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institutetext: Department of Physics & Astronomy, University of Victoria,
PO Box 1700 STN CSC, Victoria, BC, V8W 2Y2, Canada

Causal first-order hydrodynamics from kinetic theory and holography

Raphael E. Hoult and Pavel Kovtun
Abstract

We show how causal relativistic Navier-Stokes equations arise from the relativistic Boltzmann equation: the causality is preserved via a judicious choice of the zero modes of the collision operator. A completely analogous procedure may be used to extract causal hydrodynamics from the fluid-gravity correspondence: again, causality of the hydrodynamic equations is preserved by a suitable choice of zero modes of the corresponding differential operators in the bulk. We give examples of zero modes which give rise to causal hydrodynamic equations for non-conformal fluids with a conserved U(1) global symmetry current.

1 Introduction

Relativistic viscous hydrodynamics is by now over eighty years old, starting with the classic works by Eckart PhysRev.58.919 in 1940, and by Landau and Lifshitz in the second edition of their book LL6 in 1953. Following the treatment of non-relativistic fluids, the classic theories of relativistic hydrodynamics introduced dissipative effects via terms which have derivatives of the standard hydrodynamic variables: fluid velocity uαu^{\alpha}, temperature TT, and the chemical potential μ\mu. Schematically, the energy-momentum tensor TαβT^{\alpha\beta} and the particle number current JαJ^{\alpha} of the classic theories take the form of the following constitutive relations:

Tαβ,Jα=O(T,u,μ)+O(T,u,μ),\displaystyle T^{\alpha\beta},J^{\alpha}=O(T,u,\mu)+O(\partial T,\partial u,\partial\mu)\,, (1)

where the first term in the right-hand side corresponds to perfect fluids, and the second term encodes dissipative corrections due to viscosity and heat conductivity. The hydrodynamic equations are the conservation laws

αTαβ=0,αJα=0,\displaystyle\partial_{\alpha}T^{\alpha\beta}=0\,,\ \ \ \ \partial_{\alpha}J^{\alpha}=0\,, (2)

which give partial differential equations for TT, uu, and μ\mu. The classic theories are often called “first-order” theories, because the above TαβT^{\alpha\beta} and JαJ^{\alpha} contain only up to one derivative of the hydrodynamic variables. It was understood soon after that the classic hydrodynamic theories suffer from violations of causality. From a mathematical point of view, the hydrodynamic equations of the classic theories are not hyperbolic. Related to that, the classic theories predict that the uniform equilibrium state of a non-gravitating fluid in flat space is unstable. See Refs. Hiscock:1985zz and Hiscock:1987zz for an extensive discussion of instability and acausality in the classic theories.

The most popular proposal to remedy the violations of causality in the classic formulations are the Müller-Israel-Stewart (MIS) theories Muller:1967 ; Israel:1976tn ; Israel-Stewart . Schematically, MIS theories introduce extra tensor variables collectively denoted by Π\Pi, and posit that

Tαβ,Jα=O(T,u,μ)+Π,\displaystyle T^{\alpha\beta},J^{\alpha}=O(T,u,\mu)+\Pi\,, (3)
τuλλΠ=O(Π,T,u,μ),\displaystyle\tau\,u^{\lambda}\partial_{\lambda}\Pi=O(\Pi,\partial T,\partial u,\partial\mu)\,, (4)

where τ\tau denote phenomenological “relaxation times” introduced in the MIS theory. The terms O(T,u,μ)O(\partial T,\partial u,\partial\mu) in the right-hand side of (4) are inherited from the classic first-order theories. Combined with the standard conservation laws αTαβ=0\partial_{\alpha}T^{\alpha\beta}=0 and αJα=0\partial_{\alpha}J^{\alpha}=0, one finds partial differential equations for Π\Pi, uu, TT, and μ\mu. The MIS equations are hyperbolic provided the parameters and the variables of the theory satisfy certain constraints, though demonstrating hyperbolicity in the full non-linear theory is tricky, and was only accomplished recently Bemfica:2020xym .

The introduction of numerous extra variables Π\Pi in the MIS theory seems like a drastic modification of the classic hydrodynamic formulation (1), and it is. Moreover, there is no need to introduce extra variables Π\Pi to maintain causality: the classic theories can be made consistent with causality with only minimal modification, keeping the first-order structure (1) intact. The reason is that the classic theories PhysRev.58.919 ; LL6 do not include all possible one-derivative terms in the right-hand side of the constitutive relations (1). The choice of which one-derivative terms are included in eq. (1) can be traced to the convention for the out-of-equilibrium definitions of TT, uαu^{\alpha}, and μ\mu. This convention is often called a choice of “frame”, thus one speaks of “Eckart frame”, “Landau-Lifshitz frame”, etc. One can consider a most general “frame”, which in practice amounts to including all possible one-derivative terms in the right-hand side of eq. (1). One can choose “frames” in which the hydrodynamic equations (2) are hyperbolic, the equilibrium state is stable, and the entropy production is positive within the domain of validity of the derivative expansion. Such “good frames” are the essence of the BDNK approach Bemfica:2017wps ; Kovtun:2019hdm ; Bemfica:2019knx ; Hoult:2020eho ; Bemfica:2020zjp . Formally, such theories are first-order theories because the constitutive relations still have the form (1). Thus, if one’s goal is to have a minimal causal theory of relativistic hydrodynamics, the MIS theory is overkill, and the more conservative first-order BDNK formulation is sufficient. It is straightforward to combine the two approaches by including all possible O(T,u,μ)O(\partial T,\partial u,\partial\mu) terms in the right-hand side of eq. (4), see Noronha:2021syv . For a numerical exploration of causal first-order hydrodynamics see Pandya:2021ief .

The purpose of this paper is to show how the equations of causal first-order hydrodynamics arise from relativistic kinetic theory. Kinetic theory is not required for hydrodynamics: a fluid can happily flow and obey hydrodynamic constitutive relations on macroscopic distance and time scales even if the fluid is not composed of quasi-particles. Perhaps the most extreme examples come from fluids comprised of strongly interacting quantum fields in non-abelian gauge theories, found in the holographic correspondence Aharony:1999ti . Their hydrodynamic flows have been studied extensively, see e.g. Chesler:2013lia . In these examples, strong quantum fluctuations completely wash out the very notion of a quasi-particle, rendering kinetic theory inapplicable. On the other hand, for those fluids which are comprised of well-defined quasi-particles, the Boltzmann equation provides a useful simple model of macroscopic dynamics.

The derivation of first-order causal hydrodynamics from kinetic theory has been addressed previously in refs. Bemfica:2017wps ; Bemfica:2019knx . Our treatment here differs in several respects. We do not ignore the conserved particle number current, and we do not impose any “matching conditions” on the higher moments of the distribution function. We show how first-order causal hydrodynamics arises from the simplest derivative expansion (the Hilbert expansion) of the solutions to the Boltzmann equation, and that “good frames” arise simply as a “good” choice of the free functions which parametrize the zero modes of the linearized collision operator in real space.

The method by which hydrodynamics is extracted from classical gravity in asymptotically anti-de Sitter spacetimes via the fluid/gravity correspondence Bhattacharyya:2008jc is analogous in many ways to the Hilbert expansion in kinetic theory. The methods used to extract causal hydrodynamics from kinetic theory apply equally well to holography, allowing the construction of causal hydrodynamic theories with holographic duals.

The structure of the paper is as follows. In section 2, we show how causal first-order hydrodynamics arises from the Hilbert expansion in relativistic kinetic theory. In section 3, we show how an analogous procedure leads to causal hydrodynamics via the fluid/gravity correspondence. In appendices A and B we discuss examples of causal hydrodynamic frames, illustrating a causal choice of the zero modes. Finally, in appendix C, we comment on the “matching conditions” on the higher moments of the distribution function.

2 Boltzmann equation

Relativistic kinetic theory is an established subject deGroot ; Cercignani-Kremer . The fundamental object of the theory is the one-particle distribution function f(x,p)f(x,p), where both the particle’s location xx and momentum pp are four-vectors. The particles are on-shell, with p0(𝐩2+m2)1/2p^{0}\equiv({\bf p}^{2}+m^{2})^{1/2}. The distribution function counts the particles, and is normalized so that the number density is

n(x)=d3p(2π)3f(x,p).\displaystyle n(x)=\int\!\!\frac{d^{3}p}{(2\pi)^{3}}\;f(x,p)\,. (5)

The particle number current is the covariant version of the above:

Jμ=ppμf(x,p),\displaystyle J^{\mu}=\int_{p}p^{\mu}f(x,p)\,, (6)

where pd3p/[(2π)3p0]\int_{p}\dots\equiv\int d^{3}p/[(2\pi)^{3}p^{0}]\dots denotes the Lorentz-invariant integration measure. Similarly, the energy-momentum tensor is

Tμν=ppμpνf(x,p).\displaystyle T^{\mu\nu}=\int_{p}p^{\mu}p^{\nu}f(x,p)\,. (7)

Conservation laws

The Boltzmann equation is the evolution equation for the distribution function,

pμμf(x,p)=𝒞[f],\displaystyle p^{\mu}\partial_{\mu}f(x,p)={\cal C}[f]\,, (8)

where the right-hand side is the collision term which is an integral operator (in momentum) that acts on fpf(x,p)f_{p}\equiv f(x,p), and is at least quadratic in ff. The details of 𝒞{\cal C} depend on the interactions and on the statistics of the particles, and we will assume that the inter-particle interactions conserve energy, momentum, and particle number. A simple form to keep in mind is 2-to-2 elastic collisions111Upper sign is for bosons, lower is for fermions.

𝒞[f]=12p1,p2,p3W(p,p1|p2,p3)[fp2fp3(1±fp)(1±fp1)fpfp1(1±fp2)(1±fp3)].\displaystyle{\cal C}[f]={\textstyle{\frac{1}{2}}}\int_{p_{1},p_{2},p_{3}}W(p,p_{1}|p_{2},p_{3})\left[f_{p_{2}}f_{p_{3}}(1\pm f_{p})(1\pm f_{p_{1}})-f_{p}f_{p_{1}}(1\pm f_{p_{2}})(1\pm f_{p_{3}})\right]\,. (9)

The transition rates obey W(p,p1|p2,p3)=W(p2,p3|p,p1)=W(p1,p|p2,p3)=W(p,p1|p3,p2)W(p,p_{1}|p_{2},p_{3})=W(p_{2},p_{3}|p,p_{1})=W(p_{1},p|p_{2},p_{3})=W(p,p_{1}|p_{3},p_{2}), and are proportional to δ(p+p1p2p3)\delta(p+p_{1}-p_{2}-p_{3}). It then follows that

p[a(x)+bμ(x)pμ]𝒞[fp]=0,\displaystyle\int_{p}[a(x)+b_{\mu}(x)p^{\mu}]\,{\cal C}[f_{p}]=0\,, (10)

with arbitrary functions a(x)a(x), bμ(x)b_{\mu}(x). In particular, p𝒞[fp]=0\int_{p}{\cal C}[f_{p}]=0 and ppμ𝒞[fp]=0\int_{p}p^{\mu}{\cal C}[f_{p}]=0. Together with the Boltzmann equation (8), these immediately imply

μJμ=0,μTμν=0.\displaystyle\partial_{\mu}J^{\mu}=0\,,\ \ \ \ \partial_{\mu}T^{\mu\nu}=0\,. (11)

Alternatively, the conservation laws (11) can be viewed as the zeroth and first “moments” of the Boltzmann equation, i.e. they follow by applying p\int_{p}\dots and ppν\int_{p}p^{\nu}\dots to eq. (8), and are true for any f(x,p)f(x,p). The property (10) of the collision operator is a manifestation of the conservation of energy, momentum, and particle number. Approximate forms of the collision operator which violate eq. (10) (such as the relaxation-time approximation) are in general inconsistent with the conservation laws (11) which form the basis of hydrodynamics.222 A way to fix the relativistic relaxation-time approximation was discussed recently in ref. Rocha:2021zcw .

Equilibrium

Consider distribution functions of the form

𝐟(x,p)=[e𝜷μ(x)pμ𝜶(x)1]1,\displaystyle{\bf f}(x,p)=[e^{-{\bm{\beta}}_{\mu}(x)p^{\mu}-{\bm{\alpha}}(x)}\mp 1]^{-1}\,, (12)

with arbitrary 𝜷μ(x){\bm{\beta}}_{\mu}(x), 𝜶(x){\bm{\alpha}}(x). These are local Bose/Fermi distributions for a fluid at temperature 𝑻=1/𝜷2{\bm{T}}=1/\sqrt{-{\bm{\beta}}^{2}}, with velocity 𝒖α=𝜷α/𝜷2{\bm{u}}^{\alpha}={\bm{\beta}}^{\alpha}/\sqrt{-{\bm{\beta}}^{2}}, and chemical potential 𝝁=𝜶/𝜷2{\bm{\mu}}={\bm{\alpha}}/\sqrt{-{\bm{\beta}}^{2}}. The collision integral is such that it satisfies 𝒞[𝐟]=0{\cal C}[{\bf f}]=0. If we want the function (12) to actually solve the Boltzmann equation, we need pμpνμ𝜷ν+pμμ𝜶=0p^{\mu}p^{\nu}\partial_{\mu}{\bm{\beta}}_{\nu}+p^{\mu}\partial_{\mu}{\bm{\alpha}}=0, hence the functions 𝜷μ(x){\bm{\beta}}_{\mu}(x) and 𝜶(x){\bm{\alpha}}(x) must satisfy

μ𝜷ν(x)+ν𝜷μ(x)=0,μ𝜶(x)=0.\displaystyle\partial_{\mu}{\bm{\beta}}_{\nu}(x)+\partial_{\nu}{\bm{\beta}}_{\mu}(x)=0\,,\ \ \ \ \partial_{\mu}{\bm{\alpha}}(x)=0\,. (13)

Generalized to curved space, the first equation would say that 𝜷μ{\bm{\beta}}_{\mu} is a Killing vector.

