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. 2021 Dec 26;24(1):43. doi: 10.3390/e24010043

Relativistic Rational Extended Thermodynamics of Polyatomic Gases with a New Hierarchy of Moments

Takashi Arima 1, Maria Cristina Carrisi 2, Sebastiano Pennisi 2, Tommaso Ruggeri 3,*
Editor: Lamberto Rondoni
PMCID: PMC8774792  PMID: 35052069

Abstract

A relativistic version of the rational extended thermodynamics of polyatomic gases based on a new hierarchy of moments that takes into account the total energy composed by the rest energy and the energy of the molecular internal mode is proposed. The moment equations associated with the Boltzmann–Chernikov equation are derived, and the system for the first 15 equations is closed by the procedure of the maximum entropy principle and by using an appropriate BGK model for the collisional term. The entropy principle with a convex entropy density is proved in a neighborhood of equilibrium state, and, as a consequence, the system is symmetric hyperbolic and the Cauchy problem is well-posed. The ultra-relativistic and classical limits are also studied. The theories with 14 and 6 moments are deduced as principal subsystems. Particularly interesting is the subsystem with 6 fields in which the dissipation is only due to the dynamical pressure. This simplified model can be very useful when bulk viscosity is dominant and might be important in cosmological problems. Using the Maxwellian iteration, we obtain the parabolic limit, and the heat conductivity, shear viscosity, and bulk viscosity are deduced and plotted.

Keywords: relativistic extended thermodynamics, rarefied polyatomic gas, causal theory of relativistic fluids

1. Introduction

Rational extended thermodynamics (RET) is a theory applicable to nonequilibrium phenomena out of local equilibrium. It is expressed by a hyperbolic system of field equations with local constitutive equations and is strictly related to the kinetic theory with the closure method of the hierarchies of moment equations in both classical and relativistic frameworks [1,2].

The first relativistic version of the modern RET was given by Liu, Müller, and Ruggeri (LMR) [3] considering the Boltzmann–Chernikov relativistic equation [4,5,6]:

pααf=Q, (1)

in which the distribution function f depends on (xα,pβ), where xα are the space-time coordinates, pα is the four-momentum, α=/xα, Q is the collisional term, and α,β=0,1,2,3. For monatomic gases, the relativistic moment equations associated with (1), truncated at tensorial index N+1 are:

αAαα1αn=Iα1αnwithn=0,,N, (2)

with

Aαα1αn=cmn1R3fpαpα1pαndP,Iα1αn=cmn1R3Qpα1pαndP, (3)

where c denotes the light velocity, m is the particle mass in the rest frame, and

dP=dp1dp2dp3p0.

If n=0, the tensor reduces to Aα; moreover, the production tensor in the right-side of (2) is zero for n=0,1, because the first 5 equations represent the conservation laws of the particle number and of the energy-momentum, respectively.

When N=1, we have the relativistic Euler system

αAα=0,αAαβ=0, (4)

where, also in the following, AαVα and AαβTαβ have the physical meaning, respectively, of the particle number vector and the energy-momentum tensor. Instead, when N=2, we have the LMR theory of a relativistic gas with 14 fields:

αAα=0,αAαβ=0,αAαβγ=Iβγ,γ=0,1,2,3;Iαα=0. (5)

Recently, Pennisi and Ruggeri first constructed a relativistic RET theory for polyatomic gases with (2) in the case of N=2 [7] (see also [8,9]) whose moments are given by

Aα=mcR30fpαϕ(I)dIdP,Aαβ=1mcR30fpαpβ(mc2+I)ϕ(I)dIdP,Aαβγ=1m2cR30+fpαpβpγmc2+2Iϕ(I)dIdP, (6)

where the distribution function f(xα,pβ,I) depends on the extra variable I, similar to the classical one (see [2] and references therein), that has the physical meaning of the molecular internal energy of internal modes in order to take into account the exchange of energy due to the rotation and vibration of a molecule, and ϕ(I) is the state density of the internal mode.

In [7], by taking the traceless part of the third order tensor (i.e., Aαβγ) as a field instead of Aαβγ in (5)3, the relativistic theory with 14 fields (RET14) was proposed. It was also shown that its classical limit coincides with the classical RET14 based on the binary hierarchy [2,10,11]. The beauty of the relativistic counterpart is that there exists a single hierarchy of moments, but, as was noticed by the authors, to obtain the classical theory of RET14, it was necessary to put the factor 2 in front of I in the last equation of (6)! This was also more evident in the theory with any number of moments, where Pennisi and Ruggeri generalized (6) considering the following moments [12]:

Aαα1αn=1mncR30+fpαpα1pαnmc2+nIϕ(I)dIdP,Iα1αn=1mncR30+Qpα1pαnmc2+nIϕ(I)dIdP. (7)

In this case, we need a factor nI in (7) to obtain, in the classical limit, the binary hierarchy.

To avoid this unphysical situation, Pennisi first noticed that (mc2+nI) appearing in (7) are the first two terms of the Newton binomial formula for (mc2+I)n/(mc2)n1. Therefore he proposed in [13] to modify, in the relativistic case, the definition of the moments by using the substitution:

(mc2)n1mc2+nIwithmc2+In,

that is, instead of (7), the following moments are proposed:

Aαα1αn=1mc2n1R30+fpαpα1pαnmc2+Inϕ(I)dIdP,Iα1αn=1mc2n1R30+Qpα1pαnmc2+Inϕ(I)dIdP. (8)

Such definitions are more physical because now the full energy (the sum of the rest frame energy and the energy of internal modes) mc2+I appears in the moments.

The aim of this paper is to consider the system (5) with moments given by (8). In this way, for the case with N=2 also, by taking the trace part of Aαβγ as a field, we have 15 field equations, and to close the system, we adopt the molecular procedure of RET based on the maximum entropy principle.

The paper is organized as follows. In Section 2, the values of generic moments in an equilibrium state are estimated in the general case. In Section 3, the RET theory for 15 fields (RET15) is proposed, and the constitutive quantities are closed near the equilibrium state. By adopting a variant of the BGK model appropriate for polyatomic gases proposed by Pennisi and Ruggeri [14], the production tensor is derived. In Section 4, the four-dimensional entropy flux and the entropy production are deduced within the second order with respect to the nonequilibrium variables. Then, we show the condition of convexity of the entropy density and the positivity of the entropy production, which ensure the well-posedness of the Cauchy problem and the entropy principle as a result. We also discuss in Section 5 the case of the diatomic gases for which all coefficients are expressed in closed form in terms of the ratio of two Bessel functions, similar to the case of monatomic gases. In Section 6, we study the ultra-relativistic limit. In Section 7, the principal subsystems of RET15 are studied. First, we obtain RET14 in which all field variables have physical meaning. Then, at the same level as RET14 in the sense of the principal subsystem, there also exists the subsystem with 6 fields in which the dissipation is only due to the dynamical pressure. This system is important in the case that the bulk viscosity is dominant compared to the shear viscosity and heat conductivity, and it must be particularly interesting in cosmological problems. The simplest subsystem is the Euler non-dissipative case with 5 fields. In Section 8, we use the Maxwellian iteration and, as a result, the phenomenological coefficients of the Eckart theory, that is, the heat conductivity, shear viscosity, and bulk viscosity are determined with the present model. Finally, in Section 9, we show that the classic limit of the present model coincides with the classical RET15 studied in [15].

2. Distribution Function and Moments at Equilibrium

The equilibrium distribution function fE of polyatomic gas that generalizes the Jüttner one of monatomic gas was evaluated in [7] with the variational procedure of the maximum entropy principle (MEP) [1,16,17,18]. Considering the first 5 balance equations of (5) in equilibrium state:

AEαVEα=mnUα,AEαβTEαβ=phαβ+ec2UαUβ.

MEP requires that the appropriate distribution function ff(xα,pα,I) is the one which maximizes the entropy density

ρS=hE=hEαUα=kBcUαR30+flnfpαϕ(I)dIdP,

under the constraints that the temporal parts VαUα and TαβUβ are prescribed. Here, kB,n,ρ(=nm),Uα,hαβ,p,e,S are, respectively, the Boltzmann constant, the particle number, the mass density, the four-velocity (UαUα=c2), the projector tensor (hαβ=UαUβ/c2gαβ), the pressure, the energy, and the entropy density, and gαβ=diag(1,1,1,1) is the metric tensor.

