’s life. The neutron stars are in extreme states, which is hard to be realized in terrestrial laboratories. In particular, due to the nature of the nuclear saturation properties, it is quite difficult to obtain the nuclear information in a higher density region through the terrestrial experiments. This is a reason why the equation of state (EOS) for neutron star matter has not been fixed yet. Namely, the structure of the neutron star and its maximum mass are not exactly determined. Thus, the observations of the neutron stars and/or the phenomena associated with the neutron stars are quite important for understanding the physics in such extreme states.

For example, the discovery of the 2M2M_{\odot} neutron stars D10 ; A13 ; C20 ; F21 has ruled out some of the soft EOSs as the EOS for neutron star matter. That is, the EOS, with which the maximum mass does not reach the observed mass, can be ruled out. In addition, the light bending induced by the strong gravitational field, which is one of the important relativistic effects, modifys the pulsar light curve, which principally tells us the stellar compactness, i.e., the ratio of the stellar mass to its radius (e.g., PFC83 ; LL95 ; PG03 ; PO14 ; SM18 ; Sotani20a ). In practice, through the observations with the Neutron star Interior Composition Explorer (NICER) operating on an International Space Station, the mass and radius of PSR J0030+0451 Riley19 ; Miller19 and PSR J0740+6620 Riley21 ; Miller21 are constrained. Owing to the gravitational wave observations in the event of GW170817 gw170817 , the tidal deformability of the neutron star just before the merger of the binary neutron stars is also constrained, which tells us that the 1.4M1.4M_{\odot} neutron star radius should be less than 13.613.6 km Annala18 . Furthermore, it is proposed that the neutron star mass and radius may be determined with the technique of asteroseismology thorough the future gravitational wave observations (e.g., AK1996 ; AK1998 ; STM2001 ; SH2003 ; SYMT2011 ; PA2012 ; DGKK2013 ; Sotani2020 ; SD2021 ). These astronomical constraints on the neutron star mass and radius indirectly constrain the EOS for neutron star matter especially for a higher density region.

On the other hand, terrestrial experiments are obviously important for extracting the nuclear information, which also constrains the EOS for neutron star matter, even though the resultant constraint may be mainly around the nuclear saturation density. Up to now a lot of experiments worldwide have been done to fix the nuclear saturation parameters. Owing to these attempts, some of the saturation parameters have been constrained well, but many parameters, especially for higher order terms, still remain uncertain (see Sec. II for more detail). For instance, even the constraint on the density-dependence of the nuclear symmetry energy, which is recently reported from two large facilities in Japan and the USA, still has large uncertainties SPIRIT ; PREXII . Additionally, since the EOS for neutron star matter can be characterized by the nuclear saturation parameters, the neutron star properties may be also associated with the saturation parameters. Thus, to improve our understanding of the nuclear properties, the constraint on the neutron star mass and radius from the astronomical observations are quite important as well as constraints on the nuclear properties from the terrestrial experiments.

Nevertheless, even if one would accurately observe the neutron star mass and/or radius, it is difficult to directly discuss the nuclear saturation parameters. This is because the neutron star properties are associated with the EOSs, which can be characterized by the nuclear saturation parameters, but direct connection between the neutron star properties and nuclear saturation parameters is still unclear. To partially solve this difficulty, we have already found a suitable combination of the nuclear saturation parameters, with which the low-mass neutron star models can be expressed well SIOO14 . In this study, we extend the previous work and try to derive the empirical formulas for the mass and gravitational redshift of neutron star models constructed with the central density up to threefold nuclear saturation density, which helps us to directly discuss the association between the neutron star properties and nuclear saturation parameters.

This manuscript is organized as follows. In Sec. II, we briefly mention the EOSs considered in this study. In Sec. III, we systematically examine the neutron star models and derive the empirical formulas for the neutron star mass and its gravitational redshift as a function of the nuclear saturation parameters. Finally, in Sec. IV, we conclude this study. Unless otherwise mentioned, we adopt geometric units in the following, c=G=1c=G=1, where cc and GG denote the speed of light and the gravitational constant, respectively.

Table 1: EOS parameters adopted in this study, K0K_{0}, n0n_{0}, LL, QQ, KsymK_{sym}, and QsymQ_{sym} are listed, while η\eta, ξ\xi, ηsy\eta_{sy}, and ξsy\xi_{sy} are specific combinations with them given by η=(K0L2)1/3\eta=\left(K_{0}L^{2}\right)^{1/3}, ξ=|Q6Ksym/Qsym|1/6\xi=\left|{Q^{6}K_{sym}}/{Q_{sym}}\right|^{1/6}, ηsy=[(K0+Ksym)L2]1/3\eta_{sy}=\left[(K_{0}+K_{sym})L^{2}\right]^{1/3}, and ξsy=|Q11Ksym/Qsym|1/11\xi_{sy}=\left|{Q^{11}K_{sym}}/{Q_{sym}}\right|^{1/11}. In addition, we also list the TOV mass of the neutron stars constructed with the EOSs listed here with the central density nc=3n0n_{c}=3n_{0}.
EOS K0K_{0} n0n_{0} LL QQ KsymK_{sym} QsymQ_{sym} η\eta ξ\xi ηsy\eta_{sy} ξsy\xi_{sy} Mnc/n0=3M_{n_{c}/n_{0}=3}
(MeV) (fm-3) (MeV) (MeV) (MeV) (MeV) (MeV) (MeV) (MeV) (MeV) (MM_{\odot})
OI-EOSs 200 0.165 35.6 -759 -142 801 63.3 569 41.8 649 0.68
0.165 67.8 -761 -27.6 589 97.2 457 92.5 576 1.17
220 0.161 40.2 -720 -144 731 70.9 549 49.7 621 0.81
0.161 77.6 -722 -9.83 486 110 377 108 506 1.32
240 0.159 45.0 -663 -146 642 78.6 518 57.6 579 0.95
0.158 88.2 -664 10.5 363 123 368 125 482 1.47
260 0.156 49.8 -589 -146 535 86.4 474 65.6 523 1.09
0.155 99.2 -590 32.6 219 137 429 142 496 1.61
280 0.154 54.9 -496 -146 410 94.5 418 73.8 452 1.23
0.153 111 -498 57.4 54.4 151 502 161 500 1.76
300 0.152 60.0 -386 -146 266 103 349 82.2 366 1.38
0.151 124 -387 86.1 -133 167 360 181 372 1.90
KDE0v 229 0.161 45.2 -373 -145 523 77.6 301 55.6 332 1.11
KDE0v1 228 0.165 54.7 -385 -127 484 88.0 308 67.0 341 1.19
SLy2 230 0.161 47.5 -364 -115 507 80.3 285 63.7 318 1.26
SLy4 230 0.160 45.9 -363 -120 522 78.7 284 61.6 318 1.22
SLy9 230 0.151 54.9 -350 -81.4 462 88.4 262 76.4 299 1.41
SKa 263 0.155 74.6 -300 -78.5 175 114 263 101 279 1.57
SkI3 258 0.158 101 -304 73.0 212 138 254 150 276 1.77
SkMp 231 0.157 70.3 -338 -49.8 159 105 278 96.4 304 1.45
Shen 281 0.145 111 33.5 151 157 1.82
Togashi 245 0.160 38.7 71.6 1.27