Derivative expansion in hydrodynamics

Let us forget about kinetic theory for a moment, and consider hydrodynamics per se, with the constitutive relations written in the derivative expansion:

Tμν=T0μν[β]+γT1μν[β]+γ2T2μν[β]+,\displaystyle T^{\mu\nu}=T^{\mu\nu}_{0}[\beta]+\gamma T^{\mu\nu}_{1}[\beta]+\gamma^{2}T^{\mu\nu}_{2}[\beta]+\dots\,, (14)

where γ\gamma is a formal derivative-counting parameter, and βμ=uμ/T\beta^{\mu}=u^{\mu}/T are hydrodynamic variables: TT is the temperature, and uμu^{\mu} is the fluid velocity. Truncating the above expansion at O(γn)O(\gamma^{n}) gives nn-th order hydrodynamics: T0μν=O(β)T^{\mu\nu}_{0}=O(\beta) is the perfect fluid, T1μν=O(β)T^{\mu\nu}_{1}=O(\partial\beta) contains the viscosity, T2μν=O(2β,(β)2)T^{\mu\nu}_{2}=O(\partial^{2}\beta,(\partial\beta)^{2}) etc. Let us look for the solutions using the same derivative expansion:

βμ(x)=β0μ(x)+γβ1μ(x)+γ2β2μ(x)+.\displaystyle\beta^{\mu}(x)=\beta^{\mu}_{0}(x)+\gamma\beta^{\mu}_{1}(x)+\gamma^{2}\beta^{\mu}_{2}(x)+\dots\,. (15)

We expect βn+1=O(βn)\beta_{n+1}=O(\partial\beta_{n}). Expanding the constitutive relations, we have

Tnμν[β]=Tnμν[β0]+γTn,1μν[β0,β1]+γ2Tn,2μν[β0,β1,β2]+.\displaystyle T^{\mu\nu}_{n}[\beta]=T^{\mu\nu}_{n}[\beta_{0}]+\gamma\,T^{\mu\nu}_{n,1}[\beta_{0},\beta_{1}]+\gamma^{2}\,T^{\mu\nu}_{n,2}[\beta_{0},\beta_{1},\beta_{2}]+\dots\,. (16)

The hydrodynamic variables β\beta are determined by solving μTμν[β]=0\partial_{\mu}T^{\mu\nu}[\beta]=0, order by order in γ\gamma. At the leading order, the variables β0\beta_{0} are determined by the perfect-fluid hydrodynamics:

μT0μν[β0]=0.\displaystyle\partial_{\mu}T^{\mu\nu}_{0}[\beta_{0}]=0\,. (17)

The first correction β1\beta_{1} is then determined by

μ(T0,1μν[β0,β1]+T1μν[β0])=0.\displaystyle\partial_{\mu}\left(T^{\mu\nu}_{0,1}[\beta_{0},\beta_{1}]+T^{\mu\nu}_{1}[\beta_{0}]\right)=0\,. (18)

At the next order,

μ(T0,2μν[β0,β1,β2]+T1,1μν[β0,β1]+T2μν[β0])=0,\displaystyle\partial_{\mu}\left(T^{\mu\nu}_{0,2}[\beta_{0},\beta_{1},\beta_{2}]+T^{\mu\nu}_{1,1}[\beta_{0},\beta_{1}]+T^{\mu\nu}_{2}[\beta_{0}]\right)=0\,, (19)

determines the correction β2\beta_{2}, and the chain continues. The expansion (17), (18), (19) etc. naturally arises from the derivative expansion in both kinetic theory, and in the fluid-gravity duality. Note, however, that this is not how the hydrodynamic equations are normally solved for hydrodynamic variables. In practice, the hydrodynamic constitutive relations are given to the desired order in γ\gamma, and then the conservation equations are solved “all at once” for βμ\beta^{\mu}, as opposed to finding the order-by-order contributions β0,β1\beta_{0},\beta_{1}, etc. Such a procedure may lead to solutions which violate the small-derivative assumption of the expansion. The breakdown of the derivative expansion is a separate subject which we will not explore here.

Derivative expansion for the Boltzmann equation

The distribution function (12) with arbitrary non-constant 𝜷μ(x){\bm{\beta}}_{\mu}(x) and 𝜶(x){\bm{\alpha}}(x) does not satisfy the Boltzmann equation. Approximate solutions to the Boltzmann equation may be constructed in the derivative expansion. To do so, we write the Boltzmann equation as

εpμμf(x,p)=𝒞[f],\displaystyle\varepsilon\,p^{\mu}\partial_{\mu}f(x,p)={\cal C}[f]\,, (20)

with an auxiliary parameter ε\varepsilon (to be set to one at the end), and aim to find the solution as a power series in ε\varepsilon:

f(x,p)=𝐟(x,p)+εf(1)(x,p)+ε2f(2)(x,p)+.\displaystyle f(x,p)={\bf f}(x,p)+\varepsilon f^{(1)}(x,p)+\varepsilon^{2}f^{(2)}(x,p)+\dots\,. (21)

This is sometimes called the Hilbert expansion Cercignani-Kremer . The energy-momentum tensor (7) and the current (6) then take the form

Tμν=T(0)μν+εT(1)μν+ε2T(2)μν+,\displaystyle T^{\mu\nu}=T^{\mu\nu}_{(0)}+\varepsilon T^{\mu\nu}_{(1)}+\varepsilon^{2}T^{\mu\nu}_{(2)}+\dots\,, (22)
Jμ=J(0)μ+εJ(1)μ+ε2J(2)μ+.\displaystyle J^{\mu}=J^{\mu}_{(0)}+\varepsilon J^{\mu}_{(1)}+\varepsilon^{2}J^{\mu}_{(2)}+\dots\,. (23)

These expansions for TμνT^{\mu\nu} and JμJ^{\mu} are however not necessarily the derivative expansions of the hydrodynamic constitutive relations. In order to talk about the constitutive relations, we need the hydrodynamic variables TT, uλu^{\lambda}, and μ\mu, or equivalently βλ=uλ/T\beta^{\lambda}=u^{\lambda}/T and α=μ/T\alpha=\mu/T. In kinetic theory, the hydrodynamic variables arise as arbitrary functions of xx (or “integration constants” in momentum space) in the solutions of the Boltzmann equation. The xx-dependence of these functions is then fixed by the consistency conditions for the Boltzmann equation at each order in the expansion. These consistency conditions are exactly the hydrodynamic conservation laws. Each order in the ε\varepsilon-expansion generates its own arbitrary functions, namely

βμ(x)=β(0)μ(x)+εβ(1)μ(x)+ε2β(2)μ(x)+,\displaystyle\beta^{\mu}(x)=\beta^{\mu}_{(0)}(x)+\varepsilon\beta^{\mu}_{(1)}(x)+\varepsilon^{2}\beta^{\mu}_{(2)}(x)+\dots\,, (24)
α(x)=α(0)(x)+εα(1)(x)+ε2α(2)(x)+,\displaystyle\alpha(x)=\alpha_{(0)}(x)+\varepsilon\alpha_{(1)}(x)+\varepsilon^{2}\alpha_{(2)}(x)+\dots\,, (25)

where the leading-order hydrodynamic variables β(0)μ=𝜷μ\beta^{\mu}_{(0)}={\bm{\beta}}^{\mu} and α(0)=𝜶\alpha_{(0)}={\bm{\alpha}} are the free functions that appear in the equilibrium distribution (12), and the corrections β(n)μ\beta^{\mu}_{(n)} and α(n)\alpha_{(n)} appear as undetermined functions in the solution for f(n)(x,p)f^{(n)}(x,p). Connecting to the earlier discussion of the derivative expansion in hydrodynamics, we expect to find in the Hilbert expansion

T(0)μν=T0μν[β(0),α(0)],\displaystyle T^{\mu\nu}_{(0)}=T^{\mu\nu}_{0}[\beta_{(0)},\alpha_{(0)}]\,, (26a)
T(1)μν=T0,1μν[β(0),α(0),β(1),α(1)]+T1μν[β(0),α(0)],\displaystyle T^{\mu\nu}_{(1)}=T^{\mu\nu}_{0,1}[\beta_{(0)},\alpha_{(0)},\beta_{(1)},\alpha_{(1)}]+T^{\mu\nu}_{1}[\beta_{(0)},\alpha_{(0)}]\,, (26b)
T(2)μν=T0,2μν[β(0),α(0),β(1),α(1),β(2),α(2)]+T1,1μν[β(0),α(0),β(1),α(1)]+T2μν[β(2),α(2)],\displaystyle T^{\mu\nu}_{(2)}=T^{\mu\nu}_{0,2}[\beta_{(0)},\alpha_{(0)},\beta_{(1)},\alpha_{(1)},\beta_{(2)},\alpha_{(2)}]+T^{\mu\nu}_{1,1}[\beta_{(0)},\alpha_{(0)},\beta_{(1)},\alpha_{(1)}]+T^{\mu\nu}_{2}[\beta_{(2)},\alpha_{(2)}]\,, (26c)

etc., with analogous expressions for the current JμJ^{\mu}. We expect the conservation equations to hold at each order in the expansion,

μT(n)μν=0,μJ(n)μ=0,\displaystyle\partial_{\mu}T^{\mu\nu}_{(n)}=0,\ \ \ \ \partial_{\mu}J^{\mu}_{(n)}=0\,, (27)

This is indeed what happens.

First order: The equation

At first order in the expansion we have

εpμμ𝐟(x,p)=𝒞[𝐟+εf(1)].\displaystyle\varepsilon\,p^{\mu}\partial_{\mu}{\bf f}(x,p)={\cal C}[{\bf f}+\varepsilon\,f^{(1)}]\,. (28)

We expand the collision operator to linear order in ε\varepsilon. Denoting ϕp(x)f(1)/𝐟(1±𝐟)\phi_{p}(x)\equiv f^{(1)}/{\bf f}(1\pm{\bf f}), the Boltzmann equation (28) becomes

pμμ𝐟=𝐟[ϕ],\displaystyle p^{\mu}\partial_{\mu}{\bf f}={\bf f}\,{\cal L}[\phi]\,, (29)

where {\cal L} is the linearized collision operator. Its explicit form depends on the details of the full collision operator 𝒞{\cal C}, and in general one has

[a(x)+bμ(x)pμ]=0,\displaystyle{\cal L}[a(x)+b_{\mu}(x)p^{\mu}]=0\,, (30)

with arbitrary a(x)a(x), bμ(x)b_{\mu}(x). The existence of these zero modes is a consequence of 𝒞[𝐟]=0{\cal C}[{\bf f}]=0, reflecting the microscopic conservation laws of energy, momentum, and particle number. For 2-to-2 elastic collisions (9), the explicit form is

[ϕ]=12p1,p2,p3W(p,p1|p2,p3)𝐟p1(1±𝐟p2)(1±𝐟p3)(ϕp2+ϕp3ϕpϕp1).\displaystyle{\cal L}[\phi]={\textstyle{\frac{1}{2}}}\int_{p_{1},p_{2},p_{3}}W(p,p_{1}|p_{2},p_{3}){\bf f}_{p_{1}}(1\pm{\bf f}_{p_{2}})(1\pm{\bf f}_{p_{3}})\left(\phi_{p_{2}}+\phi_{p_{3}}-\phi_{p}-\phi_{p_{1}}\right)\,. (31)

First order: The constraint

Given two functions gpg(x,p)g_{p}\equiv g(x,p), hph(x,p)h_{p}\equiv h(x,p), the linearized collision operator satisfies

p𝐟pgp[h]=p𝐟php[g].\displaystyle\int_{p}{\bf f}_{p}\,g_{p}\,{\cal L}[h]=\int_{p}{\bf f}_{p}\,h_{p}\,{\cal L}[g]\,. (32)

If we take hp=a(x)+bμ(x)pμh_{p}=a(x)+b_{\mu}(x)p^{\mu} with arbitrary a(x)a(x), bμ(x)b_{\mu}(x), take gp=ϕpg_{p}=\phi_{p}, and use the linearized Boltzmann equation (29), we immediately find