The equilibrium distribution function for a rarefied polyatomic gas that maximizes the entropy has the following expression [7]:

fE=nA¯(γ)14πm3c3e1kBT1+Imc2Uβpβ,A¯(γ)=0+J2,1*ϕ(I)dI (9)

with T being the absolute temperature,

Jm,n*=Jm,n(γ*),γ*=γ1+Imc2,γ=mc2kBT,

and

Jm,n(γ)=0+eγcoshssinhmscoshnsds,

subjected to the following recurrence relations [3,7]:

Jm+2,n(γ)=Jm,n+2(γ)Jm,n(γ), (10)
γJm+2,n(γ)=nJm,n1(γ)(n+m+1)Jm,n+1(γ). (11)

The pressure and the energy compatible with the equilibrium distribution function (9) are [7]:

p=kBmρT,e=ρc2ω(γ),withω(γ)=0+J2,2*1+Imc2ϕ(I)dI0+J2,1*ϕ(I)dI. (12)

Taking into account that e=ρc2+ρε, where ε is the internal energy, we deduce from (12):

ε=c2(ω1). (13)

Therefore, the internal energy is a function only of γ or, it is the same, of T as in the classical case for rarefied gases.

The moments in equilibrium state AEαα1αj for j2 were deduced in [13]:

AEα1αj+1=k=0j+12ρc2kθk,jh(α1α2hα2k1α2kUα2k+1Uαj+1), (14)

where

θk,j=12k+1j+12k0+J2k+2,j+12k*1+Imc2jϕ(I)dI0+J2,1*ϕ(I)dI (15)

are dimensionless functions depending only on γ. Taking into account (12) and (15), we obtain θ0,0=1,θ0,1=ω(γ), and using the recurrence Formula (10) and (11), in [13], the following recurrence relations hold:

θ0,0=1,θ0,j+1=ω(γ)θ0,jθ0,jwith=ddγ,θh,j+1=j+2γθh,j+j+32h2hθh1,jforh=1,,j+12,θj+22,j+1=1γθj2,jfor j even. (16)

It is interesting to see that all the scalar coefficients can be expressed in terms of the function ω(γ) and of its derivatives with respect to γ (or with respect to the temperature T), and ω is strictly related to the internal energy ε by (13). A similar situation is studied in the article [15] for the non-relativistic case.

The values of θh,j can be determined, by using the recurrence Formula (16), according to the following diagram:

θ0,0θ0,1θ0,2θ0,3θ1,1θ1,2θ1,3θ2,3θ2,4

We see that all the θ0,j can be obtained from θ0,0 by using Equation (16)2, and the other θh,j with jh can be obtained from Equations (16)3,4. In particular, we can evaluate the following ones that need to be known for the model with 15 fields in the subsequent sections:

θ0,0=1,θ0,1=ω,θ0,2=ω2ω,θ0,3=ω3+ω3ωω,θ0,4=ω4ω+4ωω+3ω26ω2ω,θ1,1=1γ,θ1,2=3γ2(γω+1),θ1,3=6γ3γ2(ω2ω)+2(γω+1),θ1,4=10γ43γω(γω+2)γω+6+γ3(ω3+ω3ωω),θ2,3=3γ3(γω+1),θ2,4=15γ4γ2(ω2ω)+3(γω+1). (17)

3. The Closure for the 15 Moments Model

In this section, we consider the simplest and physical case, that is, the system (2) for n=0,1,2 with the moments given by (8):

αVα=0,αTαβ=0,αAαβγ=Iβγ,β,γ=0,1,2,3. (18)

with

Vα=mcR30+fpαϕ(I)dIdP,Tαβ=cR30+fpαpβ1+Imc2ϕ(I)dIdP,Aαβγ=cmR30+fpαpβpγ1+Imc22ϕ(I)dIdP,Iβγ=cmR30+Qpβpγ1+Imc22ϕ(I)dIdP. (19)

To close the system (19), we adopt the MEP, which requires finding the distribution function that maximizes the non-equilibrium entropy density:

h=hαUα=kBcUαR30+flnfpαϕ(I)dIdPmax (20)

under the constraints that the temporal part VαUα,TαβUα and AαβγUα are prescribed. Proceeding in the usual way as indicated in previous papers of RET (see [2,7]), we obtain:

f15=e1χkB,withχ=mλ+λμpμ1+Imc2+1mλμνpμpν1+Imc22, (21)

where λ,λμ,λμν are the Lagrange multipliers.

Hereafter, recalling the following decomposition of the particle number vector and the energy-momentum tensor

Vα=ρUα,Tαβ=ec2UαUβ+p+Πhαβ+1c2(Uαqβ+Uβqα)+t<αβ>3, (22)

we can choose as fields, as usual, 14 physical variables; ρ, T, Uα, Π, qα, t<αβ>3, where Π is the dynamic pressure, qα=hμαUνTμν is the heat flux, and t<αβ>3=Tμνhμαhνβ13hαβhμν is the deviatoric shear viscous stress tensor. We also recall the constraints:

UαUα=c2,qαUα=0,t<αβ>3Uα=0,tα>3<α=0,

and we choose as the 15th variable:

Δ=4c2UαUβUγAαβγAEαβγ. (23)

The pressure p and the energy e as function of (ρ,T) are given in (12).

Remark 1.

For any symmetric tensor Mαβ, we can define its traceless part M<αβ> and its 3-dimensional traceless part M<αβ>3, which is the traceless part of its projection in the 3-dimensional space orthogonal to Uα, as follows

M<αβ>=gμαgνβ14gαβgμνMμν=Mαβ14gμνMμνgαβ,M<αβ>3=hμαhνβ13hαβhμνMμν,

which are different except for the case in which MμνUμ=0 and Mμνgμν=0. In fact, these conditions indicate that

M<αβ>=M<αβ>3.

Moreover, in the following, a parenthesis between two indexes indicates the symmetric part.

3.1. The Linear Deviation from Equilibrium

The thermodynamical definition of the equilibrium according to Müller and Ruggeri [1] is the state in which the entropy production vanishes and hence attains its minimum value. Using this definition, the theorem was proved [19,20] that the components of the Lagrange multipliers of the balance laws of nonequilibrium variables vanish, and only the five Lagrange multipliers corresponding to the equilibrium conservation laws (Euler system) remain. In the present case, we have:

λE=1Tg+c2,λμE=UμT,λμνE=0, (24)

where g=ε+p/ρTS is the equilibrium chemical potential. We remark that λE,λμE are the components of the main field that symmetrize the relativistic Euler system, as was first proved by Ruggeri and Strumia (see [21]).

In the molecular RET approach, we consider, as usual, the processes near equilibrium. For this reason, we expand (21) around an equilibrium state as follows:

f15fE11kBχ˜,χ˜=m(λλE)+(λμλμE)pμ1+Imc2+1mλμνpμpν1+Imc22. (25)

Inserting the distribution function (25) into the moments (19), we obtain the following system:

0=VαVEα=mkBVEα(λλE)+TEαμλμλμE+AEαμνλμν,t<αβ>3+Πhαβ+2c2U(αqβ)=mkBTEαβ(λλE)+AEαβμλμλμE+AEαβμνλμν,AαβγAEαβγ=mkBAEαβγ(λλE)+AEαβγμλμλμE+AEαβγμνλμν, (26)

where the equilibrium values of the tensors AEαβμ,AEαβμν, and AEαβμνγ can be obtained by (14), taking j=2,3,4:

AEαβγ=ρθ0,2UαUβUγ+ρc2θ1,2h(αβUγ),AEαβμν=ρθ0,3UαUβUμUν+ρc2θ1,3h(αβUμUν)+ρc4θ2,3h(αβhμν),AEαβγμν=ρθ0,4UαUβUγUμUν+ρc2θ1,4h(αβUγUμUν)+ρc4θ2,4h(αβhγμUν), (27)

with the θ’s given in (17).