II EOS for neutron star matter

To construct the neutron star models by solving the Tolman-Oppenheimer-Volkoff (TOV) equation, one has to assume an EOS for neutron star matter. In this study, we mainly adopt the phenomenological nuclear EOS models, focusing only on the unified EOS, i.e., the neutron star crust EOS is constructed with the same nuclear model as in the neutron star core EOS. As a phenomenological macroscopic model, we adopt the EOSs proposed by Oyamatsu and Iida (hereafter referred to as the OI-EOS) OI03 ; OI07 . The OI-EOSs are constructed with the Padé-type potential energies in such a way as to reproduce empirical masses and radii of stable nuclei, using a simplified version of the extended Thomas-Fermi theory. On the other hand, as a phenomenological Skyrme-type model, we adopt KDE0v, KDE0v1 KDE0v , SLy2, SLy4, SLy9 SLy4 ; SLy9 , SKa SKa , SkI3 SkI3 , and SkMp SkMp . In addition, we also adopt the Shen EOS Shen , which is based on the relativistic mean field theory, and the Togashi EOS Togashi17 , which is derived by the variational many-body calculation with AV18 two-body and UIX three-body potentials. In Fig. 1, we show the mass and radius relation for the neutron star models constructed with the EOSs adopted in this study, where the stellar models with nc/n0=1n_{c}/n_{0}=1, 2, and 3 are shown with the marks. We note that some of the stellar models with nc/n0=1n_{c}/n_{0}=1 are out of the panel due to the large radius. One can observe that some of EOSs are obviously ruled out from the 2M2M_{\odot} observations D10 ; A13 ; C20 ; F21 or the radius constraint from the GW170817 Annala18 , but in order to examine with the wide parameter space, we adopt even such EOSs in this study.

Refer to caption
Figure 1: Mass and radius relation for the neutron star models constructed with the EOSs listed in Table 1, where the top and bottom panels correspond to the result with OI-EOSs and the others, respectively. The OI-EOSs are named with the value of K0K_{0}, e.g., OI200 for the OI-EOSs with K0=200K_{0}=200 MeV. In the top panel, the solid and dashed lines respectively denote the OI-EOSs with larger and smaller values of LL for each value of K0K_{0} (see Table 1). In each panel, the neutron star models with nc/n0=1n_{c}/n_{0}=1, 2, and 3 are shown with the marks.

In any case, the bulk energy per nucleon for the uniform nuclear matter at zero temperature can generally be expressed as a function of the baryon number density, nb=nn+npn_{\rm b}=n_{n}+n_{p}, and an asymmetry parameter, α=(nnnp)/nb\alpha=(n_{n}-n_{p})/n_{\rm b}, with the neutron number density, nnn_{n}, and the proton number density, npn_{p};

EA=ws(nb)+α2S(nb)+𝒪(α3),\frac{E}{A}=w_{s}(n_{\rm b})+\alpha^{2}S(n_{\rm b})+{\cal O}(\alpha^{3}), (1)

where wsw_{s} corresponds to the energy per nucleon of symmetric nuclear matter, while SS denotes the density-dependent symmetry energy. Additionally, wsw_{s} and SS can be expanded around the saturation density, n0n_{0}, of the symmetric nuclear matter as a function of u=(nbn0)/(3n0)u=(n_{\rm b}-n_{0})/(3n_{0});

ws(nb)=w0+K02u2+Q6u3+𝒪(u4),\displaystyle w_{s}(n_{\rm b})=w_{0}+\frac{K_{0}}{2}u^{2}+\frac{Q}{6}u^{3}+{\cal O}(u^{4}), (2)
S(nb)=S0+Lu+Ksym2u2+Qsym6u3+𝒪(u4).\displaystyle S(n_{\rm b})=S_{0}+Lu+\frac{K_{sym}}{2}u^{2}+\frac{Q_{sym}}{6}u^{3}+{\cal O}(u^{4}). (3)

The coefficients in these expressions are the nuclear saturation parameters, with which each EOS is characterized. The parameters for the adopted EOSs are concretely listed in Table 1, where η\eta, ξ\xi, ηsy\eta_{sy}, and ξsy\xi_{sy} are the specific combination of the nuclear saturation parameters (see the following sections for details), defined by

η=(K0L2)1/3,\displaystyle\eta=\left(K_{0}L^{2}\right)^{1/3}, (4)
ξ=|Q6KsymQsym|1/6,\displaystyle\xi=\left|\frac{Q^{6}K_{sym}}{Q_{sym}}\right|^{1/6}, (5)
ηsy=[(K0+Ksym)L2]1/3,\displaystyle\eta_{sy}=\left[(K_{0}+K_{sym})L^{2}\right]^{1/3}, (6)
ξsy=|Q11KsymQsym|1/11.\displaystyle\xi_{sy}=\left|\frac{Q^{11}K_{sym}}{Q_{sym}}\right|^{1/11}. (7)

Among the nuclear saturation parameters, n0n_{0}, w0w_{0}, and S0S_{0} are well constrained as n00.150.16n_{0}\approx 0.15-0.16 fm-3, w015.8w_{0}\approx-15.8 MeV OHKT17 , and S031.6±2.7S_{0}\approx 31.6\pm 2.7 MeV Li19 . Meanwhile, K0K_{0} and LL are more difficult to be determined from the terrestrial experiments, because these parameters are the density derivative at the saturation point, i.e., one needs to know the information not only at the saturation point but also in wider range around the saturation point. The constraints on these parameters are gradually improved and the current fiducial values are K0=230±40K_{0}=230\pm 40 MeV KM13 and L=58.9±16L=58.9\pm 16 MeV Li19 , even though the constraints on LL recently reported from two large facilities still have a large uncertainty, i.e., 42L11742\leq L\leq 117 MeV with Sπ\piRIT by the Radioactive Isotope Beam Factory at RIKEN in Japan SPIRIT and L=106±37L=106\pm 37 MeV with PREX-II by the Thomas Jefferson National Accelerator Facility in Newport News, the United States PREXII . Moreover, the saturation parameters in higher order terms, such as QQ, KsymK_{sym}, QsymQ_{sym}, are almost unconstrained from the experiments, but they are theoretically predicted as 800Q400-800\leq Q\leq 400 MeV, 400Ksym100-400\leq K_{sym}\leq 100 MeV, and 200Qsym800-200\leq Q_{sym}\leq 800 MeV Li19 .