0=a(x)μ𝐉μ+bμ(x)λ𝐓λμ.\displaystyle 0=a(x)\,\partial_{\mu}{\bf J}^{\mu}+b_{\mu}(x)\,\partial_{\lambda}{\bf T}^{\lambda\mu}\,. (33)

In other words, at first order in the ε\varepsilon-expansion, the functions 𝜷μ(x){\bm{\beta}}_{\mu}(x) and 𝜶(x){\bm{\alpha}}(x) that appear in the local-equilibrium distribution function (12) must obey

μ𝐉μ=0,μ𝐓μν=0.\displaystyle\partial_{\mu}{\bf J}^{\mu}=0\,,\ \ \ \ \partial_{\mu}{\bf T}^{\mu\nu}=0\,. (34)

These are the perfect-fluid conservation equations. The above 𝐓μν{\bf T}^{\mu\nu} and 𝐉μ{\bf J}^{\mu} can be written as

𝐓μν=ϵ𝒖μ𝒖ν+𝒑𝚫μν,𝐉μ=𝒏𝒖μ,\displaystyle{\bf T}^{\mu\nu}={\bm{\epsilon}}{\bm{u}}^{\mu}{\bm{u}}^{\nu}+{\bm{p}}{\bm{\Delta}}^{\mu\nu}\,,\ \ \ \ {\bf J}^{\mu}={\bm{n}}{\bm{u}}^{\mu}\,, (35)

where 𝚫μνgμν+𝒖μ𝒖ν{\bm{\Delta}}^{\mu\nu}\equiv g^{\mu\nu}+{\bm{u}}^{\mu}{\bm{u}}^{\nu}, and the coefficients are

𝒏(𝑻,𝜶)=𝑻𝜷μppμ𝐟p,\displaystyle{\bm{n}}({\bm{T}},{\bm{\alpha}})=-{\bm{T}}{\bm{\beta}}_{\mu}\int_{p}p^{\mu}\,{\bf f}_{p}\,, (36)
ϵ(𝑻,𝜶)=𝑻2𝜷μ𝜷νppμpν𝐟p,\displaystyle{\bm{\epsilon}}({\bm{T}},{\bm{\alpha}})={\bm{T}}^{2}{\bm{\beta}}_{\mu}{\bm{\beta}}_{\nu}\int_{p}p^{\mu}p^{\nu}\,{\bf f}_{p}\,, (37)
𝒑(𝑻,𝜶)=13𝚫μνppμpν𝐟p,\displaystyle{\bm{p}}({\bm{T}},{\bm{\alpha}})={\textstyle{\frac{1}{3}}}{\bm{\Delta}}_{\mu\nu}\int_{p}p^{\mu}p^{\nu}\,{\bf f}_{p}\,, (38)

corresponding to the ideal-gas particle number density, energy density, and pressure. In the notation of eq. (26a), 𝐓μν=T0μν{\bf T}^{\mu\nu}=T^{\mu\nu}_{0}, 𝐉μ=J0μ{\bf J}^{\mu}=J^{\mu}_{0}. The conservation equations (34) are

nu+(n/T)T˙+(n/α)α˙=0,\displaystyle n\,\partial{\cdot}u+(\partial n/\partial T)\dot{T}+(\partial n/\partial\alpha)\dot{\alpha}=0\,, (39a)
(ϵ/T)T˙+(ϵ/α)α˙+(ϵ+p)u=0,\displaystyle(\partial\epsilon/\partial T)\dot{T}+(\partial\epsilon/\partial\alpha)\dot{\alpha}+(\epsilon{+}p)\partial{\cdot}u=0\,, (39b)
(ϵ+p)u˙μ+(p/T)μT+(p/α)μα=0,\displaystyle(\epsilon{+}p)\dot{u}_{\mu}+(\partial p/\partial T)\partial_{\mu}^{\perp}T+(\partial p/\partial\alpha)\partial_{\mu}^{\perp}\alpha=0\,, (39c)

where all quantities are of order O(ε0)O(\varepsilon^{0}). The dot stands for uλλu^{\lambda}\partial_{\lambda}, and μΔμνν\partial_{\mu}^{\perp}\equiv\Delta_{\mu\nu}\partial^{\nu}. The vector conservation equation can be rewritten as u˙μ+μT/T+nTϵ+pμα=0\dot{u}_{\mu}+\partial_{\mu}^{\perp}T/T+\frac{nT}{\epsilon+p}\partial_{\mu}^{\perp}\alpha=0.

Another way to arrive at eqs. (34) is to note that in the Boltzmann equation (29) the linearized collision operator {\cal L} has zero modes, and therefore is not invertible. In general, the linear equation H=[ϕ]H={\cal L}[\phi] can only be solved for ϕ\phi if the left-hand side HH is orthogonal to the zero-modes of the operator {\cal L} in the right-hand side. For the linearized Boltzmann equation, the zero-modes are 1 and pλp^{\lambda}, and the consistency conditions amount to

p𝐟pH=0,p𝐟pHpλ=0,\displaystyle\int_{p}{\bf f}_{p}\,H=0\,,\ \ \ \ \int_{p}{\bf f}_{p}\,H\,p^{\lambda}=0\,, (40)

with H=pμμ𝐟p/𝐟pH=p^{\mu}\partial_{\mu}{\bf f}_{p}/{\bf f}_{p}. This again gives eq. (34). In other words, the equations of 0th0^{\rm th}-order (perfect-fluid) hydrodynamics arise as constraint equations at 1st1^{\rm st}-order in the expansion.

First order: Homogeneous solution

At the first order in the expansion we have to solve eq. (29) which we write as H=[ϕ]H={\cal L}[\phi], with H=pμμ𝐟p/𝐟pH=p^{\mu}\partial_{\mu}{\bf f}_{p}/{\bf f}_{p}. The solution can be written as ϕp(x)=a(x)+bμ(x)pμ+Φ(x,p)\phi_{p}(x)=a(x)+b_{\mu}(x)p^{\mu}+\Phi(x,p) where a(x)a(x) and bμ(x)b_{\mu}(x) are arbitrary, and the inhomogeneous solution Φ\Phi satisfies Φ|H0=0\Phi|_{H\to 0}=0. Remembering the definition ϕp=f(1)/𝐟(1±𝐟)\phi_{p}=f^{(1)}/{\bf f}(1\pm{\bf f}), the distribution function to first order in ε\varepsilon is

fp=𝐟p+𝐟p(1±𝐟p)(εa+εbμpμ)+𝐟p(1±𝐟p)εΦ+O(ε2).\displaystyle f_{p}={\bf f}_{p}+{\bf f}_{p}(1\pm{\bf f}_{p})\left(\varepsilon a+\varepsilon b_{\mu}p^{\mu}\right)+{\bf f}_{p}(1\pm{\bf f}_{p})\varepsilon\Phi+O(\varepsilon^{2})\,. (41)

From here, it is clear that the functions bμ(x)b_{\mu}(x) and a(x)a(x) can be understood as O(ε)O(\varepsilon) redefinitions of the functions βμ(x)\beta_{\mu}(x) and α(x)\alpha(x) which sit in 𝐟p{\bf f}_{p}. Indeed, for βμ(x)=βμ(0)(x)+εβμ(1)(x)\beta_{\mu}(x)=\beta_{\mu}^{(0)}(x)+\varepsilon\beta_{\mu}^{(1)}(x), α(x)=α(0)(x)+εα(1)(x)\alpha(x)=\alpha^{(0)}(x)+\varepsilon\alpha^{(1)}(x) we have in terms of 𝐟p(0)𝐟p(β(0),α(0)){\bf f}_{p}^{(0)}\equiv{\bf f}_{p}(\beta^{(0)},\alpha^{(0)}):

𝐟p(β,α)=𝐟p(0)+𝐟p(0)(1±𝐟p(0))(εα(1)+εβμ(1)pμ)+O(ε2).\displaystyle{\bf f}_{p}(\beta,\alpha)={\bf f}_{p}^{(0)}+{\bf f}_{p}^{(0)}(1\pm{\bf f}_{p}^{(0)})\left(\varepsilon\alpha^{(1)}+\varepsilon\beta_{\mu}^{(1)}p^{\mu}\right)+O(\varepsilon^{2})\,. (42)

Alternatively, when we evaluate the energy-momentum tensor TμνT^{\mu\nu} and the current JμJ^{\mu} using the distribution function (41), the only effect of the “integration constants” bμ(x)b_{\mu}(x) and a(x)a(x) is a linearized redefinition of 𝜷μ(x){\bm{\beta}}_{\mu}(x) and 𝜶(x){\bm{\alpha}}(x) in the perfect-fluid 𝐓μν{\bf T}^{\mu\nu} and 𝐉μ{\bf J}^{\mu}. We thus identify the correction to the hydrodynamic variables in (24) and (25) as β(1)μ=bμ\beta^{\mu}_{(1)}=b^{\mu}, α(1)=a\alpha_{(1)}=a, keeping in mind that bμb^{\mu} and aa are arbitrary, hence the fluid velocity, temperature, and the chemical potential at O(ε)O(\varepsilon) are intrinsically ambiguous quantities. Explicitly, the function (42) leads to the shift of 𝑻=T(0){\bm{T}}=T_{(0)}, 𝜶=α(0){\bm{\alpha}}=\alpha_{(0)}, and 𝒖μ=u(0)μ{\bm{u}}^{\mu}=u^{\mu}_{(0)} in the perfect-fluid expressions (35) by

T(0)T(0)+εT(1)=𝑻+ε𝑻2𝒖λbλ,\displaystyle T_{(0)}\to T_{(0)}+\varepsilon T_{(1)}={\bm{T}}+\varepsilon{\bm{T}}^{2}{\bm{u}}^{\lambda}b_{\lambda}\,, (43)
α(0)α(0)+εα(1)=𝜶+εa,\displaystyle\alpha_{(0)}\to\alpha_{(0)}+\varepsilon\alpha_{(1)}={\bm{\alpha}}+\varepsilon a\,, (44)
u(0)μu(0)μ+εu(1)μ=𝒖μ+ε𝑻𝚫μλbλ.\displaystyle u^{\mu}_{(0)}\to u^{\mu}_{(0)}+\varepsilon u^{\mu}_{(1)}={\bm{u}}^{\mu}+\varepsilon{\bm{T}}{\bm{\Delta}}^{\mu\lambda}b_{\lambda}\,. (45)

The resulting energy-momentum tensor and the current evaluated with the first-order distribution function (41) are:

Tμν=(T0μν+εT0,1μν)+εT1μν=𝐓μν[T(0)+εT(1),α(0)+εα(1),u(0)+εu(1)]+εT1μν,\displaystyle T^{\mu\nu}=(T^{\mu\nu}_{0}+\varepsilon T^{\mu\nu}_{0,1})+\varepsilon T^{\mu\nu}_{1}={\bf T}^{\mu\nu}[T_{(0)}+\varepsilon T_{(1)},\alpha_{(0)}+\varepsilon\alpha_{(1)},u_{(0)}+\varepsilon u_{(1)}]+\varepsilon T^{\mu\nu}_{1}\,, (46)
Jμ=(J0μ+εJ0,1μ)+εJ1μ=𝐉μ[T(0)+εT(1),α(0)+εα(1),u(0)+εu(1)]+εJ1μ,\displaystyle J^{\mu}=(J^{\mu}_{0}+\varepsilon J^{\mu}_{0,1})+\varepsilon J^{\mu}_{1}={\bf J}^{\mu}[T_{(0)}+\varepsilon T_{(1)},\alpha_{(0)}+\varepsilon\alpha_{(1)},u_{(0)}+\varepsilon u_{(1)}]+\varepsilon J^{\mu}_{1}\,, (47)

where the corrections T1μνT^{\mu\nu}_{1}, J1μJ^{\mu}_{1} are due to the inhomogeneous solution Φ(x,p)\Phi(x,p) in eq. (41).

First order: Inhomogeneous solution

The hard part is to find the inhomogeneous solution Φ\Phi which satisfies

pμμ𝐟p𝐟p=(1±𝐟p)(pμpνμ𝜷ν+pμμ𝜶)=[Φ].\displaystyle\frac{p^{\mu}\partial_{\mu}{\bf f}_{p}}{{\bf f}_{p}}=(1\pm{\bf f}_{p})\left(p^{\mu}p^{\nu}\partial_{\mu}{\bm{\beta}}_{\nu}+p^{\mu}\partial_{\mu}{\bm{\alpha}}\right)={\cal L}[\Phi]\,. (48)

In general, for any timelike βμ(x)\beta^{\mu}(x) and α(x)\alpha(x) we have the identity

pμpνμβν+pμμα\displaystyle p^{\mu}p^{\nu}\partial_{\mu}{\beta}_{\nu}+p^{\mu}\partial_{\mu}{\alpha} =pμpνσμν[u]2T+pμ(μαpuT(μT/T+u˙μ))\displaystyle=\frac{p^{\mu}p^{\nu}\sigma_{\mu\nu}[u]}{2T}+p^{\mu}\left(\partial_{\mu}^{\perp}\alpha-\frac{p{\cdot}u}{T}(\partial_{\mu}^{\perp}T/T+\dot{u}_{\mu})\right)
+(p2dTu+(pu)2TT˙T(pu)α˙),\displaystyle+\left(\frac{p_{\perp}^{2}}{dT}\partial{\cdot}u+\frac{(p{\cdot}u)^{2}}{T}\frac{\dot{T}}{T}-(p{\cdot}u)\dot{\alpha}\right)\,, (49)

where σμν[u]=(ΔμαΔνβ+ΔναΔμβ2dΔμνΔαβ)αuβ\sigma^{\mu\nu}[u]=(\Delta^{\mu\alpha}\Delta^{\nu\beta}+\Delta^{\nu\alpha}\Delta^{\mu\beta}-\frac{2}{d}\Delta^{\mu\nu}\Delta^{\alpha\beta})\partial_{\alpha}u_{\beta} is the shear tensor, dd is the number of space dimensions, pμΔμλpλp^{\mu}_{\perp}\equiv\Delta^{\mu\lambda}p_{\lambda}, and the hydrodynamic variables are T=1β2T=\frac{1}{\sqrt{-{\beta}^{2}}}, uμ=βμβ2u^{\mu}=\frac{{\beta}^{\mu}}{\sqrt{-{\beta}^{2}}}.