The system (26) permits one to deduce the 15 Lagrange multipliers in terms of the 15 field variables, including Δ given in (23), and then we can obtain the remaining part of the tensor Aαβγ.

To solve this system, we consider first Equation (26)1 contracted with Uα, Equation (26)2 contracted with UαUβ, Equation (26)3 contracted with UαUβUγ/c3, Equation (26)2 contracted with hαβ/3, and (26)3 contracted with Uαhβγ/(3c2), obtaining the system

θ0,0(λλE)+θ0,1UμλμUμT+θ0,2UμUνλμν+c23θ1,2hμνλμν=0,θ0,1(λλE)+θ0,2UμλμUμT+θ0,3UμUνλμν+c26θ1,3hμνλμν=0,θ0,2(λλE)+θ0,3UμλμUμT+θ0,4UμUνλμν+c210θ1,4hμνλμν=kB4m2nc4Δ,θ1,1(λλE)+13θ1,2UμλμUμT+16θ1,3UμUνλμν+59c2θ2,3hμνλμν=kBm2nc2Π,13θ1,2(λλE)+16θ1,3UμλμUμT+110θ1,4UμUνλμν+c29θ2,4hμνλμν==kB3m2c4nAαβγAEαβγUαhβγ. (28)

This is a system of 5 equations in the 4 unknowns λλE, UμλμUμT, UμUνλμν, hμνλμν; in order to have solutions, the determinant of the complete matrix must be zero, that is,

0=θ0,0θ0,1θ0,213θ1,20θ0,1θ0,2θ0,316θ1,30θ0,2θ0,3θ0,4110θ1,4kB4mc4Δθ1,113θ1,216θ1,359θ2,3kBmc2Π13θ1,216θ1,3110θ1,419θ2,4kB3mc4AαβγAEαβγUαhβγ. (29)

By defining

D4=θ0,0θ0,1θ0,213θ1,2θ0,1θ0,2θ0,316θ1,3θ0,2θ0,3θ0,4110θ1,4θ1,113θ1,216θ1,359θ2,3,NΠ=θ0,0θ0,1θ0,213θ1,2θ0,1θ0,2θ0,316θ1,3θ0,2θ0,3θ0,4110θ1,413θ1,216θ1,3110θ1,419θ2,4,NΔ=θ0,0θ0,1θ0,213θ1,2θ0,1θ0,2θ0,316θ1,3θ1,113θ1,216θ1,359θ2,313θ1,216θ1,3110θ1,419θ2,4,

Equation (29) gives:

13c2AαβγAEαβγUαhβγ=NΠD4ΠNΔD414c2Δ. (30)

We contract now Equation (26)1 with hαδ, Equation (26)2 with Uαhβδ, Equation (26)3 with UαUβhγδ/c3 and (26)3 with hαδhβγ/(3c2), obtaining the system

c2θ1,1hδμ(λμλμE)+23c2θ1,2Uμhδνλμν=0,c2θ1,2hδμ(λμλμE)+c2θ1,3Uμhδνλμν=3kBm2c2nqδ,c2θ1,3hδμ(λμλμE)+1815c2θ1,4Uμhδνλμν=6kBm2c4nAαβγAEαβγUαUβhγδ,53c4θ2,3hδμ(λμλμE)+23c4θ2,4Uμhδνλμν=kBm2nAαβγAEαβγhαβhγδ. (31)

By eliminating the parameters hδμ(λμλμE) and Uμhδνλμν from these equations, we obtain

AαβγAEαβγUαUβhγδ=c2N3D3qδ,AαβγAEαβγhαβhγδ=N31D3qδ, (32)

with

D3=θ1,1θ1,2θ1,232θ1,3,N3=12θ1,1θ1,2θ1,395θ1,4,N31=θ1,1θ1,25θ2,33θ2,4.

We contract now Equation (26)2 with hα<δhβθ>3 and (26)3 with hα<δhβθ>3Uγ, obtaining

kBmt<δθ>3=23mnc4θ2,3hμ<δhθ>3νλμν,AαβγAEαβγhα<δhβθ>3Uγ=215mkBmnc6θ2,4hμ<δhθ>3νλμν, (33)

from which it follows

AαβγAEαβγhα<δhβθ>3Uγ=C5c2t<δθ>3withC5=15θ2,4θ2,3. (34)

Finally, (26)3 contracted with hα<δhβθhγψ>3 gives

AαβγAEαβγhα<δhβθhγψ>3=0.

This result, jointly with (30), (32), and (34), gives the decomposition of the triple tensor Aαβγ:

AαβγAEαβγ=14c4ΔUαUβUγ34c2NΔD4Δh(αβUγ)3NΠD4Πh(αβUγ)+3c2N3D3q(αUβUγ)+35N31D3h(αβqγ)+3C5t(<αβ>3Uγ).

Thanks to Equation (27)1, we have the closure of the triple tensor in terms of the physical variables:

Aαβγ=ρθ0,2+14c4ΔUαUβUγ+ρc2θ1,234c2NΔD4Δ3NΠD4Πh(αβUγ)+3c2N3D3q(αUβUγ)+35N31D3h(αβqγ)+3C5t(<αβ>3Uγ). (35)

3.2. Inversion of the Lagrange Multipliers

In this section, we present the explicit expression of the Lagrange multipliers in terms of the 15 physical independent variables. From the representation theorems, they are expressed as follows:

λλE=a1Π+a2Δ,λμλμE=b1Π+b2ΔUμ+b3qμ,λμν=α1Π+β1ΔUμUν+α2Π+β2Δhμν+α3qμUν+qνUμ+α4t<μν>3, (36)

where λE and λμE can be found in Equation (24), and the coefficients a1,2,b1,2,3, α1,2,3,4 and β1,2 are functions of ρ and γ. By using Equations (28), (31) and (33), it is possible to obtain the explicit expressions of these coefficients.

For convenience, let us denote by D4ij the minor determinant obtained from D4 by deleting its ith row and jth column. From system (28), we obtain

λλE=kBmc4ρD4Πc2D441+Δ4D431,Uμ(λμλμE)=kBmc4ρD4Πc2D442Δ4D432,UβUγλβγ=kBmc4ρD4Πc2D443+Δ4D433,hβγλβγ=kBmc4ρD4ΠD444Δ4c2D434. (37)

From system (31) we obtain

hδμλμλμE=3kBθ1,2mc4ρD3qδandUβhγδλβγ=9kBθ1,12mc4ρD3qδ. (38)

Finally, from Equation (33) we have

hβ<δhθ>3γλβγ=3kB2mc4ρθ2,3t<δθ>3,

that, multiplied by t<δθ>3, gives

t<βγ>3λβγ=3kB2mc4ρθ2,3t<βγ>3t<βγ>3. (39)

By comparing Equations (36)1 with (37)1, we have

a1=kBmc2ρD4D441,a2=kB4mc4ρD4D431. (40)

By multiplying Equation (36)2 times Uμ and hμδ, respectively, and using Equations (37)2 and (38)1, we have

b1=kBmc4ρD4D442,b2=kB4mc6ρD4D432,b3=3kBθ1,2mc4ρD3. (41)

Finally, by multiplying Equation (36)3 times UμUν, hμν, Uνhμδ, hμ<δhθ>ν, respectively, and using Equations (37)–(39), we obtain that

α1=kBmc6ρD4D443,α2=kB3mc4ρD4D444,α3=9kBθ1,12mc6ρD3,α4=3kB2mc4ρθ2,3,β1=kB4mc8ρD4D433,β2=kB12mc6ρD4D434. (42)

3.3. Production Term with a Variant BGK Model

To complete the closure of the system (18), we need to have the expression of the production tensor Iβγ. It depends on the collisional term Q (see (19)2), and obtaining the expression of Q is a hard task in relativity. Usually, for monatomic gas, the relativistic generalization of the BGK approximation first made by Marle [22,23] and successively by Anderson and Witting [24] is adopted. The Marle model is an extension of the classical BGK model in the Eckart frame [6,25], and the Anderson–Witting model obtains such extension using the Landau–Lifshitz frame [6,26]. There are some weak points for the Marle model, and the Anderson–Witting model uses the Landau–Lifshitz four velocity. Starting from these considerations, Pennisi and Ruggeri proposed a variant of the Anderson–Witting model in the Eckart frame both for monatomic and polyatomic gases, and proved that the conservation laws of particle number and energy-momentum are satisfied and the H-theorem holds [14] (see also [2]). In the polyatomic case, the following collision term has been proposed:

Q=Uαpαc2τfEffEpμqμ1+Imc2bmc2, (43)

where 3b is the coefficient of h(αβUγ) in Equation (27)1, that is, 3b=ρc2θ1,2, and τ>0 denotes the relaxation time.