It is known that S0S_{0} is strongly associated with LL as S028+0.075LS_{0}\approx 28+0.075L OI03 ; LL13 . In a similar way, we find that K0+KsymK_{0}+K_{sym} is also strongly associated with LL, adopting 118 models for the Skyrme-type EOSs listed in Ref. Danielewicz09 and 304 models for OI-EOSs. We plot K0+KsymK_{0}+K_{sym} as a function of LL in Fig. 2, where the thick solid line denotes the fitting formula given by

K0+Ksym=75.86+371.8(L100MeV).K_{0}+K_{sym}=-75.86+371.8\left(\frac{L}{100\ {\rm MeV}}\right). (8)

The similar correlation has been reported in Ref. Tews17 , which is shown in Fig. 2 with the dotted line. This type of correlation may be very useful for constraining the value of KsymK_{sym} with using the constraints on K0K_{0} and LL, because the uncertainty in KsymK_{sym} is still very large. In practice, by assigning the fiducial values of K0K_{0} and LL mentioned above in Eq. (8), one can find that 186Ksym13-186\leq K_{sym}\leq 13 MeV.

Refer to caption
Figure 2: The relation between K0+KsymK_{0}+K_{sym} and LL for the OI-EOSs and Skyrme-type EOSs. The solid line denotes the fitting given by Eq. (8), while the dotted line denote the fitting proposed in the previous study Tews17 .

III Neutron star mass formula

The neutron star structure is determined by solving the TOV equations together with the appropriate EOS. The neutron star may sometimes be considered as a huge nucleus, but its structure is quite dense, compared to atomic nuclei. Nevertheless, since the density inside low-mass neutron stars is definitely low, their mass seems to be strongly associated with the nuclear saturation properties. In practice, it has been found that the mass, MM, and gravitational redshift, z(12GM/Rc2)1/21z\equiv(1-2GM/Rc^{2})^{-1/2}-1, for the low-mass neutron stars, whose central density is less than twice the nuclear saturation density, are well expressed as a function of η\eta defined by Eq. (4) and uc=ρc/ρ0u_{c}=\rho_{c}/\rho_{0}, where ρc\rho_{c} and ρ0\rho_{0} are the central energy density and the energy density corresponding to the nuclear saturation density, i.e., ρ0=2.68×1014\rho_{0}=2.68\times 10^{14} g/cm3 SIOO14 . That is, one can estimate neutron star mass and radius by combining the empirical formulas, M=M(uc,η)M=M(u_{c},\eta) and z=z(uc,η)z=z(u_{c},\eta). In practice, assuming the recent experimental constraints obtained with Sπ\piRIT and PREX-II SPIRIT ; PREXII , one can show the allowed region in the neutron star mass and radius relation SNN22 . Using this new parameter η\eta, one can also discuss the rotational properties of the low-mass neutron stars SSB16 and the possible maximum mass of neutron stars Sotani17 ; SK17 . In this study, we try to extend this type of empirical formulas even for higher central density up to three times saturation density. This is because, as the central density becomes larger, the empirical formulas discussed in more detail below lose accuracy. This may come from the additional EOS dependence, such as higher order coefficients in Eqs. (2) and (3). In addition, for reference, we show the mass of neutron stars with nc=3n0n_{c}=3n_{0} constructed with the EOSs considered in this study in Table 1, with which one may be able to adopt our empirical relations discussed below if the stellar mass is less than 0.681.90M/M\simeq 0.68-1.90M/M_{\odot} (average value is 1.34M1.34M_{\odot}).

III.1 Function of η\eta

Since the saturation density, n0n_{0}, also depends on the EOS models, as shown in Table 1, it may be better to consider the mass and redshift for the low-mass neutron star as a function of nc/n0n_{c}/n_{0} instead of ρc/ρ0\rho_{c}/\rho_{0} with the fixed value of ρ0\rho_{0}, where ncn_{c} is the baryon number density at the stellar center. In fact, as shown in Fig. 3, one can observe that the neutron star mass, MM, and gravitational redshift, zz, with the fixed central baryon number density, e.g., nc/n0=1,2,3n_{c}/n_{0}=1,2,3, are strongly correlated with η\eta. We note that MM and zz are quite similar dependence on η\eta, even though each value is completely different, as shown in Ref. SIOO14 . With this result, we can derive the fitting formulas as

MηM=a0m+a1mln(η100)+a2mη100+a3mη1002,\displaystyle\frac{M_{\eta}}{M_{\odot}}=a_{0}^{m}+a_{1}^{m}\ln(\eta_{100})+a_{2}^{m}\eta_{100}+a_{3}^{m}\eta_{100}^{2}, (9)
zη=a0z+a1zln(η100)+a2zη100+a3zη1002,\displaystyle z_{\eta}=a_{0}^{z}+a_{1}^{z}\ln(\eta_{100})+a_{2}^{z}\eta_{100}+a_{3}^{z}\eta_{100}^{2}, (10)

where η100η/(100MeV)\eta_{100}\equiv\eta/(100\ {\rm MeV}), while aima_{i}^{m} and aiza_{i}^{z} for i=03i=0-3 are the coefficients in the fitting formulas, depending on the normalized central density, cnc/n0{\cal R}_{c}\equiv n_{c}/n_{0}. Here, in order to distinguish the mass and radius determined by integrating TOV equations with each EOS, the mass and redshift estimated with the fitting formulas given by Eqs. (9) and (10) are referred to as MηM_{\eta} and zηz_{\eta}. In addition, as shown in Fig. 4, we find that the coefficients aima_{i}^{m} and aiza_{i}^{z} are well expressed as a function of c{\cal R}_{c} as

aim(c)=ai0m+ai1mc+ai2mc3+ai3mc5,\displaystyle a_{i}^{m}({\cal R}_{c})=a_{i0}^{m}+a_{i1}^{m}{\cal R}_{c}+a_{i2}^{m}{\cal R}_{c}^{3}+a_{i3}^{m}{\cal R}_{c}^{5}, (11)
aiz(c)=ai0z+ai1zc+ai2zc3+ai3zc5,\displaystyle a_{i}^{z}({\cal R}_{c})=a_{i0}^{z}+a_{i1}^{z}{\cal R}_{c}+a_{i2}^{z}{\cal R}_{c}^{3}+a_{i3}^{z}{\cal R}_{c}^{5}, (12)

where the exact values of aijma_{ij}^{m} and aijza_{ij}^{z} for i=03i=0-3 and j=03j=0-3 are listed in Table 2. Now, we can get the empirical formulas for the neutron star mass and redshift as Mη=Mη(c,η)M_{\eta}=M_{\eta}({\cal R}_{c},\eta) and zη=zη(c,η)z_{\eta}=z_{\eta}({\cal R}_{c},\eta) given by Eqs. (9) – (12).