Based on eqs. (48) and (2), it is difficult to guess how the solution Φ\Phi depends on the derivatives of the hydrodynamic variables, e.g. the relative contributions of 𝑻˙\dot{\bm{T}} and 𝒖\partial{\cdot}{\bm{u}} to Φ\Phi. The standard approach is to use the constraints (39) to eliminate the zeroth-order 𝒖˙μ\dot{\bm{u}}_{\mu}, 𝑻˙\dot{\bm{T}}, and 𝜶˙\dot{\bm{\alpha}} in terms of the zeroth-order 𝒖\partial{\cdot}{\bm{u}}, μ𝜶\partial_{\mu}^{\perp}{\bm{\alpha}}, μ𝑻\partial_{\mu}^{\perp}{\bm{T}}. Then the linearized Boltzmann equation (48) becomes

(1±𝐟p)[Fσpμpνσμν[𝒖]+Fu𝒖+Fαpμμ𝜶]=[Φ],\displaystyle(1\pm{\bf f}_{p})\left[F_{\sigma}p^{\mu}p^{\nu}\sigma_{\mu\nu}[{\bm{u}}]+F_{u}\partial{\cdot}{\bm{u}}+F_{\alpha}p^{\mu}\partial_{\mu}^{\perp}{\bm{\alpha}}\right]={\cal L}[\Phi]\,, (50)

where the functions FσF_{\sigma}, FuF_{u}, FαF_{\alpha} depend on 𝑻{\bm{T}}, 𝜶{\bm{\alpha}}, (p𝒖)(p{\cdot}{\bm{u}}), and are fixed by the ideal-gas equation of state. In particular, Fσ=12𝑻F_{\sigma}=\frac{1}{2{\bm{T}}}, Fα=1+𝒏ϵ+𝒑(p𝒖)F_{\alpha}=1+\frac{{\bm{n}}}{{\bm{\epsilon}}+{\bm{p}}}(p{\cdot}{\bm{u}}). For massless particles, FuF_{u} would vanish (at order ε\varepsilon), as a consequence of scale-invariant thermodynamics, 𝒑(𝑻,𝜶)=𝑻d+1g(𝜶){\bm{p}}({\bm{T}},{\bm{\alpha}})={\bm{T}}^{d+1}g({\bm{\alpha}}). Note that μ𝑻\partial_{\mu}^{\perp}{\bm{T}} does not appear in the left-hand side of eq. (50), once 𝒖˙μ\dot{\bm{u}}_{\mu} has been eliminated. Now from eq. (50), the unknown Φ\Phi can be parametrized as

(1±𝐟p)Φ=Kηpμpνσμν[𝒖]+Kζ𝒖+Kαpμμ𝜶,\displaystyle(1\pm{\bf f}_{p})\Phi=K_{\eta}p^{\mu}p^{\nu}\sigma_{\mu\nu}[{\bm{u}}]+K_{\zeta}\partial{\cdot}{\bm{u}}+K_{\alpha}p^{\mu}\partial_{\mu}^{\perp}{\bm{\alpha}}\,, (51)

where the coefficients KηK_{\eta}, KζK_{\zeta}, KαK_{\alpha} in general depend on 𝑻{\bm{T}}, 𝜶{\bm{\alpha}}, and p𝒖p{\cdot}{\bm{u}}, and can in principle be found by solving the linearized Boltzmann equation (50). Let us write the first-order distribution function in terms of the first-order hydrodynamic variables βμ=βμ(0)+εβμ(1)\beta_{\mu}=\beta_{\mu}^{(0)}+\varepsilon\beta_{\mu}^{(1)}, α=α(0)+εα(1)\alpha=\alpha^{(0)}+\varepsilon\alpha^{(1)},

fp=𝐟p(β,α)+ε𝐟p(β,α)[Kηpμpνσμν[u]+Kζu+Kαpμμα].\displaystyle f_{p}={\bf f}_{p}(\beta,\alpha)+\varepsilon\,{\bf f}_{p}(\beta,\alpha)\left[K_{\eta}p^{\mu}p^{\nu}\sigma_{\mu\nu}[u]+K_{\zeta}\partial{\cdot}u+K_{\alpha}p^{\mu}\partial_{\mu}^{\perp}\alpha\right]\,. (52)

The first term has both O(1)O(1) and O(ε)O(\varepsilon) contributions. In the second term, the O(ε)O(\varepsilon) contributions in uu, TT, and α\alpha give O(ε2)O(\varepsilon^{2}) contributions to fpf_{p} which can be neglected at first order. We can now use the distribution function (52) to evaluate the corrections T1μνT^{\mu\nu}_{1}, J1μJ^{\mu}_{1} in (46), (47).

First order: Constitutive relations

Beyond leading (perfect-fluid) order, the energy-momentum tensor and the current will no longer have the simple form (35). For any normalized timelike vector uμu^{\mu}, the energy-momentum tensor and the current may be decomposed as Kovtun:2012rj

Tμν=uμuν+𝒫Δμν+𝒬μuν+𝒬νuμ+𝒯μν,\displaystyle T^{\mu\nu}={{\cal E}}u^{\mu}u^{\nu}+{{\cal P}}\Delta^{\mu\nu}+{{\cal Q}}^{\mu}u^{\nu}+{{\cal Q}}^{\nu}u^{\mu}+{{\cal T}}^{\mu\nu}\,, (53)
Jμ=𝒩uμ+𝒥μ,\displaystyle J^{\mu}={{\cal N}}u^{\mu}+{{\cal J}}^{\mu}\,, (54)

where 𝒬u=𝒥u=𝒯u=0{{\cal Q}}{\cdot}u={{\cal J}}{\cdot}u={{\cal T}}{\cdot}u=0, and 𝒯μν{\cal T}^{\mu\nu} is symmetric and traceless. These decompositions define {\cal E}, 𝒫{\cal P}, 𝒬{\cal Q}, 𝒯{\cal T}, 𝒩{\cal N} and 𝒥{\cal J}, for a given uμu^{\mu}. At first order in the ε\varepsilon-expansion, uμ=βμ/β2u^{\mu}={\beta}^{\mu}/{\sqrt{-{\beta}^{2}}}, where βμ=β(0)μ+εβ(1)μ\beta^{\mu}=\beta^{\mu}_{(0)}+\varepsilon\beta^{\mu}_{(1)}, as in Eq. (45). Similarly, at first order T=T(0)+εT(1)T=T_{(0)}+\varepsilon T_{(1)}, and α=α(0)+εα(1)\alpha=\alpha_{(0)}+\varepsilon\alpha_{(1)}. The first-order corrections to βμ\beta^{\mu} and α\alpha are arbitrary, and one can always redefine β(1)μβ(1)μ+bμ\beta^{\mu}_{(1)}\to\beta^{\mu}_{(1)}+b^{\prime\mu}, α(1)α(1)+a\alpha_{(1)}\to\alpha_{(1)}+a^{\prime}. At zeroth order in the expansion, =ϵ+O(ε){\cal E}={\bm{\epsilon}}+O(\varepsilon), 𝒫=𝒑+O(ε){\cal P}={\bm{p}}+O(\varepsilon), 𝒩=𝒏+O(ε){\cal N}={\bm{n}}+O(\varepsilon), while 𝒬μ{\cal Q}^{\mu}, 𝒯μν{\cal T}^{\mu\nu} and 𝒥μ{\cal J}^{\mu} are O(ε)O(\varepsilon). Substituting the distribution function (52) into the general expressions (6), (7), we find the following coefficients of the decomposition (53), (54) in terms of first-order uμu^{\mu}, TT, and α\alpha:

=ϵ+ε(ϵ/T)T2ub+ε(ϵ/α)a+ε(pu)2Kζu+O(ε2),\displaystyle{\cal E}=\epsilon+\varepsilon(\partial\epsilon/\partial T)T^{2}u{\cdot}b^{\prime}+\varepsilon(\partial\epsilon/\partial\alpha)a^{\prime}+\varepsilon\langle(p{\cdot}u)^{2}K_{\zeta}\rangle\partial{\cdot}u+O(\varepsilon^{2})\,, (55a)
𝒫=p+ε(p/T)T2ub+ε(p/α)a+ε1dp2Kζu+O(ε2),\displaystyle{\cal P}=p+\varepsilon(\partial p/\partial T)T^{2}u{\cdot}b^{\prime}+\varepsilon(\partial p/\partial\alpha)a^{\prime}+\varepsilon\langle{\textstyle{\frac{1}{d}}}p_{\perp}^{2}K_{\zeta}\rangle\partial{\cdot}u+O(\varepsilon^{2})\,, (55b)
𝒬μ=ε(ϵ+p)TΔμλbλε1dp2(pu)Kαμα+O(ε2),\displaystyle{\cal Q}^{\mu}=\varepsilon(\epsilon{+}p)T\Delta^{\mu\lambda}b^{\prime}_{\lambda}-\varepsilon\langle{\textstyle{\frac{1}{d}}}p_{\perp}^{2}(p{\cdot}u)K_{\alpha}\rangle\partial^{\mu}_{\perp}\alpha+O(\varepsilon^{2})\,, (55c)
𝒯μν=ε2d(d+2)(p2)2Kησμν+O(ε2),\displaystyle{\cal T}^{\mu\nu}=\varepsilon{\textstyle{\frac{2}{d(d+2)}}}\langle(p_{\perp}^{2})^{2}K_{\eta}\rangle\sigma^{\mu\nu}+O(\varepsilon^{2})\,, (55d)
𝒩=n+ε(n/T)T2ub+ε(n/α)aεpuKζu+O(ε2),\displaystyle{\cal N}=n+\varepsilon(\partial n/\partial T)T^{2}u{\cdot}b^{\prime}+\varepsilon(\partial n/\partial\alpha)a^{\prime}-\varepsilon\langle p{\cdot}u\,K_{\zeta}\rangle\partial{\cdot}u+O(\varepsilon^{2})\,, (55e)
𝒥μ=εnTΔμλbλ+ε1dp2Kαμα+O(ε2).\displaystyle{\cal J}^{\mu}=\varepsilon nT\Delta^{\mu\lambda}b^{\prime}_{\lambda}+\varepsilon\langle{\textstyle{\frac{1}{d}}}p_{\perp}^{2}K_{\alpha}\rangle\partial^{\mu}_{\perp}\alpha+O(\varepsilon^{2})\,. (55f)

Here ϵ\epsilon, pp, and nn are functions of (ε\varepsilon-corrected) TT and α\alpha. The angular brackets stand for =p𝐟p\langle\cdots\rangle=\int_{p}{\bf f}_{p}\cdots. These are the constitutive relations for a viscous relativistic fluid at first order in the derivative expansion. The energy-momentum tensor and the current given by these constitutive relations (in terms of O(ε)O(\varepsilon)-corrected hydrodynamic variables) must obey the standard conservation equations (11), which are true for any distribution function.

First order: Hydrodynamic “frames”

One might be tempted to ignore the “integration constants” bμ(x)b_{\mu}^{\prime}(x) and a(x)a^{\prime}(x) altogether. However, they have a simple physical meaning: the hydrodynamic variables TT, uλu^{\lambda}, and α\alpha that appear in the O(ε)O(\varepsilon) (i.e. Navier-Stokes) hydrodynamic equations can differ from the hydrodynamic variables that appear in the distribution function (12) by derivative corrections, reflecting the ambiguity in what one chooses to mean by “fluid velocity”, “fluid temperature” and “fluid chemical potential” beyond the perfect-fluid approximation. The most general parametrization of such arbitrary one-derivative corrections is

bμ=(b1T˙/T+b2u+b3α˙)uμ+b4u˙μ+b5μT/T+b6μα,\displaystyle b^{\prime}_{\mu}=(b_{1}\dot{T}/T+b_{2}\partial{\cdot}u+b_{3}\dot{\alpha})u_{\mu}+b_{4}\dot{u}_{\mu}+b_{5}\partial_{\mu}^{\perp}T/T+b_{6}\partial_{\mu}^{\perp}\alpha\,, (56a)
a=a1T˙/T+a2u+a3α˙,\displaystyle a^{\prime}=a_{1}\dot{T}/T+a_{2}\partial{\cdot}u+a_{3}\dot{\alpha}\,, (56b)

with arbitrary coefficients bn(T,α)b_{n}(T,\alpha) and an(T,α)a_{n}(T,\alpha). In relativistic hydrodynamics, one’s choice of a particular form of these derivative corrections is often called a choice of “frame”.