Recently, the existence and asymptotic behavior of classical solutions for the Boltzmann–Chernikov Equation (1) with Q given by (43) when the initial data is sufficiently close to a global equilibrium was proved [27].

The most general expression of a nonequilibrium double tensor as a linear function of Δ, Π, t<μν>3 and qμ is the following:

Iβγ=(B1ΔΔ+B1ΠΠ)UβUγ+(B2ΔΔ+B2ΠΠ)hβγ+BqU(βqγ)+Btt<βγ>3.

In order to determine the coefficients in Iαβ, we have to substitute Equation (43) into Equation (19)4, obtaining

Iβγ=cmR30+Uαpαc2τfEffEpμqμ1+Imc2bmc2pβpγ1+Imc22ϕ(I)dIdP==Uαc2τ(AEαβγAαβγ)3Uαqμθ1,2m2nc6τAEαβγμ,

then we have

B1Δ=14c4τ,B1Π=0,B2Δ=14c2τNΔD4,B2Π=1τNΠD4Bq=1c2τθ1,3θ1,22N3D3,Bt=1τC5. (44)

Therefore, the final expression of the production term Iβγ is

Iβγ=1τ14c4ΔUβUγ+14c2NΔD4Δ+NΠD4Πhβγ+2c2N3D3+θ1,3θ1,21c2q(βUγ)C5t<βγ>3 (45)

We summarize the results of this section as:

Statement 1.

The closed system (18) obtained via MEP is the one for which Vα,Tαβ,Aαβγ,Iβγ are given explicitly in terms of the 15 fields (ρ,γ,Π,Δ,Uα,qα,t<αβ>3) using the expressions (22), (35), and (45). All coefficients are completely determined in terms of a single function ω(γ) given by Equation (12)3 and its derivatives up to the order 3. Observe, by taking into account (13), that the coefficients θ’s given in (17) can be formally written in terms of the internal energy ε and its derivatives.

3.4. Closed System of the Field Equations and Material Derivative

It is now possible to explicitly write the differential system for the field variables using the material derivative. The relativistic material derivative of a function f is defined as the derivative with respect to the proper time τ¯ along the path of the particle:

f˙=dfdτ¯=dfdtdtdτ¯=Γ(tf+vjjf)=Uααf, (46)

where Γ is the Lorentz factor, and we take into account that

Uα=dxαdτ¯(Γc,Γvj),

where vj is the velocity. Now, we observe that for any balance laws, we can have the following identity:

Iα1αn=αAαα1αn=gαββAαα1αn=hαβ+UβUαc2βAαα1αn==Uαc2A˙αα1αnhαββAαα1αn.

In our case with n=0,1,2, these equations are written as follows:

αρUα=0,hδβUαc2T˙αβhαμμTαβ=0,UβUαc2T˙αβhαμμTαβ=0,hδβhθγUαc2A˙αβγhαμμAαβγIβγ=0,hδβUγUαc2A˙αβγhαμμAαβγIβγ=0,UβUγUαc2A˙αβγhαμμAαβγIβγ=0.

By using the expressions (22), (35), and (45), respectively, for Vα,Tαβ, Aαβγ and Iβγ, we see that these become

ρ˙+ραUα=0,e+p+Πc2U˙δ+1c2hβδq˙β+1c2t<αδ>3U˙αhδμμ(p+Π)1c2qμμUδ1c2qδαUαhβδhαμμt<αβ>3=0,e˙+2Uαc2q˙α+(e+p+Π)αUαhαμμqαt<αβ>3αUβ=0,hδβ13ρc2θ1,214c2NΔD4ΔNΠD4Π+C5hδγhθβt˙<θγ>3+t<δβ>3C˙52c2N3D3+15N31D3q(δhβ)γU˙γ15c2N31D3hβδqαU˙α+13ρc2θ1,2+14c2NΔD4Δ+NΠD4ΠhδβαUα+2hθ(δhβ)μμUθ+15qμhδβ+2q(δhβ)μμN31D315N31D3hδβhαμμqα+2hθ(δhβ)μμqθ+C5t<δβ>3αUα+2t<μγ>3hγ(βhδ)θμUθ=1τ14c2NΔD4Δ+NΠD4Πhδβ1τC5t<δβ>3,hβδU˙βρθ0,2c2+23ρc2θ1,2+14c2Δ12c2NΔD4Δ2NΠD4Π+hβδN3D3q˙βqδN3D3+2C51t<δγ>3U˙γhδμμ13ρc4θ1,214NΔD4ΔNΠD4c2ΠN3D3+15N31D3qμμUδ+qδαUα+15N31D3hδμqγμUγ+hαμμC5c2t<αδ>3=1τN3D3θ1,32θ1,2qδ,ρθ0,2c4+14Δ3N3D3qαU˙α+αUα·ρθ0,2c4+23ρc4θ1,2+14Δ12NΔD4Δ2NΠD4Πc2hαμμN3D3c2qα2C5c2t<μγ>3μUγ=14τΔ. (47)

It may be useful to decompose (47)4 into the trace and spatial traceless parts. The trace part is given by

ρc2θ1,234c2NΔD4Δ3NΠD4Π+C5hθγt˙<θγ>3+1c22N3D315N31D3qγU˙γ13ρc2θ1,2+14c2NΔD4Δ+NΠD4ΠαUα+qμμN31D3N31D3hαμμqα2C5tγ>3<μμUγ=3τ14c2NΔD4Δ+NΠD4Π, (48)

and the spatial traceless part is:

C5hγ<δhβ>3θt˙<γθ>3+t<δβ>3C˙5+2c2N3D3+15N31D3q<δU˙β>3++213ρc2θ1,2+14c2NΔD4Δ+NπD4πhγ<δhβ>3μμUγ++25q<δhβ>3μμN31D325N31D3hγ<δhβ>3μμqγ++C5t<δβ>3αUα+2t<μγ>3hγ<βhδ>3νμUν=1τC5t<δβ>3. (49)

The system formed by the 15 Equations (47)1,2,3, (48), (49) and (47)5,6 is a closed system for the 15 unknown (ρ,Uδ,T,Π,t<αβ>3,qδ,Δ).

4. Entropy Density, Convexity, Entropy Principle, and Well-Posedness of Cauchy Problem

In this section, we evaluate the entropy law, and we want to prove that all solutions are entropic with an entropy density that is a convex function.

4.1. Entropy Density

By substituting the distribution function (25) with (36) into (20), we can evaluate the four-dimensional entropy flux. In this procedure, it is necessary to be careful concerning the order of the nonequilibrium variables. The present linear constitutive equation is related to the entropy with the second order of the nonequilibrium variables. By taking into account up to the second order in the expansion of the distribution function and of the constitutive equations, we may evaluate as follows:

hα=hEα+h(1)α+h(2)α, (50)

where h(1)α and h(2)α are, respectively, the contribution of the first and second order terms of the nonequilibrium variables, which can be derived as follows (see Appendix A for details):

h(1)α=ckBR30+pαfEχEχ˜(1)φ(I)dIdP,h(2)α=c2kBR30+pαfEχ˜(1)2φ(I)dIdP, (51)

where χ˜(1) is χ˜ defined in (25) with the linear constitutive equations studied in the previous. After cumbersome calculations, we obtain explicit expression of them as follows:

h(1)α=λEVαVEα+UμTTαμTEαμ=qαT,h(2)α=m2kBλλE2VEα+λμλμEλνλνEAEαμν+λμνλψθAEαμνψθ++2λλEλμλμETEαμ+2λλEλμνAEαμν+2λθλθEλμνAEαθμν=1c2Uαc2α4C52t<μν>3t<μν>3c2α3N3D3+b32qμqμ+L1Π2+L2Δ2+2L3ΠΔ+12b1b3+c2N3D3α1+N31D3α2+2α3c2NΠD4Πqα+12b2+c2N3D3β1+N31D3β2+12α3NΔD4Δqα+12b3+2c2α3C525α4N31D3t<αμ>3qμ, (52)

where

L1=3c22α2NΠD4,L2=183β2NΔD4c2β1,L3=143α24NΔD4+3c2β2NΠD4c2α14.