Table 2: Values of aijma_{ij}^{m} and aijza_{ij}^{z} in Eqs. (11) and (12).
jj 0 1 2 3
a0jma_{0j}^{m} 3.21103.2110 5.5024-5.5024 1.33751.3375 0.059490-0.059490
a1jma_{1j}^{m} 1.83401.8340 3.2893-3.2893 0.872060.87206 0.039859-0.039859
a2jma_{2j}^{m} 4.3905-4.3905 7.45827.4582 1.6450-1.6450 0.0714060.071406
a3jma_{3j}^{m} 0.945440.94544 1.5004-1.5004 0.335220.33522 0.014110-0.014110
a0jza_{0j}^{z} 0.253850.25385 0.60188-0.60188 0.158080.15808 0.0053861-0.0053861
a1jza_{1j}^{z} 0.151410.15141 0.36133-0.36133 0.102750.10275 0.0035881-0.0035881
a2jza_{2j}^{z} 0.38040-0.38040 0.843060.84306 0.19442-0.19442 0.00642460.0064246
a3jza_{3j}^{z} 0.0866530.086653 0.18150-0.18150 0.0417460.041746 0.0013309-0.0013309
Refer to caption
Figure 3: The neutron star mass, MM, and gravitational redshift, zz, for various EOSs with the fixed central baryon number density, nc/n0=1,2,3n_{c}/n_{0}=1,2,3, are plotted as a function of η\eta. This thick-solid lines denote the fitting lines given by Eqs. (9) and (10).
Refer to caption
Figure 4: The nc/n0n_{c}/n_{0} dependence of the coefficients, aima_{i}^{m} and aiza_{i}^{z}, in the fitting formula of stellar mass and gravitational redshift as a function of η/(100MeV)\eta/(100\ {\rm MeV}) expressed by Eqs. (9) and (10). The open marks denote the values of aima_{i}^{m} and aiza_{i}^{z} in the fitting formulas, while the solid lines denote the fitting as a function of nc/n0n_{c}/n_{0} as Eqs. (11) and (12).

Next, in order to improve the resultant empirical formulas, we try to characterize the deviation of the neutron star mass and redshift determined with each EOS from those estimated with the fitting formulas given by Eqs. (9) – (12), using a specific combination of the nuclear saturation parameters in the higher order terms. That is, the deviation of the mass and redshift are given by

ΔMη=MTOVMη(c,η),\displaystyle\Delta M_{\eta}=M_{\rm TOV}-M_{\eta}({\cal R}_{c},\eta), (13)
Δzη=zTOVzη(c,η),\displaystyle\Delta z_{\eta}=z_{\rm TOV}-z_{\eta}({\cal R}_{c},\eta), (14)

where MTOVM_{\rm TOV} and zTOVz_{\rm TOV} are the neutron star mass and redshift determined by integrating the TOV equations together with each EOS. Through a trial and error process, we find a good combination of KsymK_{sym}, QQ, and QsymQ_{sym}, which is ξ\xi defined by Eq. (5), for characterizing ΔMη\Delta M_{\eta} and Δzη\Delta z_{\eta}, even though it may be not so tight correlation. We note that it may be necessary to modify the definition of ξ\xi, if ξ\xi is out of the range considered in this study, i.e., 250< ξ< 600250\,\,\raisebox{-3.44444pt}{$\stackrel{{\scriptstyle\textstyle<}}{{\sim}}$ }\xi\,\,\raisebox{-3.44444pt}{$\stackrel{{\scriptstyle\textstyle<}}{{\sim}}$ }600 MeV with the EOSs adopted in this study. In fact, ξ\xi is not defined when Qsym=0Q_{sym}=0. In practice, for the neutron star models with nc/n0=2n_{c}/n_{0}=2 and 3, we show ΔMη/M\Delta M_{\eta}/M_{\odot} and zηz_{\eta} as a function of ξ\xi in Fig. 5, considering the OI-EOSs and the Skyrme-type EOSs. In this figure, we also plot the fitting formulas given by

ΔMηM=b0m/ξ500+b1mξ500+b2mξ5002+b3mξ5003,\displaystyle\frac{\Delta M_{\eta}}{M_{\odot}}=b_{0}^{m}/\xi_{500}+b_{1}^{m}\xi_{500}+b_{2}^{m}\xi_{500}^{2}+b_{3}^{m}\xi_{500}^{3}, (15)
Δzη=b0z/ξ500+b1zξ500+b2zξ5002+b3zξ5003,\displaystyle\Delta z_{\eta}=b_{0}^{z}/\xi_{500}+b_{1}^{z}\xi_{500}+b_{2}^{z}\xi_{500}^{2}+b_{3}^{z}\xi_{500}^{3}, (16)

where ξ500ξ/(500MeV)\xi_{500}\equiv\xi/(500\ {\rm MeV}), while again bimb_{i}^{m} and bizb_{i}^{z} for i=03i=0-3 are the adjusting coefficients depending on c{\cal R}_{c}. In a similar way for deriving the fitting formulas for ΔMη\Delta M_{\eta} and Δzη\Delta z_{\eta}, the coefficients in Eqs. (15) and (16) are plotted in Fig. 6 as a function of nc/n0n_{c}/n_{0}, which can be fitted with

bim(c)=bi0m+bi1mc2+bi2mc4+bi3mc6,\displaystyle b_{i}^{m}({\cal R}_{c})=b_{i0}^{m}+b_{i1}^{m}{\cal R}_{c}^{2}+b_{i2}^{m}{\cal R}_{c}^{4}+b_{i3}^{m}{\cal R}_{c}^{6}, (17)
biz(c)=bi0z+bi1zc2+bi2zc4+bi3zc6,\displaystyle b_{i}^{z}({\cal R}_{c})=b_{i0}^{z}+b_{i1}^{z}{\cal R}_{c}^{2}+b_{i2}^{z}{\cal R}_{c}^{4}+b_{i3}^{z}{\cal R}_{c}^{6}, (18)

where the concrete values of the coefficients bijmb_{ij}^{m} and bijzb_{ij}^{z} for i=03i=0-3 and j=03j=0-3 are listed in Table 3. We note that we consider the fitting of ΔMη\Delta M_{\eta} and Δzη\Delta z_{\eta} only for nc/n0>1n_{c}/n_{0}>1 as in Fig. 6, even though in principle one can also fit them for lower density region. This is because the correlation of ΔMη\Delta M_{\eta} and Δzη\Delta z_{\eta} with ξ\xi becomes weaker and the absolute values of ΔMη\Delta M_{\eta} and Δzη\Delta z_{\eta} become much smaller, as the density becomes lower. So, for nc/n01n_{c}/n_{0}\leq 1 we simply assume that ΔMη=0\Delta M_{\eta}=0 and Δzη=0\Delta z_{\eta}=0 in this study.