The parametrization (56) contains the most general one-derivative corrections with arbitrary coefficients bnb_{n} and ana_{n}. One could further demand that the redefinitions of TT, α\alpha and uλu^{\lambda} (provided by bμb^{\prime}_{\mu} and aa^{\prime}) are such that they vanish in equilibrium, even when the fluid is subject to a static external gravitational field. In equilibrium, one can choose the fluid velocity as the normalized timelike Killing vector. In zero-derivative hydrodynamics (perfect fluids) this is manifested by eq. (13), however such a choice of the fluid velocity in equilibruim of course extends beyond zero-derivative hydrodynamics, and has non-trivial consequences Jensen:2012jh . The Killing equation (13) for βμ\beta_{\mu} implies u˙μ+μT/T=0\dot{u}_{\mu}+\partial_{\mu}^{\perp}T/T=0, even though u˙μ\dot{u}_{\mu} and μT\partial_{\mu}^{\perp}T may separately be non-zero in external gravitational field. Thus demanding that (56a), (56b) vanish in equilibrium, we have b4=b5b_{4}=b_{5}. Such a choice was called a “thermodynamic frame” in ref. Jensen:2012jh . The choice amounts to demanding that the hydrostatic limit of the constitutive relations (55) follows by varying the equilibrium grand canonical free energy with respect to the external metric (for TμνT^{\mu\nu}), or with respect to the external gauge field (for JμJ^{\mu}).

The popular frame adopted by Landau and Lifshitz LL6 is obtained in the following way. One chooses b1=b3=b4=b5=a1=a3=0b_{1}=b_{3}=b_{4}=b_{5}=a_{1}=a_{3}=0, leaving one with

bμ=b2(u)uμ+b6μα,a=a2(u).\displaystyle b^{\prime}_{\mu}=b_{2}(\partial{\cdot}u)u_{\mu}+b_{6}\partial_{\mu}^{\perp}\alpha\,,\ \ \ \ a^{\prime}=a_{2}(\partial{\cdot}u)\,. (57)

The arbitrary coefficients b2b_{2} and a2a_{2} are fixed by demanding that =ϵ+O(ε2){\cal E}=\epsilon+O(\varepsilon^{2}), 𝒩=n+O(ε2){\cal N}=n+O(\varepsilon^{2}). Following the constitutive relations (55), this determines b2b_{2} and a2a_{2} in terms of (pu)2Kζ\langle(p{\cdot}u)^{2}K_{\zeta}\rangle and (pu)Kζ\langle(p{\cdot}u)K_{\zeta}\rangle. After that, the non-equilibrium pressure takes the form 𝒫=pεζ(u)+O(ε2){\cal P}=p-\varepsilon\zeta(\partial{\cdot}u)+O(\varepsilon^{2}), where ζ\zeta is the bulk viscosity,

ζ=((pϵ)n1d)(pu)2Kζ(pn)ϵ(pu)Kζ+m2dKζ,\displaystyle\zeta=\left(\left(\frac{\partial p}{\partial\epsilon}\right)_{\!n}-\frac{1}{d}\right)\langle(p{\cdot}u)^{2}K_{\zeta}\rangle-\left(\frac{\partial p}{\partial n}\right)_{\!\epsilon}\langle(p{\cdot}u)K_{\zeta}\rangle+\frac{m^{2}}{d}\langle K_{\zeta}\rangle\,, (58)

and we have used the on-shell relation m2=(pu)2p2m^{2}=(p{\cdot}u)^{2}-p_{\perp}^{2}. For massless particles, we have m2=0m^{2}=0, ϵ=dp\epsilon=d\,p, and the above expression gives ζ=0\zeta=0. Finally, the coefficient b6b_{6} is fixed by demanding 𝒬μ=O(ε2){\cal Q}^{\mu}=O(\varepsilon^{2}). Following the constitutive relations (55), this determines b6b_{6} in terms of p2(pu)Kα\langle p_{\perp}^{2}(p{\cdot}u)K_{\alpha}\rangle. The particle number flux takes the form 𝒥μ=εσTμα+O(ε2){\cal J}^{\mu}=-\varepsilon\sigma T\partial^{\mu}_{\perp}\alpha+O(\varepsilon^{2}), where σ\sigma is the particle number conductivity (which would become electrical conductivity if the particles were to carry electric charge),

σ=1dTp2Kα1dTnϵ+pp2(pu)Kα.\displaystyle\sigma=-\frac{1}{d\,T}\langle p_{\perp}^{2}K_{\alpha}\rangle-\frac{1}{d\,T}\frac{n}{\epsilon{+}p}\langle p_{\perp}^{2}(p{\cdot}u)K_{\alpha}\rangle\,. (59)

The frame of Eckart PhysRev.58.919 is obtained in a similar manner. One chooses b4=b5b_{4}=b_{5} (consistent with the thermodynamic frame), and sets b1=b3=b6=a1=a3=0b_{1}=b_{3}=b_{6}=a_{1}=a_{3}=0, so that

bμ=b2(u)uμ+b4(u˙μ+μTT),a=a2(u).\displaystyle b^{\prime}_{\mu}=b_{2}(\partial{\cdot}u)u_{\mu}+b_{4}\left(\dot{u}_{\mu}+\frac{\partial_{\mu}^{\perp}T}{T}\right)\,,\ \ \ \ a^{\prime}=a_{2}(\partial{\cdot}u)\,. (60)

The arbitrary coefficients b2b_{2} and a2a_{2} are fixed by demanding that =ϵ+O(ε2){\cal E}=\epsilon+O(\varepsilon^{2}), 𝒩=n+O(ε2){\cal N}=n+O(\varepsilon^{2}), while b4b_{4} is fixed by demanding 𝒥μ=O(ε2){\cal J}^{\mu}=O(\varepsilon^{2}). The bulk viscosity ζ\zeta again arises as the non-equilibrium correction to pressure, while the conductivity σ\sigma arises as the non-equilibrium contribution to the energy flux 𝒬μ{\cal Q}^{\mu}.

The transport coefficients ζ\zeta and σ\sigma are physical observables, and do not depend on how one chooses to fix the arbitrary coefficients in eq. (56). For example, one could choose a frame where the bulk viscosity arises as a non-equilibrium correction to the energy density, while the pressure stays uncorrected to first order, 𝒫=p+O(ε2){\cal P}=p+O(\varepsilon^{2}). The actual values of ζ\zeta and σ\sigma are of course unchanged by where they appear in the constitutive relations Kovtun:2019hdm .

In the above examples of Landau-Lifshitz and Eckart frames, the arbitrary coefficients bn(T,α)b_{n}(T,\alpha) and an(T,α)a_{n}(T,\alpha) in eq. (56) were fixed by a choice of aesthetics. For example, in the Landau-Lifshitz frame the fluid velocity uμu^{\mu} appears as an eigenvector of the energy-momentum tensor, while in the Eckart frame the equations resemble the historical formulation of the non-relativistic equations of compressible dissipative hydrodynamics. The idea behind BDNK hydrodynamics is: rather than being guided by aesthetics, the arbitrary coefficients bnb_{n} and ana_{n} need to be chosen in a way that makes the resulting hydrodynamical equations mathematically well-posed. It is a non-trivial statement that it is in fact possible to choose the coefficients ana_{n}, bnb_{n} such that the hydrodynamic equations are hyperbolic and causal. We illustrate this in appendices A and B.

Second order

Going to order O(ε2)O(\varepsilon^{2}) the Boltzmann equation becomes

εpμμ(𝐟+εf(1))=𝒞[𝐟+εf(1)+ε2f(2)].\displaystyle\varepsilon\,p^{\mu}\partial_{\mu}\left({\bf f}+\varepsilon f^{(1)}\right)={\cal C}[{\bf f}+\varepsilon f^{(1)}+\varepsilon^{2}f^{(2)}]\,. (61)

Recall that the linearized collision operator is defined as 𝒞[𝐟+δf]=𝐟[ϕ]+O(δf2){\cal C}[{\bf f}+\delta\!f]={\bf f}{\cal L}[\phi]+O(\delta\!f^{2}), where ϕ=δf/𝐟(1±𝐟)\phi=\delta\!f/{\bf f}(1\pm{\bf f}). Thus to order O(ε2)O(\varepsilon^{2}) we have

𝒞[𝐟+εf(1)+ε2f(2)]=𝐟[εϕ(1)+ε2ϕ(2)]+ε2C(2)[ϕ(1)],\displaystyle{\cal C}[{\bf f}+\varepsilon f^{(1)}+\varepsilon^{2}f^{(2)}]={\bf f}{\cal L}[\varepsilon\phi^{(1)}+\varepsilon^{2}\phi^{(2)}]+\varepsilon^{2}C^{(2)}[\phi^{(1)}], (62)

where ϕ(n)f(n)/𝐟(1±𝐟)\phi^{(n)}\equiv f^{(n)}/{\bf f}(1\pm{\bf f}), and C(2)C^{(2)} is quadratic in ϕ(1)\phi^{(1)}, but does not contain ϕ(2)\phi^{(2)}. Without specifying the explicit form of C(2)C^{(2)}, it follows that for arbitrary a(x)a(x), bμ(x)b_{\mu}(x) we have

p(a(x)+bμ(x)pμ)C(2)[ϕp(1)]=0,\displaystyle\int_{p}\left(a(x)+b_{\mu}(x)p^{\mu}\right)C^{(2)}[\phi^{(1)}_{p}]=0, (63)

as a consequence of the microscopic conservation laws embodied by eqs. (10), (30), and (32). The Boltzmann equation at order O(ε2)O(\varepsilon^{2}) is

pμμf(1)C(2)[ϕ(1)]=𝐟[ϕ(2)],\displaystyle p^{\mu}\partial_{\mu}f^{(1)}-C^{(2)}[\phi^{(1)}]={\bf f}{\cal L}[\phi^{(2)}]\,, (64)

where f(1)f^{(1)} in the left-hand side is known from the O(ε)O(\varepsilon) calculation in eqs. (41), (51),

fp(1)=𝐟p(1±𝐟p)(a(1)+bμ(1)pμ)+𝐟p(Kηpμpνσμν+Kζu+Kαpμμα).\displaystyle f^{(1)}_{p}={\bf f}_{p}(1\pm{\bf f}_{p})\left(a^{(1)}+b^{(1)}_{\mu}p^{\mu}\right)+{\bf f}_{p}\left(K_{\eta}p^{\mu}p^{\nu}\sigma_{\mu\nu}+K_{\zeta}\partial{\cdot}u+K_{\alpha}p^{\mu}\partial_{\mu}^{\perp}\alpha\right)\,. (65)

As before, the linear equation (64) can only be solved for ϕ(2)\phi^{(2)} if the left-hand side is orthogonal to the zero-modes of the operator {\cal L} in the right-hand side. The quadratic part C(2)C^{(2)} drops out from the orthogonality condition thanks to eq. (63), and the constraint becomes p(a+bνpν)pμμf(1)=0\int_{p}\left(a+b_{\nu}p^{\nu}\right)p^{\mu}\partial_{\mu}f^{(1)}=0, or equivalently

μJ(1)μ=0,μT(1)μν=0.\displaystyle\partial_{\mu}J^{\mu}_{(1)}=0\,,\ \ \ \ \partial_{\mu}T^{\mu\nu}_{(1)}=0\,. (66)

Here J(1)μJ^{\mu}_{(1)} and T(1)μνT^{\mu\nu}_{(1)} are given by eqs. (6), (7), evaluated with fp(1)f^{(1)}_{p} in eq. (65). Connecting these expressions to T(1)μνT^{\mu\nu}_{(1)} in eq. (26b), the first term in (65) gives T0,1μνT^{\mu\nu}_{0,1}, the second term in (65) gives T1μνT^{\mu\nu}_{1}, and similarly for the current J(1)μJ^{\mu}_{(1)}. In other words, the equations of 1-st order (Navier-Stokes) hydrodynamics arise as constraint equations at 2-nd order in the expansion. The same happens to all orders: the equations (27) of nthn^{\rm th}-order hydrodynamics arise as constraint equations at (n+1)th(n{+}1)^{\rm th}-order in the expansion.

3 Fluid/Gravity correspondence

In the preceding section, we have outlined a procedure to derive causal hydrodynamics from kinetic theory. There is an analogous procedure to derive hydrodynamic equations from classical gravity in asymptotically anti-de Sitter spacetimes. This is done via the fluid/gravity correspondence Bhattacharyya:2008jc ; Erdmenger:2008rm ; Banerjee:2008th , see Hubeny:2011hd for a review.