In particular, for the entropy density h=hαUα, we have

h=hE+c2α4C52t<μν>3t<μν>3+c2α3N3D3+b32qμqμΠΔL1L3L3L2ΠΔ. (53)

We emphasize that the convexity of the entropy density is satisfied because from (52)1, we have h(1)αUα=0, and from (51), we have h(2)αUα<0 everywhere and zero only at equilibrium. Therefore, the following inequalities are automatically satisfied:

α4C5<0,2c2α3N3D3+b3>0(becauseqαqα<0),L1>0,L1L2L32>0.

4.2. Entropy Production

According with the theorem proved by Boillat and Ruggeri [19] (see also [1,2]), the procedure of MEP at molecular level is equivalent to the closure using the entropy principle, and the Lagrange multipliers coincide with the main field for which the original system becomes symmetric hyperbolic [2]. Therefore, the closed system satisfies the entropy balance law

αhα=Σ, (54)

where the entropy four-vector is given by (50), (52). For what concerns the entropy production Σ according to the result of Ruggeri and Strumia [2], this is given by the scalar product between the main field components and the production terms [21]. In the present case, we have

Σ=Iβγλβγ. (55)

By using Equation (45), we have

Σ=1τ14c4ΔUβUγλβγ+14c2NΔD4Δ+NΠD4Πhβγλβγ+2c2N3D3+θ1,3θ1,21c2q(βUγ)λβγC5t<βγ>3λβγ. (56)

By substituting Equations (37)–(39) into Equation (56), and remembering that qβUγλβγ=qαhαβUγλβγ, we obtain Σ in a quadratic form, as follows:

Σ=3kBC52τmc4ρθ2,3t<βγ>3t<βγ>3+9kBθ1,12τm2nc6D32N3D3+θ1,3θ1,2qαqα+ΔΠM1M2M2M3ΔΠ, (57)

where

M1=kB16c8τm2nD4D433+NΔD4D434,M2=kB4c6τm2nD4D443+NΔD4D444NΠD4D434,M3=kBc4τm2nD4NΠD4D444.

The Sylvester criteria allow us to state that the quadratic form is positive definite iff all the following conditions hold:

3kBC52τmc4ρθ2,3>0,2N3D3+θ1,3θ1,29kBθ1,12τm2nc6D3<0,M1>0,M1M3(M2)2>0. (58)

The first condition of (58) is automatically satisfied because of the definition of the functions involved.

In order to prove the second condition, we can consider a space like vector Xβ and the following function that is defined to be positive for each value of Xβ:

g(Xβ)=UαcτkBR30+fEpαXβpβθ1,3θ1,21+Imc22mc21+Imc22Uνpν2ϕ(I)dIdP.

By exploiting the calculation in the above integral and by using Equation (27), we have

g(Xβ)=m2nc2τkB13θ1,32θ1,225θ1,4XβXβ.

If we choose, as a particular value,

Xβ=1D39kB2m2nc4θ1,1qβ,

we obtain

g(Xβ)=9kBθ1,12τm2nc6D32N3D3+θ1,3θ1,2qαqα>0.

This proves that also the second condition of (58) is satisfied.

Conditions 3 and 4 of (58) can be proved by showing that they are coefficients of a quadratic form that is definite positive. In order to obtain the entropy production up to the second order, we have to substitute Equation (19)4 into (55) and take the collisional term (43) up to the first order. Then,

Σ(2)=cmR30+Q(1)pβpγλβγ1+Imc22ϕ(I)dIdP,

with

Q(1)=fEc2τkBUαpαχ˜kBbmc2pμqμ1+Imc2.

If we substitute to λβγ its expression obtained from Equation (25)2, we obtain

Σ(2)=cR30+Q(1)χ˜ϕ(I)dIdP.

In the state where qβ=0 and t<αβ>3=0, the Lagrange multipliers and the Entropy production assume particular values that we denote with a *, in particular

Σ(2*)=cmR30+Q(1*)χ˜*ϕ(I)dIdP=cmR30+fEc2τkBUαpαχ*˜2ϕ(I)dIdP,

which is clearly a positive quantity. Moreover, we have

Σ(2*)=Iβγ*λβγ*

which corresponds to the quadratic form

ΔΠM1M2M2M3ΔΠ,

which, therefore, turns out to be definite positive. Therefore, the following is proved:

Statement 2.

The entropy density (53) is a convex function and has its maximum at equilibrium. The solutions satisfies the entropy principle (54) with an entropy production (57) that is always non-negative. According to the general theory of symmetrization given first in covariant formulation in [21], and the equivalence between Lagrange multipliers and main field [19], the closed system is symmetric hyperbolic in the neighborhood of equilibrium if we chose as variables the main field variables (36), with coefficients given in (40)–(42), and the Cauchy problem is well posed locally in time.

5. Diatomic Gases

The system (47) is very complex, in particular, because it is not simple to evaluate the function ω(γ), which involves two integrals (12)3 that cannot have analytical expression for a generic polyatomic gas. Taking into account the relations [7]

J2,1(γ)=1γK2(γ),J2,2(γ)=1γK3(γ)1γK2(γ),

where Kn denotes the modified Bessel function, we can rewrite ω given in (12)3 in terms of the modified Bessel functions [7]:

ω(γ)=1γ0+K3(γ*)ϕ(I)dI0+K2(γ*)γ*ϕ(I)dI1.

Moreover, to calculate the integrals, we need to prescribe the measure ϕ(I). In [7], the measure ϕ(I) was assumed as

ϕ(I)=Ia,a=D52,

because it is the one for which the macroscopic internal energy in the classical limit, when γ, it converges with that of a classical polyatomic gas, where D indicates the degree of freedom of a molecule. As was observed by Ruggeri, Xiao, and Zhao [28] in the case of a=0 (i.e., D=5 corresponding to diatomic gas), the energy e has an explicit expression similar to monatomic gas:

e=pγK0(γ)K1(γ)+3.

Therefore, from (12), we have

ωdiat(γ)=K0(γ)K1(γ)+3γ.

Using the following recurrence formulas of the Bessel functions

Kn(γ)=γ2nKn+1(γ)Kn1(γ), (59)

we can express ω in terms of

G(γ)=K3(γ)K2(γ).

In fact, we can obtain immediately the following expression:

ωdiat(γ)=1γ+γγG4, (60)

which is a simple function similar to the one of monatomic gas, for which we have [3]:

ωmono(γ)=1+γG.

Taking into account that the derivatives of the Bessel function are known, all coefficients appearing in the differential system (47) can be written explicitly in terms of G(γ), by using (59) and the recurrence Formula (58). This is simple by using a symbolic calculus like Mathematica®.

6. Ultra-Relativistic Limit

In the ultra-relativistic limit where γ0, it was proved in [29,30] that the energy converges to

e=(α+1)nmc2γ,withα=2ifa2aifa2. (61)

This implies

ωultra=(α+1)γ,withα=2ifa2aifa2. (62)

By means of this expression, we can evaluate the coefficients θh,j in (17), which become:

θ0,0,θ0,1,θ0,2,θ0,3,θ0,4=1,α+1γ,(α+1)(α+2)γ2,(α+1)(α+2)(α+3)γ3,(α+1)(α+2)(α+3)(α+4)γ4,θ1,1,θ1,2,θ1,3,θ1,4=1γ,3(α+2)γ2,6(α+2)(α+3)γ3,10(α+2)(α+3)(α+4)γ4,θ2,3,θ2,4=3(α+2)γ3,15(α+2)(α+4)γ4.