Refer to caption
Figure 5: Considering the OI-EOSs and the Skyrme-type EOSs, ΔMη/M\Delta M_{\eta}/M_{\odot} and zηz_{\eta} calculated with Eqs. (13) and (14) are shown as a function of ξ\xi for nc/n0=2n_{c}/n_{0}=2 (open circles) and 3 (filled squares). The dotted and solid lines are fitting lines given by Eqs. (15) and (16).
Refer to caption
Figure 6: The coefficients in Eqs. (15) and (16) are shown as a function of nc/n0n_{c}/n_{0} with marks, while the solid lines denote the fitting given by Eqs. (17) and (18), respectively.
Table 3: Values of bijmb_{ij}^{m} and bijzb_{ij}^{z} in Eqs. (17) and (18).
jj 0 1 2 3
b0jmb_{0j}^{m} 7.711×102-7.711\times 10^{-2} 4.122×1024.122\times 10^{-2} 8.051×1048.051\times 10^{-4} 7.267×105-7.267\times 10^{-5}
b1jmb_{1j}^{m} 7.763×1017.763\times 10^{-1} 5.341×101-5.341\times 10^{-1} 5.793×1025.793\times 10^{-2} 2.995×103-2.995\times 10^{-3}
b2jmb_{2j}^{m} 1.470-1.470 1.1231.123 1.774×101-1.774\times 10^{-1} 9.771×1039.771\times 10^{-3}
b3jmb_{3j}^{m} 7.276×1017.276\times 10^{-1} 5.897×101-5.897\times 10^{-1} 1.077×1011.077\times 10^{-1} 6.041×103-6.041\times 10^{-3}
b0jzb_{0j}^{z} 2.783×103-2.783\times 10^{-3} 1.679×1031.679\times 10^{-3} 9.658×1049.658\times 10^{-4} 3.707×105-3.707\times 10^{-5}
b1jzb_{1j}^{z} 3.989×1023.989\times 10^{-2} 4.167×102-4.167\times 10^{-2} 1.204×1031.204\times 10^{-3} 1.209×104-1.209\times 10^{-4}
b2jzb_{2j}^{z} 9.514×102-9.514\times 10^{-2} 1.031×1011.031\times 10^{-1} 1.341×102-1.341\times 10^{-2} 7.713×1047.713\times 10^{-4}
b3jzb_{3j}^{z} 5.321×1025.321\times 10^{-2} 5.814×102-5.814\times 10^{-2} 9.859×1039.859\times 10^{-3} 5.368×104-5.368\times 10^{-4}

Now, we can derive new empirical formulas for the neutron star mass, MηξM_{\eta\xi}, and redshift, zηξz_{\eta\xi}, as a function of c(=nc/n0){\cal R}_{c}(=n_{c}/n_{0}), η\eta, and ξ\xi:

MηξM=Mη(c,η)M+ΔMη(c,ξ)M,\displaystyle\frac{M_{\eta\xi}}{M_{\odot}}=\frac{M_{\eta}({\cal R}_{c},\eta)}{M_{\odot}}+\frac{\Delta M_{\eta}({\cal R}_{c},\xi)}{M_{\odot}}, (19)
zηξ=zη(c,η)+Δzη(c,ξ),\displaystyle z_{\eta\xi}=z_{\eta}({\cal R}_{c},\eta)+\Delta z_{\eta}({\cal R}_{c},\xi), (20)

where the first terms are given by Eqs. (9) – (12) and the second terms are given by Eqs. (15) – (18). In order to check the accuracy of our empirical formulas, Mη(c,η)M_{\eta}({\cal R}_{c},\eta), zη(c,ηz_{\eta}({\cal R}_{c},\eta), Mηξ(c,η,ξ)M_{\eta\xi}({\cal R}_{c},\eta,\xi), and zηξ(c,η,ξ)z_{\eta\xi}({\cal R}_{c},\eta,\xi), in Fig. 7 we show the relative deviation from the neutron star mass and redshift determined through the TOV equations, where the bottom panels are the relative deviation of the neutron star radius estimated with the empirical formulas for the mass and redshift from the TOV solution. From this figure, one can see that the neutron star mass is estimated within 10%\sim 10\% accuracy, while the radius for the canonical neutron star is estimated within 3%\sim 3\% accuracy, using the empirical formulas, Mηξ(c,η,ξ)M_{\eta\xi}({\cal R}_{c},\eta,\xi) and zηξ(c,η,ξ)z_{\eta\xi}({\cal R}_{c},\eta,\xi). We also make a comment that the mass estimation with Mη(c,η)M_{\eta}({\cal R}_{c},\eta) (top left panel) is better than that with Mηξ(c,η,ξ)M_{\eta\xi}({\cal R}_{c},\eta,\xi) (top right panel) in the density region around nc/n01.5n_{c}/n_{0}\simeq 1.5, which comes from the fact that the correlation between ΔMη\Delta M_{\eta} and ξ\xi becomes worse as the density becomes lower. We note that the mass and gravitational redshift have quite similar dependence on η\eta, as shown in Fig. 3, i.e., it seems to get a small amount of difference in information from the mass and gravitational redshift. Even so, one can accurately recover the radius, using the empirical relations for the mass and gravitational redshift.

Refer to caption
Figure 7: Relative deviation of the neutron star mass (top panel) and redshift (middle panel) estimated with the empirical formulas from those constructed with each EOS are shown as a function of the normalized central baryon number density. The left panels are the deviation with the empirical formulas, Mη(c,η)M_{\eta}({\cal R}_{c},\eta) and zη(c,η)z_{\eta}({\cal R}_{c},\eta), while the right panels are that with Mηξ(c,η,ξ)M_{\eta\xi}({\cal R}_{c},\eta,\xi) and zηξ(c,η,ξ)z_{\eta\xi}({\cal R}_{c},\eta,\xi). The bottom panels are the relative deviation of the neutron star radius estimated with the empirical formulas for the mass and redshift from that calculated with each EOS.

At the end, we mention another possibility for characterizing ΔMη\Delta M_{\eta} and Δzη\Delta z_{\eta} instead of ξ\xi. In practice, we find that a new parameter, ξc\xi_{{\cal R}_{c}}, defined by

ξc=|Q2cKsymQsym|1/2c\xi_{{\cal R}_{c}}=\left|\frac{Q^{2{\cal R}_{c}}K_{sym}}{Q_{sym}}\right|^{1/2{\cal R}_{c}} (21)

seems to be better than ξ\xi given by Eq. (5) for characterizing ΔMη\Delta M_{\eta} and Δzη\Delta z_{\eta}. That is, adopting the same functional form as Eqs. (15) and (16), one can express ΔMη\Delta M_{\eta} and Δzη\Delta z_{\eta} with ξc\xi_{{\cal R}_{c}}, where the correlation in a lower density region is better than the case with ξ\xi. But, unfortunately, the dependence of the coefficients bimb_{i}^{m} and bizb_{i}^{z} on c{\cal R}_{c} becomes more complex. So, in this study, we simply adopt ξ\xi as mentioned above.