Einstein-Maxwell equations and Hilbert expansion

Following the original fluid-gravity discussion, we focus on the simplest holographic model of a 3+1 dimensional quantum field theory with a conserved global U(1) symmetry: the Einstein-Maxwell theory in AdS5,

S=116πGN(5)d5xg[R+1214FMNFMN],S=\frac{1}{16\pi G_{N}^{(5)}}\int d^{5}x\sqrt{-g}\biggl{[}R+12-\frac{1}{4}F_{MN}F^{MN}\biggr{]}, (67)

where latin indices M,NM,N are bulk indices; greek indices, raised and lowered by the Minkowski metric ημν\eta^{\mu\nu}, will be used for the boundary directions. The AdS radius of curvature has been set to one, hence the cosmological constant is Λ=6\Lambda=-6. The Einstein-Maxwell equations are

RMN12RgMN6gMN+12[FMKFNK+14gMNFKLFKL]=0,\displaystyle R_{MN}-\frac{1}{2}Rg_{MN}-6g_{MN}+\frac{1}{2}\biggl{[}F_{MK}F^{K}_{\,\,N}+\frac{1}{4}g_{MN}F_{KL}F^{KL}\biggr{]}=0, (68a)
MFMN=0.\displaystyle\nabla_{M}F^{MN}=0. (68b)

The solution of (68) that corresponds to the equilibrium state in the dual field theory at non-zero temperature and non-zero U(1) charge density is the electrically charged black brane,

ds2=2uμdxμdrr2f(r)uμuνdxμdxν+r2Δμνdxμdxν,f(r)=11b4r4+Q2r6,\displaystyle ds^{2}=-2u_{\mu}dx^{\mu}dr-r^{2}f(r)u_{\mu}u_{\nu}dx^{\mu}dx^{\nu}+r^{2}\Delta_{\mu\nu}dx^{\mu}dx^{\nu},\quad f(r)=1-\frac{1}{b^{4}r^{4}}+\frac{Q^{2}}{r^{6}}, (69a)
AMdxM=3Q2r2uμdxμ.\displaystyle A_{M}dx^{M}=\frac{\sqrt{3}Q}{2r^{2}}u_{\mu}dx^{\mu}. (69b)

The solution contains three constant parameters: a timelike covector uμu_{\mu} (normalized such that uμuμ=1u_{\mu}u^{\mu}=-1), a charge QQ, and a mass parameter bb. As before, Δμν=ημν+uμuν\Delta_{\mu\nu}=\eta_{\mu\nu}+u_{\mu}u_{\nu} is the spatial projector on the boundary. This metric is written in infalling Eddington-Finkelstein coordinates. The vector uμu^{\mu} defines the rest frame of the fluid on the boundary. The parameters bb and QQ are (somewhat unilluminating) functions of the temperature TT and the U(1) chemical potential μ\mu of the boundary fluid. The explicit expressions for b(T,μ)b(T,\mu) and Q(T,μ)Q(T,\mu) can be obtained from refs. Erdmenger:2008rm ; Banerjee:2008th , in particular b(T,μ0)=1/πTb(T,\mu{\to}0)=1/\pi T and Q(T,μ0)=0Q(T,\mu{\to}0)=0.

Drawing an analogy with kinetic theory, the equilibrium metric 𝐠{\bf g} and the equilibrium gauge field 𝐀{\bf A} of eq. (69) are the holographic analogues of the equilibrium distribution function 𝐟{\bf f}. If the parameters bb, QQ, and uμu_{\mu} are promoted to be functions of the boundary coordinates, i.e. b(x),uμ(x),Q(x)b(x),u_{\mu}(x),Q(x), then (69) is no longer a solution to (68). However, in analogy with kinetic theory, we may construct approximate solutions through a Hilbert expansion of the form

g(x)=𝐠(x)+εg(1)(x)+ε2g(2)(x)+O(ε3),\displaystyle g(x)={\bf g}(x)+\varepsilon g^{(1)}(x)+\varepsilon^{2}g^{(2)}(x)+O(\varepsilon^{3}), (70a)
A(x)=𝐀(x)+εA(1)(x)+ε2A(2)(x)+O(ε3).\displaystyle A(x)={\bf A}(x)+\varepsilon A^{(1)}(x)+\varepsilon^{2}A^{(2)}(x)+O(\varepsilon^{3}). (70b)

Similarly, the parameters themselves get corrected order-by-order as well:

b(x)=b(0)(x)+εb(1)(x)+ε2b(2)(x)+O(ε3),\displaystyle b(x)=b^{(0)}(x)+\varepsilon b^{(1)}(x)+\varepsilon^{2}b^{(2)}(x)+O(\varepsilon^{3}), (71a)
uμ(x)=uμ(0)(x)+εuμ(1)(x)+ε2uμ(2)(x)+O(ε3),\displaystyle u_{\mu}(x)=u_{\mu}^{(0)}(x)+\varepsilon u_{\mu}^{(1)}(x)+\varepsilon^{2}u_{\mu}^{(2)}(x)+O(\varepsilon^{3}), (71b)
Q(x)=Q(0)(x)+εQ(1)(x)+ε2Q(2)(x)+O(ε3).\displaystyle Q(x)=Q^{(0)}(x)+\varepsilon Q^{(1)}(x)+\varepsilon^{2}Q^{(2)}(x)+O(\varepsilon^{3}). (71c)

Inserting (70) into the Einstein-Maxwell equations (68) and equating like-powers gives an analogue to the linearized Boltzmann equation:

[g(n),A(n)]=sn[g(n1),A(n1),],{\cal H}[g^{(n)},A^{(n)}]=s_{n}[g^{(n-1)},A^{(n-1)},...], (72)

where the operator {\cal H}, like the linearized collision operator {\cal L}, depends only of the equilibrium metric 𝐠{\bf g} and equilibrium gauge field 𝐀{\bf A}, is the same at all orders in ε\varepsilon, and (crucially) has zero modes. In the same way that {\cal L} involves integrals of pp, the operator {\cal H} involves derivatives with respect to rr (compare with the interpretation of the rr-direction as the energy scale in the dual field theory). The source term depends only on the lower-order corrections to the metric and the gauge field. The explicit expressions for {\cal H} and s0s_{0}, s1s_{1}, s2s_{2} may be found in Bhattacharyya:2008jc ; Erdmenger:2008rm ; Banerjee:2008th . The constraint equations in the bulk give rise to

μT(n1)μν=0,μJ(n1)μ=0,\partial_{\mu}T^{\mu\nu}_{(n-1)}=0,\qquad\partial_{\mu}J^{\mu}_{(n-1)}=0, (73)

where T(n1)μνT^{\mu\nu}_{(n-1)} and J(n1)μJ^{\mu}_{(n-1)} are the (n1)th(n-1)^{\rm th}-order correction to the boundary stress-energy tensor and the U(1) charge current, respectively. Again, this is the exact same constraint that one finds in kinetic theory: the perfect-fluid equations come about as a constraint at first order, the Navier-Stokes equations arise as a constraint at second order, etc.

Zero modes of {\cal H}

The operator {\cal H} is a linear differential operator in rr whose coefficients depend on the zeroth-order functions b(0)(x)b^{(0)}(x), uμ(0)(x)u_{\mu}^{(0)}(x), and Q(0)(x)Q^{(0)}(x). Hence, the zero modes of {\cal H} must be specific functions of rr and b(0)(x)b^{(0)}(x), uμ(0)(x)u_{\mu}^{(0)}(x), Q(0)(x)Q^{(0)}(x) which are multiplied by arbitrary functions of the boundary coordinates (integration constants with respect to rr).

Suppose we want to solve the Einstein-Maxwell equations to first order in ε\varepsilon. After enforcing boundary conditions and removing gauge redundancies, the solution can be written as

ds2=𝐠MNdxMdxN\displaystyle ds^{2}={\bf g}_{MN}dx^{M}dx^{N}
+ε(GMN(1)+𝔟(x)fMN(b)+𝔮(x)fMN(Q)+𝔲λ(x)[f(u)]MNλ)dxMdxN+O(ε2),\displaystyle\quad\,\,\,+\varepsilon\biggl{(}G^{(1)}_{MN}+{\mathfrak{b}}(x)f^{(b)}_{MN}+{\mathfrak{q}}(x)f^{(Q)}_{MN}+{\mathfrak{u}}_{\lambda}(x)\left[f^{(u)}\right]^{\lambda}_{MN}\biggr{)}dx^{M}dx^{N}+O(\varepsilon^{2}), (74a)
AMdxM=𝐀MdxM+ε(AM(1)dxM+𝔮(x)fM(Q)+𝔲λ(x)[f(u)]Mλ)dxM+O(ε2).\displaystyle A_{M}dx^{M}={\bf A}_{M}dx^{M}+\varepsilon\left(A^{(1)}_{M}dx^{M}+{\mathfrak{q}}(x)f^{(Q)}_{M}+{\mathfrak{u}}_{\lambda}(x)\left[f^{(u)}\right]^{\lambda}_{M}\right)dx^{M}+O(\varepsilon^{2})\,. (74b)

Here GMN(1)G_{MN}^{(1)}, AM(1)A_{M}^{(1)} are particular solutions found by inverting the operator {\cal H} (analogous to Φp\Phi_{p} in the previous section), and depend on the source s1s_{1} in the right-hand side of (72). The functions 𝔟(x){\mathfrak{b}}(x), 𝔮(x){\mathfrak{q}}(x), and 𝔲λ(x){\mathfrak{u}}_{\lambda}(x) are “integration constants” with respect to rr, and uλ𝔲λ=0u^{\lambda}{\mathfrak{u}}_{\lambda}=0. Finally, fMN(b)f^{(b)}_{MN}, fMN(Q)f^{(Q)}_{MN}, [f(u)]MNλ\left[f^{(u)}\right]^{\lambda}_{MN}, fM(Q)f_{M}^{(Q)}, and [f(u)]Mλ\left[f^{(u)}\right]^{\lambda}_{M} are the accompanying bases for the zero modes of {\cal H}. Their explicit form is

fMN(b)dxMdxN\displaystyle f_{MN}^{(b)}dx^{M}dx^{N} =4b(0)5r2uμ(0)uν(0)dxμdxν,\displaystyle=-\frac{4}{b_{(0)}^{5}r^{2}}u_{\mu}^{(0)}u_{\nu}^{(0)}dx^{\mu}dx^{\nu}, (75a)
fMN(Q)dxMdxN\displaystyle f_{MN}^{(Q)}dx^{M}dx^{N} =2Q(0)r4uμ(0)uν(0)dxμdxν,\displaystyle=-\frac{2Q^{(0)}}{r^{4}}u_{\mu}^{(0)}u_{\nu}^{(0)}dx^{\mu}dx^{\nu}, (75b)
[f(u)]MNλdxMdxN\displaystyle\biggl{[}f^{(u)}\biggr{]}^{\lambda}_{MN}dx^{M}dx^{N} =r2(1f(0)(r))ηλα(Δαμ(0)uν(0)+Δαν(0)uμ(0))dxμdxν,\displaystyle=r^{2}(1-f^{(0)}(r))\eta^{\lambda\alpha}\left(\Delta_{\alpha\mu}^{(0)}u_{\nu}^{(0)}+\Delta_{\alpha\nu}^{(0)}u_{\mu}^{(0)}\right)dx^{\mu}dx^{\nu}, (75c)
fM(Q)dxM\displaystyle f_{M}^{(Q)}dx^{M} =32r2uμ(0)dxμ,\displaystyle=\frac{\sqrt{3}}{2r^{2}}u_{\mu}^{(0)}dx^{\mu}, (75d)
[f(u)]MλdxM\displaystyle\biggl{[}f^{(u)}\biggr{]}^{\lambda}_{M}dx^{M} =3Q(0)2r2ηλαΔαμ(0)dxμ,\displaystyle=\frac{\sqrt{3}Q^{(0)}}{2r^{2}}\eta^{\lambda\alpha}\Delta_{\alpha\mu}^{(0)}dx^{\mu}, (75e)

where f(0)(r)=11/(b(0)4r4)+Q(0)2/r6f^{(0)}(r)=1-1/(b_{(0)}^{4}r^{4})+Q_{(0)}^{2}/r^{6}. The normalization in (75) has been chosen so that the “integration constants” 𝔟{\mathfrak{b}}, 𝔮{\mathfrak{q}}, and 𝔲λ{\mathfrak{u}}_{\lambda} represent corrections to the quantities bb, QQ, and uμu_{\mu}, respectively. We can see that this is the case by looking at the equilibrium metric 𝐠{\bf g} and equilibrium gauge field 𝐀{\bf A}, and then expanding these parameters as in (71). Note that uλ(1)u(0)λ=O(ε2)u_{\lambda}^{(1)}u^{\lambda}_{(0)}=O(\varepsilon^{2}), and so to first order in ε\varepsilon, u(1)λΔλμ(0)=uμ(1)u^{\lambda}_{(1)}\Delta_{\lambda\mu}^{(0)}=u_{\mu}^{(1)}. Expanding, we find