It follows that, in the ultra-relativistic limit, we have

N3D3=2(α+3)γ,N31D3=10γ,C5=α+4γ,

and

NΠD4=α+4γ,NΔD4=1α+1, (63)

where the last two equations hold for α2 (i.e., a2). For a=2, the ultra-relativistic limit of NΠD4 and of NΔD4 gives the indeterminate form 00. We show (see Appendix B for details) that it can be solved by considering higher order terms for the energy e, allowing one to prove that Equation (63) is valid also with a=2, and hence that the closure of the present model is continuous with respect to the parameter α, at the ultra-relativistic limit.

7. Principal Subsystems of RET15

For a general hyperbolic system of balance laws, the system with a smaller set of the field equations can be deduced (principal subsystems), retaining the property that the convexity of the entropy and the positivity of the entropy production is preserved according to the definition given in [20]. The principal subsystems are obtained by putting some components of the main field as a constant, and the corresponding balance laws are deleted.

Let us recall the system (18). The balance law of Aαβγ is divided into the trace part Aβαβ and the traceless part Aα<βγ>. As we study below, by deleting the trace part and putting the corresponding component of the main field as zero, we obtain the theory with 14 fields (RET14). On the other hand, by conducting the same procedure on the traceless part, we obtain the theory with 6 fields (RET6). It is remarkable that RET14 and RET6 is the same order in the sense of the principle subsystem, differently from the classical case in which the classical RET6 is a principal subsystem of classical RET14. Moreover, the relativistic Euler theory is deduced as a principal subsystem by deleting the balance laws of Aαβγ and putting the corresponding component of the main field as zero.

7.1. RET14: 14 Fields Theory

The RET14 is obtained as a principal subsystem of RET15 under the condition λαα=0. From (36)3, this condition provides Δ expressed by Π as follows:

Δ(14)=c2α13α2c2β13β2Π=4NaDac2Π, (64)

where Na=D444+D443 and Da=D434+D433. Then, the independent fields are the following 14 fields: (ρ,γ,Π,Uα,qα,t<αβ>3). By deleting the balance equation corresponding to λαα, that is, the one of Aβαβ, the present system of the balance equations is as follows:

αVα=0,αTαβ=0,αAα<βγ>=I<βγ>. (65)

With (64), the constitutive equation is modified in this subsystem. For the comparison with the RET14 theory studied in [7], let us denote

N1πD1π=13NaDa,N11πD1π=1D4NaDaNΔ+NΠ.

We can prove the following identity:

NbDa=1D4NaDaNΔ+NΠ,withNb=NΔ34+NΔ33,

where NΔ33 and NΔ34 are the minor determinants of NΔ, which deletes the third row and third column, and the third row and fourth column, respectively. Then, as a result, instead of (35), the closure for Aαβγ in the present principal subsystem is given by

Aαβγ=ρθ0,23c2N1πD1πΠUαUβUγ+ρc2θ1,23N11πD1πΠU(αhβγ)++3c2N3D3q(αUβUγ)+35N31D3q(αhβγ)+3C5t(<αβ>3Uγ). (66)

This result is formally the same as the result of [7] (Equation (56) of the paper). However, there are differences in the coefficients due to the presence of mc2+In instead of mc2+nI in the integrals.

Similarly, we obtain the production term in this principal subsystem as follows:

I<βγ>=1c2τ3N1π+N11πD1πΠU<βUγ>+1c2τθ1,3θ1,22N3D3q(βUγ)1τC5t<βγ>3. (67)

This expression (67) is formally the same as the result of [8] (Equation (16) of the paper), except that now we have θ1,3θ1,2 instead of B2B4 defined in [8], and the difference of the integral in the coefficients is similar with the case for Aαβγ.

The system (65) is symmetric hyperbolic in the main field (λ,λα,λ<μν>)given respectively by (36) withΔ=Δ(14) given by (64).

7.2. RET6: 6 Fields Theory

We consider the principal subsystem with λ<μν>=λμν14λααgμν=0, and then we have

λμν=14λααgμν. (68)

By comparing it with (36), we have

α1+α2c2Π+β1+β2c2Δ=0,qμ=0,t<μν>3=0.

The first equation indicates that, in this principal subsystem, Δ is expressed with Π as follows:

Δ(6)=c2α1+α2c2β1+β2Π=wΠ (69)

where

w=4c2D4443D443D4343D433.

It should be mentioned that the relation between Δ and Π is different from the case of RET14.

The independent fields are now the 6 fields (ρ,γ,Uα,Π), and the balance equations are the following:

αVα=0,αTαβ=0,αAβαβ=Iββ. (70)

where the energy-momentum tensor is now given, instead of (22), by

Tαβ=ec2UαUβ+p+Πhαβ. (71)

and, from (35),

Aβαβ=ρc2(θ0,2θ1,2)+A1ΠUα, (72)

where

A1=14c21+3NΔD4c2α1+α2c2β1+β212c2NΠD4=D4443D443+3NΔ349NΔ33D4343D433.

Similarly, from (45), we obtain

Iββ=A1τΠ. (73)

The corresponding Lagrange multiplier to Aβαβ is ψ=14λαα, which is obtained from (68) as follows:

ψ=c2α1β2α2β1c2β1+β2Π. (74)

The system (70) with (71) and (72) is symmetric hyperbolic in the main field (λ,λα,ψ)given respectively by (see (36)1,2 ):

λ=g+c2T+(a1+a2w)Π,λα=1T1+(b1+b2w)ΠUα, (75)

and ψ given by(74).

The closed field equations with the material derivative are obtained as follows:

ρ˙+ραUα=0,e+p+Πc2U˙δ+hδμμ(p+Π)=0,e˙+(e+p+Π)αUα=0,Π˙+ρc2θ0,2θ1,2A1γ˙+A˙1A1Π+ΠαUα=Πτ. (76)

Taking into account

hδμμ(p+Π)=Uδp˙+Π˙c2δ(p+Π), (77)

and from (12):

e˙=c2(ρ˙ω+ρωγ˙),p˙=c2γ2(γρ˙ργ˙), (78)

the system (76) can be put in the normal form:

ρ˙+ραUα=0,ρ+ρε+p+Πc2U˙δδ(p+Π)(p+Π)c211A1ωA1Πρc2+A1γ2+θ0,2θ1,2UδαUα=Πτc2Uδ,ρc2ωγ˙+(p+Π)αUα=0,Π˙+Πp+Πρc2A1ωA1Π+ρc2θ0,2θ1,2αUα=Πτ. (79)

It is extremely interesting that in the relativistic theory the acceleration is influenced by the relaxation time trough the right hand side of (79)2, and this may be important for the application to the problems of cosmology.

7.3. RET5: Euler 5 Fields Theory

Let us consider the principal subsystem with λμν=0. This indicates that any nonequilibrium variables are set to be zero, i.e.,

Π=Δ=0,t<μν>3=0,qα=0. (80)

The independent fields are the 5 fields (n,Uα,γ), and the balance equations are

αVα=0,αTαβ=0, (81)

with

Tαβ=ec2UαUβ+phαβ. (82)

The deduced system is the one of the relativistic Euler theory, and the system (81) becomes symmetric in the main field (λ=(g+c2)/T,λα=Uα/T), as obtained first by Ruggeri and Strumia in [21].

8. Maxwellian Iteration and Phenomenological Coefficients

In order to find the parabolic limit of a system (47) and to obtain the corresponding Eckart equations, we adopt the Maxwellian iteration [31] on (47), in which only the first order terms with respect to the relaxation time are retained. The phenomenological coefficients, that is, the heat conductivity χ, the shear viscosity μ, and the bulk viscosity ν, are identified with the relaxation time.