III.2 Function of ηsy\eta_{sy}

Up to now we consider to derive the empirical formulas with η\eta, but another combination of the nuclear saturation parameters may be better to express the neutron star mass and redshift. Here, we consider to derive the empirical formulas as a function of ηsy\eta_{sy} defined by Eq. (6) instead of η\eta. In Fig. 8 we plot the neutron star mass and redshift with nc/n0=1,2,3n_{c}/n_{0}=1,2,3 constructed with each EOS, together with the fitting lines given by

MηsyM=asy,0m+asy,1mln(ηsy,100)+asy,2mηsy,100+asy,3mηsy,1002,\displaystyle\frac{M_{\eta_{sy}}}{M_{\odot}}=a_{sy,0}^{m}+a_{sy,1}^{m}\ln(\eta_{sy,100})+a_{sy,2}^{m}\eta_{sy,100}+a_{sy,3}^{m}\eta_{sy,100}^{2}, (22)
zηsy=asy,0z+asy,1zln(ηsy,100)+asy,2zηsy,100+asy,3zηsy,1002,\displaystyle z_{\eta_{sy}}=a_{sy,0}^{z}+a_{sy,1}^{z}\ln(\eta_{sy,100})+a_{sy,2}^{z}\eta_{sy,100}+a_{sy,3}^{z}\eta_{sy,100}^{2}, (23)

where ηsy,100ηsy/(100MeV)\eta_{sy,100}\equiv\eta_{sy}/(100\ {\rm MeV}). Again, the coefficients, asy,ima_{sy,i}^{m} and asy,iza_{sy,i}^{z}, depend on c{\cal R}_{c}, which are shown in Fig. 9. In this figure, the marks denote numerical values determined by fitting with Eqs. (22) and (23) as in Fig. 8, while the solid lines denote the fitting of asy,ima_{sy,i}^{m} and asy,iza_{sy,i}^{z} as a function of c{\cal R}_{c} with

asy,im(c)=asy,i0m+asy,i1mc+asy,i2mc3+asy,i3mc5,\displaystyle a_{sy,i}^{m}({\cal R}_{c})=a_{sy,i0}^{m}+a_{sy,i1}^{m}{\cal R}_{c}+a_{sy,i2}^{m}{\cal R}_{c}^{3}+a_{sy,i3}^{m}{\cal R}_{c}^{5}, (24)
asy,iz(c)=asy,i0z+asy,i1zc+asy,i2zc3+asy,i3zc5,\displaystyle a_{sy,i}^{z}({\cal R}_{c})=a_{sy,i0}^{z}+a_{sy,i1}^{z}{\cal R}_{c}+a_{sy,i2}^{z}{\cal R}_{c}^{3}+a_{sy,i3}^{z}{\cal R}_{c}^{5}, (25)

where the concrete values of asy,ijma_{sy,ij}^{m} and asy,ijza_{sy,ij}^{z} for i=03i=0-3 and j=03j=0-3 are listed in Table 4. Comparing Fig. 8 to Fig. 3, η\eta seems to be better than ηsy\eta_{sy} in this stage, because a specific EOS model (e.g., OI 220) with nc/n0=3n_{c}/n_{0}=3 largely deviates from the fitting line in Fig. 8.

Refer to caption
Figure 8: Same as in Fig. 3, but as a function of ηsy\eta_{sy}. The thick-solid lines denote the fitting lines given by Eqs. (22) and (23).
Refer to caption
Figure 9: The coefficients in Eqs. (22) and (23) are plotted as a function of c=nc/n0{\cal R}_{c}=n_{c}/n_{0}, while the solid lines are the corresponding fitting given by Eqs. (24) and (25).
Table 4: Values of asy,ijma_{sy,ij}^{m} and asy,ijza_{sy,ij}^{z} in Eqs. (24) and (25).
jj 0 1 2 3
asy,0jma_{sy,0j}^{m} 0.69900.6990 1.2408-1.2408 0.56550.5655 0.02710-0.02710
asy,1jma_{sy,1j}^{m} 0.32200.3220 0.6504-0.6504 0.32660.3266 0.01596-0.01596
asy,2jma_{sy,2j}^{m} 1.2165-1.2165 2.14432.1443 0.6833-0.6833 0.031340.03134
asy,3jma_{sy,3j}^{m} 0.23140.2314 0.3555-0.3555 0.13740.1374 0.006172-0.006172
asy,0jza_{sy,0j}^{z} 0.052860.05286 0.1492-0.1492 0.073550.07355 0.002614-0.002614
asy,1jza_{sy,1j}^{z} 0.035030.03503 0.08519-0.08519 0.042520.04252 0.001517-0.001517
asy,2jza_{sy,2j}^{z} 0.1233-0.1233 0.27260.2726 0.08809-0.08809 0.0029650.002965
asy,3jza_{sy,3j}^{z} 0.026290.02629 0.05430-0.05430 0.019290.01929 0.0006297-0.0006297

Then, we consider to characterize the deviation of the neutron star mass and redshift estimated with the empirical formulas, Mηsy(c,ηsy)M_{\eta_{sy}}({\cal R}_{c},\eta_{sy}) and zηsy(c,ηsy)z_{\eta_{sy}}({\cal R}_{c},\eta_{sy}), given by Eqs. (22) – (25) from those determined as the TOV solution. Such a deviation is given by

ΔMηsy=MTOVMηsy(c,ηsy),\displaystyle\Delta M_{\eta_{sy}}=M_{\rm TOV}-M_{\eta_{sy}}({\cal R}_{c},\eta_{sy}), (26)
Δzηsy=zTOVzηsy(c,ηsy).\displaystyle\Delta z_{\eta_{sy}}=z_{\rm TOV}-z_{\eta_{sy}}({\cal R}_{c},\eta_{sy}). (27)

In the beginning we try to characterize ΔMηsy\Delta M_{\eta_{sy}} and Δzηsy\Delta z_{\eta_{sy}} with a specific combination of QQ and QsymQ_{sym}, because KsymK_{sym} is already included in the definition of ηsy\eta_{sy}, but eventually we find that the combination of KsymK_{sym}, QQ, and QsymQ_{sym} defined by Eq. (7) are suitable for this problem. In fact, as shown in Fig. 10, ΔMηsy\Delta M_{\eta_{sy}} and Δzηsy\Delta z_{\eta_{sy}} are well fitted as a function of ξsy\xi_{sy}, where the open-circles (filled-squares) denote the values of ΔMηsy\Delta M_{\eta_{sy}} and Δzηsy\Delta z_{\eta_{sy}} with nc/n0=2n_{c}/n_{0}=2 (nc/n0=3n_{c}/n_{0}=3), while the dotted (solid) lines denote the fitting of those values with nc/n0=2n_{c}/n_{0}=2 (nc/n0=3n_{c}/n_{0}=3) by