𝐠MNdxMdxN=\displaystyle{\bf g}_{MN}dx^{M}dx^{N}= 2uμ(0)dxμdrr2(11b(0)4r4+Q(0)2r6)uμ(0)uν(0)dxμdxν+r2Δμν(0)dxμdxν\displaystyle-2u_{\mu}^{(0)}dx^{\mu}dr-r^{2}\left(1-\frac{1}{b_{(0)}^{4}r^{4}}+\frac{Q_{(0)}^{2}}{r^{6}}\right)u^{(0)}_{\mu}u^{(0)}_{\nu}dx^{\mu}dx^{\nu}+r^{2}\Delta^{(0)}_{\mu\nu}dx^{\mu}dx^{\nu}
+ε[2uμ(1)dxμdr(4b(1)r2b(0)5+2Q(0)Q(1)r4)uμ(0)uν(0)dxμdxν\displaystyle+\varepsilon\biggl{[}-2u^{(1)}_{\mu}dx^{\mu}dr-\left(\frac{4b^{(1)}}{r^{2}b_{(0)}^{5}}+\frac{2Q^{(0)}Q^{(1)}}{r^{4}}\right)u_{\mu}^{(0)}u_{\nu}^{(0)}dx^{\mu}dx^{\nu}
+r2(1f(0)(r))uα(1)ηαλ(Δλμ(0)uν(0)+uμ(0)Δλν(0))dxμdxν]+O(ε2),\displaystyle+r^{2}(1-f^{(0)}(r))u_{\alpha}^{(1)}\eta^{\alpha\lambda}\left(\Delta_{\lambda\mu}^{(0)}u_{\nu}^{(0)}+u_{\mu}^{(0)}\Delta_{\lambda\nu}^{(0)}\right)dx^{\mu}dx^{\nu}\biggr{]}+O(\varepsilon^{2}), (76)
𝐀MdxM=3Q(0)2r2uμ(0)dxμ+ε[3Q(1)2r2uμ(0)dxμ+3Q(0)2r2uα(1)ηαλΔλμ(0)dxμ]+O(ε2).\displaystyle{\bf A}_{M}dx^{M}=\frac{\sqrt{3}Q^{(0)}}{2r^{2}}u_{\mu}^{(0)}dx^{\mu}+\varepsilon\biggl{[}\frac{\sqrt{3}Q^{(1)}}{2r^{2}}u_{\mu}^{(0)}dx^{\mu}+\frac{\sqrt{3}Q^{(0)}}{2r^{2}}u_{\alpha}^{(1)}\eta^{\alpha\lambda}\Delta_{\lambda\mu}^{(0)}dx^{\mu}\biggr{]}+O(\varepsilon^{2}). (77)

By direct comparison, one can see that b(1)=𝔟(x)b^{(1)}={\mathfrak{b}}(x), Q(1)=𝔮(x)Q^{(1)}={\mathfrak{q}}(x), and uμ(1)=𝔲μ(x)u_{\mu}^{(1)}={\mathfrak{u}}_{\mu}(x). As the hydrodynamic variables βμ=uμ/T\beta_{\mu}=u^{\mu}/T and α=μ/T\alpha=\mu/T are functions of bb, QQ, and uμu_{\mu}, the “integration constants” 𝔟{\mathfrak{b}}, 𝔮{\mathfrak{q}}, and 𝔲λ{\mathfrak{u}}^{\lambda} will set the hydrodynamic “frame”. The corrections to the “conventional” hydrodynamic variables α=μ/T\alpha=\mu/T and βμ=uμ/T\beta_{\mu}=u_{\mu}/T are given by

α(1)\displaystyle\alpha^{(1)} =α(0)b(0)𝔟+α(0)Q(0)𝔮,\displaystyle=\frac{\partial\alpha^{(0)}}{\partial b^{(0)}}{\mathfrak{b}}+\frac{\partial\alpha^{(0)}}{\partial Q^{(0)}}\,{\mathfrak{q}}, (78a)
βμ(1)\displaystyle\beta_{\mu}^{(1)} =1T(0)2(T(0)b(0)𝔟+T(0)Q(0)𝔮)uμ(0)+1T(0)𝔲λΔλμ(0).\displaystyle=-\frac{1}{T_{(0)}^{2}}\left(\frac{\partial T^{(0)}}{\partial b^{(0)}}\,{\mathfrak{b}}+\frac{\partial T^{(0)}}{\partial Q^{(0)}}{\mathfrak{q}}\right)u_{\mu}^{(0)}+\frac{1}{T_{(0)}}{\mathfrak{u}}^{\lambda}\Delta_{\lambda\mu}^{(0)}\,. (78b)

The partial derivatives can be evaluated by inverting the known equilibrium functions b(T,μ)b(T,\mu) and Q(T,μ)Q(T,\mu) to find T(b,Q)T(b,Q) and μ(b,Q)\mu(b,Q). Thus fixing 𝔟{\mathfrak{b}}, 𝔮{\mathfrak{q}}, and 𝔲μ{\mathfrak{u}}_{\mu} is equivalent to fixing the definitions of the hydrodynamic variables βμ\beta_{\mu} and α\alpha at O(ε)O(\varepsilon). The original fluid-gravity references Bhattacharyya:2008jc ; Erdmenger:2008rm ; Banerjee:2008th adopted the Landau-Lifshitz convention, however tuning 𝔟{\mathfrak{b}}, 𝔮{\mathfrak{q}}, and 𝔲μ{\mathfrak{u}}_{\mu} may be used to generate other conventions. In particular, hydrodynamic field redefinitions can be used to arrive at stable and causal first-order hydrodynamics as described in Kovtun:2019hdm .

4 Conclusions

Physically, hydrodynamics is a theory of local densities of conserved quantities (energy, momentum, etc) which can not disappear through microscopic interactions, but rather spread out through the corresponding fluxes. On the other hand, when derived from a more fundamental microscopic description such as the kinetic theory or holography, classical hydrodynamics may be viewed as a theory of zero modes. In kinetic theory, the zero modes are those of the linearized collision operator {\cal L}. In the fluid-gravity correspondence, the zero modes are those of the operator {\cal H}. While the bulk fields in the fluid-gravity correspondence are the analogues of the distribution function, the operator {\cal H} is the analogue of the linearized collision operator. Indeed, as was emphasized in ref. Hubeny:2011hd , the equations of bulk dynamics may be considered as a strong-coupling analogue of the Boltzmann equation.

The freedom of choosing the zero modes at each order of the derivative expansion translates to the freedom of field redefinitions of the hydrodynamic variables. While in kinetic theory the zero modes are naturally associated with the shifts of βμ=uμ/T\beta^{\mu}=u^{\mu}/T and α=μ/T\alpha=\mu/T which parametrize the equilibrium distribution function, the zero modes in the fluid-gravity correspondence are naturally associated with the shifts of b(T,α)b(T,\alpha), uμu^{\mu}, and Q(T,α)Q(T,\alpha) which parametrize the equilibrium bulk metric and the gauge field. Still, hydrodynamic field redefinitions work in exactly the same way in both setups: neither the Hilbert expansion in kinetic theory nor the analogous expansion in fluid-gravity come with a preferred “frame”. In both kinetic theory and in fluid-gravity one may obtain causal hydrodynamic equations through a judicious choice of zero modes at one-derivative order. We plan to return to further exploring the connections between the Botlzmann equation and the fluid-gravity duality in the future.

Acknowledgements.
This work was supported in part by the NSERC of Canada.

Appendix A Examples of causal frames

Following ref. Kovtun:2019hdm , we will denote the one-derivative terms in the constitutive relations as

=ϵ+ε1T˙/T+ε2u+ε3α˙+O(2),\displaystyle{\cal E}=\epsilon+\varepsilon_{1}\dot{T}/T+\varepsilon_{2}\partial{\cdot}u+\varepsilon_{3}\dot{\alpha}+O(\partial^{2}), (79a)
𝒫=p+π1T˙/T+π2u+π3α˙+O(2),\displaystyle{\cal P}=p+\pi_{1}\dot{T}/T+\pi_{2}\partial{\cdot}u+\pi_{3}\dot{\alpha}+O(\partial^{2}), (79b)
𝒬μ=θ1(u˙μ+μT/T)+θ3μα+O(2),\displaystyle{\cal Q}^{\mu}=\theta_{1}\left(\dot{u}^{\mu}+\partial^{\mu}_{\perp}T/T\right)+\theta_{3}\partial^{\mu}_{\perp}\alpha+O(\partial^{2}), (79c)
𝒯μν=ησμν+O(2),\displaystyle{\cal T}^{\mu\nu}=-\eta\sigma^{\mu\nu}+O(\partial^{2}), (79d)
𝒩=n+ν1T˙/T+ν2u+ν3α˙+O(2),\displaystyle{\cal N}=n+\nu_{1}\dot{T}/T+\nu_{2}\partial{\cdot}u+\nu_{3}\dot{\alpha}+O(\partial^{2}), (79e)
𝒥μ=γ1(u˙μ+μT/T)+γ3μα+O(2).\displaystyle{\cal J}^{\mu}=\gamma_{1}\left(\dot{u}^{\mu}+\partial^{\mu}_{\perp}T/T\right)+\gamma_{3}\partial^{\mu}_{\perp}\alpha+O(\partial^{2}). (79f)

The combinations of the transport parameters that are invariant under the redefinitions of TT, uμu^{\mu}, and α\alpha by one-derivative corrections are Kovtun:2019hdm

fi=πiεi(p/ϵ)nνi(p/n)ϵ,\displaystyle f_{i}=\pi_{i}-\varepsilon_{i}(\partial p/\partial\epsilon)_{n}-\nu_{i}(\partial p/\partial n)_{\epsilon}\,, (80)
i=γinθi/(ϵ+p).\displaystyle\ell_{i}=\gamma_{i}-n\theta_{i}/(\epsilon{+}p)\,. (81)

The physical transport coefficients (bulk viscosity and charge conductivity) are

ζ=f2+(pϵ)nf1+1T(pn)ϵf3,\displaystyle\zeta=-f_{2}+\left(\frac{\partial p}{\partial\epsilon}\right)_{\!n}f_{1}+\frac{1}{T}\left(\frac{\partial p}{\partial n}\right)_{\!\epsilon}f_{3}\,, (82)
σ=1T3+nϵ+p1.\displaystyle\sigma=-\frac{1}{T}\ell_{3}+\frac{n}{\epsilon+p}\ell_{1}\,. (83)

Suppose that we have found the distribution function at O(ε)O(\varepsilon) by eliminating u˙μ\dot{u}^{\mu}, T˙\dot{T} and α˙\dot{\alpha}, as in eq. (52). This choice of eliminating the time derivatives gives rise to the following constraints on the transport parameters:

π1=(pϵ)nε1+(pn)ϵν1,\displaystyle\pi_{1}=\left(\frac{\partial p}{\partial\epsilon}\right)_{n}\varepsilon_{1}+\left(\frac{\partial p}{\partial n}\right)_{\epsilon}\nu_{1}, (84a)
π2=(pϵ)nε2+(pn)ϵν2ζ,\displaystyle\pi_{2}=\left(\frac{\partial p}{\partial\epsilon}\right)_{n}\varepsilon_{2}+\left(\frac{\partial p}{\partial n}\right)_{\epsilon}\nu_{2}-\zeta, (84b)
π3=(pϵ)nε3+(pn)ϵν3,\displaystyle\pi_{3}=\left(\frac{\partial p}{\partial\epsilon}\right)_{n}\varepsilon_{3}+\left(\frac{\partial p}{\partial n}\right)_{\epsilon}\nu_{3}, (84c)
γ1=nϵ+pθ1,\displaystyle\gamma_{1}=\frac{n}{\epsilon+p}\theta_{1}, (84d)
γ3=nϵ+pθ3Tσ.\displaystyle\gamma_{3}=\frac{n}{\epsilon+p}\theta_{3}-T\sigma. (84e)

We also take θ1=θ2\theta_{1}=\theta_{2}, γ1=γ2\gamma_{1}=\gamma_{2}, as required in a thermodynamic frame. In other words, eliminating the time derivatives makes the frame invariants f1f_{1}, f3f_{3}, 1\ell_{1}, 2\ell_{2} vanish, while f2=ζf_{2}=-\zeta, and 3=Tσ\ell_{3}=-T\sigma. The non-zero values of the transport parameters εi\varepsilon_{i}, πi\pi_{i} etc in (79) are due to the zero modes of the linearized collision operator, with the exception of the physical transport coefficients η\eta, ζ\zeta, and σ\sigma which are of course insensitive to the zero modes.

Ignoring the kinetic theory motivation, one can simply view (84) as a particular set of constraints which one may choose to impose on the one-derivative transport parameters. We will now show that these constraints are consistent with causality, in other words that one may choose transport parameters εi\varepsilon_{i}, πi\pi_{i}, etc such that the constraints (84) are satisfied, and the hydrodynamic equations with the constitutive relations (79) are causal.