The method of the Maxwellian iteration is based on putting to zero the nonequilibrium variables on the left side of Equation (47):

ρ˙ρhβαβUα=0,e+pc2hδβU˙βhδμμp=0,e˙(e+p)hαμμUα=0,c23hδβρ˙θ1,2+ρθ1,2γ˙13ρc2θ1,2hδβhαμμUα+2hθ(δhβ)μμUθ==1τ14NΔD4Δc2+NΠD4Πhδβ1τC5t<δβ>3,hβδU˙βρθ0,2c2+23ρc2θ1,2hδμc43μρθ1,2=1τN3D3θ1,32θ1,2qδ,c4ρ˙θ0,2+ρθ0,2γ˙ρc4θ0,2+23θ1,2hαμμUα=14τΔ. (83)

From the first three equations of (83) and taking into account p=ρc2/γ,e=ρc2ω(γ) (see (12)), we can deduce

ρ˙=ρhμαμUα,hδμμρ=ρωγ+1c2hδβUμμUβ+ργhδμμγ,γ˙=1γωhμαμUα. (84)

Putting (84) in the remaining Equation (83)4,5,6, we obtain the solution

qβ=χhβααTTc2UμμUα,Π=ναUα,t<βδ>3=2μhβαhδμ<αUμ>,Δ=σαUα, (85)

with

χ=2ρc23BqT3θ0,2+θ1,2(1ωγ),ν=ρc23B2Π23θ1,2θ1,2γω+3NΔD423θ1,2θ0,2γω,μ=ρc23Btθ1,2, (86)

and

σ=ρB1Δ23θ1,2θ0,2γω,

where B2Π,Bq,Bt are explicitly given by (44) with the relaxation time τ.

As the first three equations in (85) are the Eckart equations, we deduce that χ,ν,μ are the heat conductivity, the bulk viscosity, and the shear viscosity, respectively. In addition, we have a new phenomenological coefficient σ, but as Δ doesn’t appear in either Vα or Tαβ (see Equation (22) or the first three equations in (47)), we arrive at the conclusion that the present theory converges to the Eckart one formed in the first three block equations of (47) with constitutive Equation (85), in which the heat conductivity, bulk viscosity, and shear viscosity are explicitly given by (86)1,2,3.

We introduce, as in [9], the dimensionless variables, as follows:

χ¯=ρTχp2τ=23γ23θ0,2+θ1,2(1ωγ)θ1,3θ1,22N3D3,ν¯=νpτ=13γNΠD423θ1,2θ1,2γω+3NΔD423θ1,2θ0,2γω,μ¯=μpτ=γ3C5θ1,2, (87)

which are functions only of γ.

8.1. Ultra-Relativistic and Classical Limit of the Phenomenological Coefficients

Taking into account Equations (62) and (63), it is simple to obtain the limit of (87) when γ0:

χ¯ultra=0,ν¯ultra=23α24(1+α)(4+α),μ¯ultra=2+α4+α.

In particular, in the most significant case in which a2 for which α=2, we have

χ¯ultra=0,ν¯ultra=0,μ¯ultra=23. (88)

Instead, in the classical limit for which γ, it was proved in [7] that the internal energy ε converges to the classical internal energy of polytropic gas: ε=(D/2)(kB/m)T. Therefore, from (13), ω converges to

ωclass=1+D2γ. (89)

In the present case, using (89), it is not difficult to find θh,j deduced in (17) in the limit γ, as follows:

θ0,0,θ0,1,θ0,2,θ0,3,θ0,4=1,1+D2γ,1+Dγ,1+3D2γ,1+2Dγ,θ1,1,θ1,2,θ1,3,θ1,4=1γ,3γ,6γ,10γ,θ2,3,θ2,4=3γ2,15γ2. (90)

Therefore, in the classical limit, we have

N3D3=2,N31D3=102+D,C5=1,NΠD4=1,NΔD4=2D, (91)

and we find from (87)

χ¯class=D+22,ν¯class=2(D3)3D,μ¯class=1, (92)

which are in perfect agreement with the phenomenological coefficients of the classical RET theory [2].

8.2. Phenomenological Coefficients in RET14 and RET6

By conducting the Maxwellian iteration to RET14 as a principal subsystem of RET15, we may expect that a different bulk viscosity appears. This is because Δ is related to Π by (64), and it affects the balance laws corresponding to Π in RET14. In fact, from (66) and (67), we can obtain the closed field equations for Π, and then, through the Maxwellian iteration, as has been done in [9], we obtain the bulk viscosity for RET14 as follows:

ν¯14=1ωθ0,2+13θ1,289γθ1,21+NΔD4NaDa+NΠD4. (93)

We remark that the heat conductivity and the shear viscosity is the same between RET15 and RET14.

Similarly, from (79)4, we obtain the bulk viscosity estimated by RET6 as follows:

ν¯6=θ0,2θ1,2ωA1. (94)

It should be noted that, in the classical case studied in [15], the bulk viscosities of RET15, RET14, and RET6 are the same. In fact, in the classical limit, ν¯14 and ν¯6 coincide with ν¯class. However, due to the mathematical structure of the relativity (i.e., the scalar fields Π and Δ appear together in the triple tensor), the method of the principal subsystem dictates the difference of the subsystems.

8.3. Heat Conductivity, Bulk Viscosity, and Shear Viscosity in Diatomic Gases

Inserting (60), after cumbersome calculations (easy with Mathematica®), we can obtain the phenomenological coefficients in the diatomic case:

χ¯=γγ2+2γG8γ4G21+2γ2G2+25γ3G16γG+322(γG4)3γγ5+5γ3+48γ+γ46γ212γG2+5γ4+12γ2+96G192,μ¯=γ2+2γG82(γG4)4γ28+γγ2+8G,ν¯=g13(γG4)g2,

with

g1=4γ15GG212+81920γ3G7G2+20196608γ27G2+4+1024γ5G21G4+660G23924096γ435G4+348G256+4γ14G617G4+21G25+γ13G7G686G4+435G2256+4γ1240G6+193G4331G2+48+4γ11G14G6+422G4943G2+500+16γ1077G6660G4+677G284+16γ9G7G6714G4+2560G2110864γ845G6910G4+1472G2204+64γ7GG6+492G42800G2+1760256γ67G6+740G41344G2+192+1835008γG1048576,g2=γ4G21+γ2G2+45γ3G8γG+16)[γ(2γ9G2G21+5γ8G13G2+40γ6G65G2+64γ4G11G225+512γ2GG2+141024γ3G2+5+γ719G417G2+284γ513G4198G2+6032γ3G4+108G252+8192G)8192].

Let us compare the phenomenological coefficients with the ones for the monatomic case obtained in [9]. In Figure 1, we plot the dependence of the dimensionless heat conductivity and shear viscosity on γ for both diatomic and monatomic cases. Concerning ν, we also plot the dimensionless bulk viscosity of RET14 derived in (93) in Figure 2. We observe that in the ultra-relativistic limit and the classical limit, the figures are in perfect agreement with the limits (88) and (92) (for D=3,5). We remark, as is evidently shown in Figure 2, how small the bulk viscosity in monatomic gas is with respect to that of the diatomic case.

Figure 1.

Figure 1

Dependence of χ¯ (left) and μ¯ (right) for diatomic (red solid line) and monatomic (black dashed line) gases on γ. The dotted line indicates the corresponding value in the classical limit. In the ultra-relativistic limit (γ0), χ¯ultra=0,μ¯ultra=2/3 both for monatomic and diatomic gases. In the classical limit (γ), χ¯class=2.5,μ¯class=1 for monatomic gas, and χ¯class=3.5,μ¯class=1 for diatomic gas.

Figure 2.

Figure 2

Dependence of ν¯ for diatomic (red solid line) and monatomic (black dashed line) gases on γ. The prediction by RET14 as a principal subsystem of RET15 is also shown with the dotted line. In the ultra-relativistic limit (γ0), ν¯ultra=0 both for monatomic and diatomic gases. In the classical limit (γ), ν¯class=0 for monatomic gas, and ν¯class=4/15 for diatomic gas.

It is also remarkable that the value of the bulk viscosity of RET6 given by (94) is quite near to the one of RET15. For this reason, we omit the plot of ν¯(6) in the figure. This indicates that RET6 captures the effect of the dynamic pressure in consistency with RET15.