ΔMηsyM=bsy,0m/ξsy,5006+bsy,1mξsy,5007+bsy,2mξsy,5008+bsy,3mξsy,50012,\displaystyle\frac{\Delta M_{\eta_{sy}}}{M_{\odot}}=b_{sy,0}^{m}/\xi_{sy,500}^{6}+b_{sy,1}^{m}\xi_{sy,500}^{7}+b_{sy,2}^{m}\xi_{sy,500}^{8}+b_{sy,3}^{m}\xi_{sy,500}^{12}, (28)
Δzηsy=bsy,0z/ξsy,5006+bsy,1zξsy,5007+bsy,2zξsy,5008+bsy,3zξsy,50012.\displaystyle\Delta z_{\eta_{sy}}=b_{sy,0}^{z}/\xi_{sy,500}^{6}+b_{sy,1}^{z}\xi_{sy,500}^{7}+b_{sy,2}^{z}\xi_{sy,500}^{8}+b_{sy,3}^{z}\xi_{sy,500}^{12}. (29)

In these fitting formulas, ξsy,500\xi_{sy,500} is defined as ξsy,500ξsy/(500MeV)\xi_{sy,500}\equiv\xi_{sy}/(500\ {\rm MeV}), while bsy,imb_{sy,i}^{m} and bsy,izb_{sy,i}^{z} for i=03i=0-3 are the adjusting coefficients, depending on nc/n0n_{c}/n_{0}. In Fig. 11, the values of bsy,imb_{sy,i}^{m} and bsy,izb_{sy,i}^{z} for i=03i=0-3 are plotted as a function of nc/n0n_{c}/n_{0}, where the solid lines are the fitting of those values with the functional form given by

bsy,0m(c)=bsy,00mc2+bsy,01mc4+bsy,02mc6+bsy,03mc9,\displaystyle b_{sy,0}^{m}({\cal R}_{c})=b_{sy,00}^{m}{\cal R}_{c}^{2}+b_{sy,01}^{m}{\cal R}_{c}^{4}+b_{sy,02}^{m}{\cal R}_{c}^{6}+b_{sy,03}^{m}{\cal R}_{c}^{9}, (30)
bsy,im(c)=bsy,i0mc2+bsy,i1mc4+bsy,i2mc5+bsy,i3mc7+bsy,i4mc9,\displaystyle b_{sy,i}^{m}({\cal R}_{c})=b_{sy,i0}^{m}{\cal R}_{c}^{2}+b_{sy,i1}^{m}{\cal R}_{c}^{4}+b_{sy,i2}^{m}{\cal R}_{c}^{5}+b_{sy,i3}^{m}{\cal R}_{c}^{7}+b_{sy,i4}^{m}{\cal R}_{c}^{9}, (31)
bsy,0z(c)=bsy,00zc3+bsy,01zc4+bsy,02zc8+bsy,03zc9,\displaystyle b_{sy,0}^{z}({\cal R}_{c})=b_{sy,00}^{z}{\cal R}_{c}^{3}+b_{sy,01}^{z}{\cal R}_{c}^{4}+b_{sy,02}^{z}{\cal R}_{c}^{8}+b_{sy,03}^{z}{\cal R}_{c}^{9}, (32)
bsy,iz(c)=bsy,i0zc2+bsy,i1zc4+bsy,i2zc5+bsy,i3zc7+bsy,i4zc9.\displaystyle b_{sy,i}^{z}({\cal R}_{c})=b_{sy,i0}^{z}{\cal R}_{c}^{2}+b_{sy,i1}^{z}{\cal R}_{c}^{4}+b_{sy,i2}^{z}{\cal R}_{c}^{5}+b_{sy,i3}^{z}{\cal R}_{c}^{7}+b_{sy,i4}^{z}{\cal R}_{c}^{9}. (33)

The coefficients in these equations, bsy,ijmb_{sy,ij}^{m} and bsy,ijzb_{sy,ij}^{z}, are concretely listed in Table 5.

Refer to caption
Figure 10: ΔMηsy\Delta M_{\eta_{sy}} and Δzηsy\Delta z_{\eta_{sy}} with nc/n0=2n_{c}/n_{0}=2 and 3 are plotted as a function of ξsy\xi_{sy}, where the thick-solid lines for nc/n0=3n_{c}/n_{0}=3 and thick-dotted lines for nc/n0=2n_{c}/n_{0}=2 are fitting lines given by Eqs. (28) and (29).
Refer to caption
Figure 11: The coefficients in the fitting formulas (Eqs. (28) and (29)), bsy,imb_{sy,i}^{m} and bsy,izb_{sy,i}^{z} for i=03i=0-3, are plotted as a function of nc/n0n_{c}/n_{0}, while the solid lines are the fitting of those values as nc/n0n_{c}/n_{0} with the functional form given by Eqs. (30) – (33).
Table 5: Values of bsy,ijmb_{sy,ij}^{m} and bsy,ijzb_{sy,ij}^{z} in Eqs. (30) – (33).
jj 0 1 2 3 4
bsy,0jmb_{sy,0j}^{m} 9.146×104-9.146\times 10^{-4} 4.823×1044.823\times 10^{-4} 5.734×105-5.734\times 10^{-5} 7.712×1077.712\times 10^{-7}
bsy,1jmb_{sy,1j}^{m} 3.719×101-3.719\times 10^{-1} 6.652×1016.652\times 10^{-1} 3.572×101-3.572\times 10^{-1} 2.324×1022.324\times 10^{-2} 7.279×104-7.279\times 10^{-4}
bsy,2jmb_{sy,2j}^{m} 3.684×1013.684\times 10^{-1} 6.647×101-6.647\times 10^{-1} 3.551×1013.551\times 10^{-1} 2.302×102-2.302\times 10^{-2} 7.217×1047.217\times 10^{-4}
bsy,3jmb_{sy,3j}^{m} 2.956×102-2.956\times 10^{-2} 5.484×1025.484\times 10^{-2} 2.879×102-2.879\times 10^{-2} 1.839×1031.839\times 10^{-3} 5.768×105-5.768\times 10^{-5}
bsy,0jzb_{sy,0j}^{z} 1.032×104-1.032\times 10^{-4} 7.160×1057.160\times 10^{-5} 1.388×106-1.388\times 10^{-6} 3.541×1073.541\times 10^{-7}
bsy,1jzb_{sy,1j}^{z} 4.730×102-4.730\times 10^{-2} 7.798×1027.798\times 10^{-2} 4.105×102-4.105\times 10^{-2} 2.563×1032.563\times 10^{-3} 7.723×105-7.723\times 10^{-5}
bsy,2jzb_{sy,2j}^{z} 4.726×1024.726\times 10^{-2} 7.785×102-7.785\times 10^{-2} 4.065×1024.065\times 10^{-2} 2.522×103-2.522\times 10^{-3} 7.586×1057.586\times 10^{-5}
bsy,3jzb_{sy,3j}^{z} 3.880×103-3.880\times 10^{-3} 6.386×1036.386\times 10^{-3} 3.246×103-3.246\times 10^{-3} 1.967×1041.967\times 10^{-4} 5.867×106-5.867\times 10^{-6}

Now, we get the alternative empirical formulas for the neutron star mass and gravitational redshift as a function of c{\cal R}_{c}, ηsy\eta_{sy}, and ξsy\xi_{sy}:

MηξsyM=Mηsy(c,ηsy)M+ΔMηsy(c,ξsy)M,\displaystyle\frac{M_{\eta\xi_{sy}}}{M_{\odot}}=\frac{M_{\eta_{sy}}({\cal R}_{c},\eta_{sy})}{M_{\odot}}+\frac{\Delta M_{\eta_{sy}}({\cal R}_{c},\xi_{sy})}{M_{\odot}}, (34)
zηξsy=zηsy(c,ηsy)+Δzηsy(c,ξsy),\displaystyle z_{\eta\xi_{sy}}=z_{\eta_{sy}}({\cal R}_{c},\eta_{sy})+\Delta z_{\eta_{sy}}({\cal R}_{c},\xi_{sy}), (35)

where the first terms are given by Eqs. (22) – (25) and the second terms are given by Eqs. (28) – (33). In order to check how well one can estimate the neutron star mass and gravitational redshift with the empirical formulas with ηsy\eta_{sy}, i.e., Mηsy(c,ηsy)M_{\eta_{sy}}({\cal R}_{c},\eta_{sy}), zηsy(c,ηsy)z_{\eta_{sy}}({\cal R}_{c},\eta_{sy}), Mηξsy(c,ηsy,ξsy)M_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}), and zηξsy(c,ηsy,ξsy)z_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}), we calculate the relative deviation from the TOV solutions constructed with concrete EOSs and show the absolute value of it in Fig. 12, where the top and middle panels correspond to the mass and gravitational redshift, while the bottom panels are the relative deviation of the radius estimated with the empirical formulas for mass and gravitational redshift. Comparing to Fig. 7, one can see that the empirical formulas with ηsy\eta_{sy} are the same level as or better than those with η\eta. In fact, with respect to the canonical neutron star models, one can estimate the mass (radius) within 7%\sim 7\% (2%\sim 2\%) accuracy, using the empirical relations, Mηξsy(c,ηsy,ξsy)M_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}) and zηξsy(c,ηsy,ξsy)z_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}). We note that one can accurately estimate the radius by using the empirical formulas for the mass and gravitational redshift again, even though the dependence of the mass and gravitational redshift on ηsy\eta_{sy} are quite similar, as shown in Fig. 8.

Refer to caption
Figure 12: Same as Fig. 7, but with the empirical formulas, Mηsy(c,ηsy)M_{\eta_{sy}}({\cal R}_{c},\eta_{sy}), zηsy(c,ηsy)z_{\eta_{sy}}({\cal R}_{c},\eta_{sy}), Mηξsy(c,ηsy,ξsy)M_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}), and zηξsy(c,ηsy,ξsy)z_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}).
Table 6: Correspondence between the empirical formulas and their equations.
empirical forumula corresponding equations
Mη(c,η)M_{\eta}({\cal R}_{c},\eta) (9) and (11)
Mηξ(c,η,ξ)M_{\eta\xi}({\cal R}_{c},\eta,\xi) (19) with (9), (11), (15), & (17)
Mηsy(c,ηsy)M_{\eta_{sy}}({\cal R}_{c},\eta_{sy}) (22) and (24)
Mηξsy(c,ηsy,ξsy)M_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}) (34) with (22), (24), (28), (30), & (31)
zη(c,η)z_{\eta}({\cal R}_{c},\eta) (10) and (12)
zηξ(c,η,ξ)z_{\eta\xi}({\cal R}_{c},\eta,\xi) (20) with (10), (12), (16), & (18)
zηsy(c,ηsy)z_{\eta_{sy}}({\cal R}_{c},\eta_{sy}) (23) and (25)
zηξsy(c,ηsy,ξsy)z_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}) (35) with (23), (25), (29), (32), & (33)
Refer to caption
Figure 13: Constraint on the parameter space with ηsy\eta_{sy} and ξsy\xi_{sy} obtained from the constraint on the 1.4M1.4M_{\odot} neutron star radius, R1.4R_{1.4}, with the gravitational wave event, GW1708107, i.e., R1.413.6R_{1.4}\leq 13.6 km Annala18 . In this figure, the shaded region corresponds to the allowed region.

Finally, in Table 6, we show the corresponding equations for the empirical relations obtained in this study. In addition, using the estimation of the neutron star mass and radius with the empirical formulas, Mηξsy(c,ηsy,ξsy)M_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}) and zηξsy(c,ηsy,ξsy)z_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}), we make a constraint on the parameter space with ηsy\eta_{sy} and ξsy\xi_{sy}. That is, owing to the gravitational wave observations at the GW170817, the tidal deformability of neutron star has been constrained, which tells us that the 1.4M1.4M_{\odot} neutron star radius should be less than 13.6 km Annala18 . In practice, assuming that M=1.4MM=1.4M_{\odot} together with Mηξsy(c,ηsy,ξsy)M_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}) and zηξsy(c,ηsy,ξsy)z_{\eta\xi_{sy}}({\cal R}_{c},\eta_{sy},\xi_{sy}), one can estimate the stellar radius with the given values of ηsy\eta_{sy} and ξsy\xi_{sy}. In Fig. 13 we plot the combination of ηsy\eta_{sy} and ξsy\xi_{sy} so that the radius becomes 13 and 14 km with dashed lines and 13.6 km with solid line. So, one can see that the shaded region corresponds to the allowed region, considering the constraint through the GW170817.

IV Conclusion

The neutron star mass and radius are one of the most important observables to constrain the EOS for dense matter. In fact, some of astronomical observations could make a constraint on EOS, essentially for higher density region. On the other hand, the terrestrial nuclear experiments constrain the nuclear properties especially around the nuclear saturation density, which enables us to screen the EOSs. So, at least the neutron star models for lower density region are strongly associated with the nuclear saturation parameters. In this study, we propose the empirical formulas for the neutron star mass and gravitational redshift as a function of the central density and the suitable combination of nuclear saturation parameters, which are applicable to the stellar models constructed with the central density up to threefold nuclear density. Combining both empirical relations, the stellar radius is also estimated. Our empirical formulas can directly connect the neutron star properties to the nuclear saturation parameters, which helps us to imagine the neutron star mass and radius with the specific values of saturation parameters constrained via experiments, and vice versa. As an application with our empirical formulas, we constrain the parameter space of the nuclear saturation parameters, considering the constraint on the neutron star radius through the gravitational wave observations at the GW170817. Although the current constraint is still poor, one can discuss the nuclear saturation parameters more severely, as the astronomical observations would increase. In this study, we focus only on the empirical relations for the neutron star mass and gravitational redshift, but it must be also possible to derive the empirical formulas for the other neutron star bulk properties, such as the moment of inertia or Love number, as in Ref. SSB16 . We will consider these topics somewhere in the future.

Acknowledgements.
This work is supported in part by Japan Society for the Promotion of Science (JSPS) KAKENHI Grant Numbers JP18K13551, JP19KK0354, JP20H04753, and JP21H01088, and by Pioneering Program of RIKEN for Evolution of Matter in the Universe (r-EMU).

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