9. Classic Limit of the Relativistic Theory

We want to perform the classical limit γ of the closed relativistic system (47) now. For this purpose, we recall the limits of the coefficients given in (90) and (91). Moreover, taking into account the decomposition UαΓc,vi, where Γ is the Lorentz factor, we have αUα=1ctΓc+kΓvk, whose limit is ivi because tΓ=Γ3vic2tvi has zero limit, and a similar evaluation applies to kΓ. Then,

1c2UμμU0=1c2Γc1ctΓc+1c2ΓvkkΓchas 0 limit,1c2UμμUi=1c2Γc1ctΓvi+1c2ΓvkkΓvihas 0 limit.

Concerning the projection operator in the limit, it is necessary to remember that, with our choice of the metric, vj=vj, then

hβα=gβα+UβUαc2hij=gij+Γ2vivjc2limc+hij=gij=δij,limc+hji=gji=diag(1,1,1).

While from

0=Uαhiα=Γchi0+Γvkhikhi0=vkchik,0=Uαh0α=Γch00+Γvkh0kh00=vkch0k=vavbc2hab.

The last two relations also hold without taking the non-relativistic limit. As a consequence, we have that limc+hi0=0 and limc+h00=0.

The relativistic material derivative (46) of a function f converges to the classical material derivative where we continue to indicate it with a dot. Then, the system (47) becomes in the classical limit:

ρ˙+ρvlxl=0,ρv˙i+pxi+Πxiσikxk=0,T˙+2TDp(p+Π)vlxlσikvkxi+qlxl=0,Π˙+23D3Dpvlxl+5D63DΠvlxl23D3Dσlkvlxk+4(D3)3D(D+2)qlxl=1τΠ,σ˙ij+σijvlxl+2σlivjxl2(p+Π)vjxi4D+2qixj=1τσij,q˙i+D+4D+2qivlxl+D+4D+2qlvixl+2D+2qlvlxi+D+22pρTp+ΠδilσilTxlpρ2Πδilσilρxl+1ρ(pΠ)δil+σilΠxlσrlxr+12DΔxi=1τqi,Δ˙+D+4DΔ+8pρΠvlxl8pρσikvixk8ρqipxi+4(D+4)pρTqlTxl+8pρqlxl8ρqiΠxi+8ρqiσilxl=1τΔ, (95)

where σij=tij. The system (95) coincides perfectly with the classical one obtained recently in [15].

We remark that, as has been studied in [15], for classical polytropic gases, RET14 is derived as a principal subsystem of RET15 by setting Δ=0. Moreover, RET6 is derived from RET14 as a principal subsystem of RET14 by setting σij=0 and qi=0. This corresponds to the fact that, in the classical limit, both Δ(14) defined in (64) and Δ(6) defined in (69) become zero.

Acknowledgments

The work has been partially supported by JSPS KAKENHI, grant numbers JP18K13471 (TA), by the Italian MIUR through the PRIN2017 project “Multiscale phenomena in Continuum Mechanics: singular limits, off-equilibrium and transitions”, project number 2017YBKNCE (SP) and GNFM/INdAM (MCC, SP and TR).

Appendix A. Entropy-Entropy Flux Density

In order to evaluate the entropy density from Equation (20), we need the expression of flnf up to the second order with respect to the nonequilibrium variables. The expansion of the distribution function around an equilibrium state is

f=fEe1kBχ˜=fE11kBχ˜+12kB2χ˜2+χ˜3(),withχ˜=χ˜(1)+χ˜(2)+χ˜(3)(),

defined in (25)2, and the notation η(i) represents the homogeneous part of the generic quantity η at the order i with respect to the nonequilibrium variables. With this notation, the quantities λλE(1), λβλβE(1), λβγ(1) are those of Equation (36).

By composing the above expressions, we see that the distribution function up to the second order is

f=fE11kBχ˜(1)+χ˜(2)+12kB2χ˜(1)2.

and

flnf=f11kBχ˜=fE11kBχ˜(1)+χ˜(2)+12kB2χ˜(1)2+·11kBχE1kBχ˜(1)+χ˜(2)+=fElnfE+1kB2fEχEχ˜(1)+1kB2fEχEχ˜(2)12kBχ˜(1)2++12kB2fEχ˜(1)2.

It follows that

hα=kBcR30+pαflnfφ(I)dIdP=hEα+h(1)α+h(2)α,

where

h(1)α=ckBR30+pαfEχEχ˜(1)φ(I)dIdP==ckBR30+pαfEmλE+1+Imc2UμTpμχ˜(1)φ(I)dIdP,
h(2)α=ckBR30+pαfEχEχ˜(2)12kBχ˜(1)2φ(I)dIdPc2kBR30+pαfEχ˜(1)2φ(I)dIdP.

Moreover, we have that the moments appearing in system (18) up to the second order are as follows:

Vα=VEα_mckBR30+pαfEχ˜(1)_+χ˜(2)12kBχ˜(1)2φ(I)dIdP,Tαβ=TEαβ_ckBR30+pαpβ1+Imc2fEχ˜(1)_+χ˜(2)12kBχ˜(1)2φ(I)dIdP,UαUβUγc4Aαβγ=UαUβUγc4AEαβγ_UαUβUγc4cmkBR30+pαpβpγ1+Imc22fEχ˜(1)_+χ˜(2)12kBχ˜(1)2φ(I)dIdP.

The underlined terms give 0 for Equation (36), and there remain

mckBR30+pαfEχ˜(2)12kBχ˜(1)2φ(I)dIdP=0,ckBR30+pαpβ1+Imc2fEχ˜(2)12kBχ˜(1)2φ(I)dIdP=0,UαUβUγc4cmkBR30+pαpβpγ1+Imc22fEχ˜(2)12kBχ˜(1)2φ(I)dIdP=0.

The first two of these allow one to prove Equation (52)1 and to write

h(2)α=c2kBR30+pαfEχ˜(1)2φ(I)dIdP.

It is sufficient to substitute the expression of χ˜ to obtain Equation (52)2.

Appendix B. Continuity of the Ultra Relativistic Limit for a=2

From (12)2, and by using the recurrence relations (11) and (10), we have

γenmc2=γ0+J2,2*1+Imc2ϕ(I)dI0+J2,1*ϕ(I)dI=3+0+J0,1*ϕ(I)dI0+J2,1*ϕ(I)dI.

By introducing the Ruggeri’s numbers Rk and using Equations (32)1 of [30], we have

γenmc2=3+3lnγR4=31lnγ

or

e=nmc2γ31lnγ. (A1)

Therefore, we have to calculate D4, NΠ and NΔ with (A1) instead of (61).

In particular, for D4 we can add to its fourth line the second one pre-multiplied by 13, so that it becomes

1γlnγ13,43γ,203γ2,43c2γ2.

It follows that, afte r cumbersome calculations that we do not report here for brevity, we have

limγ0γ9lnγD4=1312431260201260360120134320343=64.

Similarly, for NΠ we can add to its fourth line the third one multiplied by 13, so that it becomes

1γ2lnγ43,203γ,40γ2,8c2γ2.

It follows that

limγ0γ10lnγNΠ=131243126020126036012043203408=384.

Finally, for NΔ we can add to its third line the second one multiplied by 13, so that its third line becomes

1γlnγ13,43γ,203γ2,43c2γ2.

It follows that

limγ0γ9lnγNΔ=13124312602013432034342012040=643.

By joining all these results we obtain

limγ0γNΠD4=6,limγ0NΔD4=13,

which confirms (63) also for a=2.

Author Contributions

T.A., M.C.C., S.P. and T.R. were fully involved in: substantial conception and design of the paper; drafting the article and revising it critically for important intellectual content; final approval of the version to be published. All authors have read and agreed to the published version of the manuscript.

Funding

This work was funded by JSPS KAKENHI, grant numbers JP18K13471, PRIN2017, project number 2017YBKNCE.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Conflicts of Interest

The authors declare no conflict of interest.

Footnotes

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