We start with one-derivative hydrodynamics of conformal fluids. In dd space dimensions, p=ϵ/dp{=}\epsilon/d, hence (p/n)ϵ=0\left(\partial p/\partial n\right)_{\epsilon}=0, and νn\nu_{n} drop out of the constraints (84). Further, conformal symmetry dictates ζ=0\zeta=0, πn=εn/d\pi_{n}=\varepsilon_{n}/d, and the first three constraints in (84) are satisfied identically. Additionally, conformal symmetry implies ε2=ε1/d\varepsilon_{2}=\varepsilon_{1}/d, ν2=ν1/d\nu_{2}=\nu_{1}/d Kovtun:2019hdm . A class of causal and stable frames which satisfy (84) was given in ref. Hoult:2020eho : choosing

ε3=θ3=ν1=0,\displaystyle\varepsilon_{3}=\theta_{3}=\nu_{1}=0\,, (85)
ν3>σT,\displaystyle\nu_{3}>\sigma T\,, (86)
ε2>(2d2)η,\displaystyle\varepsilon_{2}>(2d-2)\eta\,, (87)
12dd1ηθ12d1ηε2>0,\displaystyle 1-\frac{2d}{d{-}1}\frac{\eta}{\theta_{1}}-\frac{2}{d{-}1}\frac{\eta}{\varepsilon_{2}}>0\,, (88)

will give rise to causal first-order hydrodynamics. In d=3d=3 space dimensions, it suffices to choose ν3>σT\nu_{3}>\sigma T, ε2>4η\varepsilon_{2}>4\eta, θ1>4η\theta_{1}>4\eta in order to satisfy the above inequalities.

Now consider non-conformal fluids in d=3d=3 space dimensions. As an example, suppose we narrow down the class of frames by demanding that

ν1=(nϵ+p)ε1,ν2=(nϵ+p)ε2,ν3=δ+(nϵ+p)ε3,\nu_{1}=\left(\frac{n}{\epsilon+p}\right)\varepsilon_{1},\ \ \ \ \nu_{2}=\left(\frac{n}{\epsilon+p}\right)\varepsilon_{2},\ \ \ \ \nu_{3}=\delta+\left(\frac{n}{\epsilon+p}\right)\varepsilon_{3}, (89)

where δ\delta is to be constrained momentarily. The short-wavelength modes propagate with a linear dispersion relation ω(𝐤)=±cs|𝐤|\omega({\bf k})=\pm c_{s}|{\bf k}|, where the speed csc_{s} is determined by

(cs2θ1η)2(cs2δTσ)(cs4cs2(vs2+ε2ε1+γsθ1)+vs2ε2γsε1)=0,\displaystyle\left(c_{s}^{2}\theta_{1}-\eta\right)^{2}\left(c_{s}^{2}\delta-T\sigma\right)\left(c_{s}^{4}-c_{s}^{2}\left(v_{s}^{2}{+}\frac{\varepsilon_{2}}{\varepsilon_{1}}{+}\frac{\gamma_{s}}{\theta_{1}}\right)+\frac{v_{s}^{2}\varepsilon_{2}-\gamma_{s}}{\varepsilon_{1}}\right)=0\,, (90)

where vs2=(p/ϵ)n+n/(ϵ+p)(p/n)ϵv_{s}^{2}=(\partial p/\partial\epsilon)_{n}+{n}/{(\epsilon{+}p)}(\partial p/\partial n)_{\epsilon} is the speed of sound, and γs=43η+ζ\gamma_{s}={\textstyle{\frac{4}{3}}}\eta+\zeta. Causality demands 0<cs2<10<c_{s}^{2}<1. The first factor (shear waves) gives the causality constraint θ1>η\theta_{1}>\eta, while the second factor constrains δ>Tσ\delta>T\sigma. The causality constraints from the last factor are

0<vs2ε2γs<ε1,\displaystyle 0<v_{s}^{2}\varepsilon_{2}-\gamma_{s}<\varepsilon_{1}\,, (91)
(1vs2)(ε1ε2)θ1>γs(ε1+θ1).\displaystyle(1-v_{s}^{2})(\varepsilon_{1}-\varepsilon_{2})\theta_{1}>\gamma_{s}(\varepsilon_{1}+\theta_{1})\,. (92)

These constraints can be satisfied for any value of vsv_{s} between 0 and 1. Demanding that the modes are stable at 𝐤=0{\bf k}=0, it is sufficient to require

T(pϵ)nε1+(pn)ϵε3>0.\displaystyle T\left(\frac{\partial p}{\partial\epsilon}\right)_{\!n}\varepsilon_{1}+\left(\frac{\partial p}{\partial n}\right)_{\!\epsilon}\varepsilon_{3}>0\,. (93)

Appendix B Real space analysis of causality

The hydrodynamic equations with the constitutive relations (79) are quasi-linear partial differential equations of the form

(Mμν)ABμνUB+(lower-derivative terms)=0,\left({M}^{\mu\nu}\right)_{AB}\partial_{\mu}\partial_{\nu}U^{B}+\left(\text{lower-derivative terms}\right)=0\,, (94)

where the vector UU contains hydrodynamic variables, for example UM=(βμ,α)U^{M}=(\beta^{\mu},\alpha). The principal part Mμν(U)M^{\mu\nu}(U) is determined by the constitutive relations, and can be read off from the hydrodynamic conservation laws, see ref. Hoult:2020eho for examples. The characteristic velocities of the system may be found by analyzing the roots of the characteristic equation

det(Mμνξμξν)=0,\det\left({M}^{\mu\nu}\xi_{\mu}\xi_{\nu}\right)=0, (95)

see e.g. Courant-Hilbert , ch. VI. The co-vectors ξμ\xi_{\mu} determined by this equation are normal to the characteristics of the system which must fall within the lightcone. We thus demand that the solutions of (95) satisfy:

  1. 1.

    ξ0=ξ0(ξi)\xi_{0}=\xi_{0}(\xi_{i}) are real (hyperbolicity), and

  2. 2.

    |ξ0||ξ||\xi_{0}|\leq|\vec{\xi}| (causality).

In first-order hydrodynamics, QAB(Mμν)ABξμξνQ_{AB}\equiv\left({M}^{\mu\nu}\right)_{AB}\xi_{\mu}\xi_{\nu} is of the form

Q=[Auνuρ+BΔρν+Cuνξρ+Dξνuρ+EξνξρFuν+GξνHuρ+IξρJ]Q=\begin{bmatrix}Au^{\nu}u_{\rho}+B\Delta^{\nu}_{\,\,\,\rho}+Cu^{\nu}\xi_{\rho}+D\xi^{\nu}u_{\rho}+E\xi^{\nu}\xi_{\rho}&Fu^{\nu}+G\xi^{\nu}\\ Hu_{\rho}+I\xi_{\rho}&J\end{bmatrix} (96)

In d+1d+1 spacetime dimensions, QQ is a (d+2)×(d+2)(d{+}2)\times(d{+}2) matrix. One can derive an explicit expression for the determinant of (96), which is also valid in curved space:

det(Q)\displaystyle\det\left(Q\right) =Bd1{B(FHAJ)+B(CJ+DJHGFI)(ξu)+B(GIEJ)(ξu)2\displaystyle=B^{d-1}\biggl{\{}B(FH-AJ)+B(CJ+DJ-HG-FI)(\xi{\cdot}u)+B(GI-EJ)(\xi{\cdot}u)^{2}
+[G(AIHC)+F(HEID)+J(CDAE)](ξΔξ)}.\displaystyle+\biggl{[}G(AI-HC)+F(HE-ID)+J(CD-AE)\biggr{]}(\xi{\cdot}\Delta{\cdot}\xi)\biggr{\}}\,. (97)

This formula facilitates the real-space analysis of causality for relativistic fluids with a conserved global U(1)U(1) charge. When the principal parts of the hydrodynamic equations from Appendix A are inserted into (B), one finds the same causality constraints as stated there.

Appendix C Matching Conditions

An alternative, indirect approach to fixing the zero-modes that arise from the linearized collision operator are so-called “matching conditions”. For example, in order to fix the zero modes in such a way as to arive at the Landau frame, one could impose that the corrections to the energy density are zero, i.e.

ϵ=p(pu)2𝐟(1±𝐟)ϕp=0.{\cal E}-\epsilon=\int_{p}(p{\cdot}u)^{2}{\bf f}\left(1\pm{\bf f}\right)\phi_{p}=0\,. (1)

This has the effect of tuning the zero modes such that =ϵ\mathcal{E}=\epsilon. Similarly, one may tune to zero the corrections to the charge density

𝒩n=p(pu)𝐟(1±𝐟)ϕp=0,{\cal N}-n=-\int_{p}(p{\cdot}u){\bf f}\left(1\pm{\bf f}\right)\phi_{p}=0\,, (2)

and the heat current

𝒬μ=p(pu)pμ𝐟(1±𝐟)ϕp=0.{\cal Q}^{\mu}=-\int_{p}(p{\cdot}u)p_{\perp}^{\mu}{\bf f}\left(1\pm{\bf f}\right)\phi_{p}=0\,. (3)

These matching conditions give only one out of an infinite number of possible hydrodynamic “frames”. A generalization of these constraints in order to generate causal “frames” has been proposed in ref. Bemfica:2017wps ; Rocha:2021lze , reading

p(pu)r𝐟(1±𝐟)ϕp\displaystyle\int_{p}(p{\cdot}u)^{r}{\bf f}\left(1\pm{\bf f}\right)\phi_{p} =0,\displaystyle=0, (4a)
p(pu)s𝐟(1±𝐟)ϕp\displaystyle\int_{p}(p{\cdot}u)^{s}{\bf f}\left(1\pm{\bf f}\right)\phi_{p} =0,\displaystyle=0, (4b)
p(pu)tpμ𝐟(1±𝐟)ϕp\displaystyle\int_{p}(p{\cdot}u)^{t}p_{\perp}^{\mu}{\bf f}\left(1\pm{\bf f}\right)\phi_{p} =0,\displaystyle=0, (4c)

where rsr\neq s, and r,s,tr,s,t are non-negative integers. While the physical meaning of setting to zero the quantities that do not appear in the constitutive relations is not immediately clear, the real question is how the matching conditions (4) are related to the hydrodynamic field redefinitions which give rise to causal “frames”.

The correction to the equilibrium distribution function is given by eq. (41),

ϕp=a(x)+bμ(x)pμ+Φp(x),\phi_{p}=a(x)+b_{\mu}(x){p^{\mu}}+\Phi_{p}(x)\,, (5)

where Φp\Phi_{p} is the inhomogeneous part of the solution, and aa, bμb_{\mu} are the space- and time-dependent parts of the zero modes. Substituting this ϕp\phi_{p} into (4), we find

a\displaystyle a =(pu)rΦp(pu)s+1(pu)r+1(pu)sΦp(pu)r+1(pu)s(pu)r(pu)s+1,\displaystyle=\frac{\langle(p{\cdot}u)^{r}\Phi_{p}\rangle\langle(p{\cdot}u)^{s+1}\rangle-\langle(p{\cdot}u)^{r+1}\rangle\langle(p{\cdot}u)^{s}\Phi_{p}\rangle}{\langle(p{\cdot}u)^{r+1}\rangle\langle(p{\cdot}u)^{s}\rangle-\langle(p{\cdot}u)^{r}\rangle\langle(p{\cdot}u)^{s+1}\rangle}\,, (6a)
bu\displaystyle b{\cdot}u =(pu)rΦp(pu)s(pu)r(pu)sΦp(pu)r+1(pu)s(pu)r(pu)s+1,\displaystyle=\frac{\langle(p{\cdot}u)^{r}\Phi_{p}\rangle\langle(p{\cdot}u)^{s}\rangle-\langle(p{\cdot}u)^{r}\rangle\langle(p{\cdot}u)^{s}\Phi_{p}\rangle}{\langle(p{\cdot}u)^{r+1}\rangle\langle(p{\cdot}u)^{s}\rangle-\langle(p{\cdot}u)^{r}\rangle\langle(p{\cdot}u)^{s+1}\rangle}\,, (6b)
bν\displaystyle b_{\nu}^{\perp} =(pu)tpμΦp1d(pu)tp2,\displaystyle=-\frac{\langle(p{\cdot}u)^{t}p^{\mu}_{\perp}\Phi_{p}\rangle}{\frac{1}{d}\langle(p{\cdot}u)^{t}p_{\perp}^{2}\rangle}\,, (6c)

where =p()𝐟(1±𝐟)\langle...\rangle=\int_{p}\left(...\right){\bf f}(1\pm{\bf f}). Clearly, one needs to know the inhomogeneous solution Φp\Phi_{p} in order to relate aa and bμb_{\mu} to rr, ss, and tt. The form of Φp\Phi_{p} depends on how one chooses to impose the perfect-fluid constraint. Let’s say we choose to eliminate the time derivatives as in eq. (51),

(1±𝐟p)Φp=Kηpμpνσμν[u]+Kζu+Kαpμμα.\displaystyle(1\pm{\bf f}_{p})\Phi_{p}=K_{\eta}p^{\mu}p^{\nu}\sigma_{\mu\nu}[{u}]+K_{\zeta}\partial{\cdot}{u}+K_{\alpha}p^{\mu}\partial_{\mu}^{\perp}{\alpha}\,. (7)

For massless particles Kζ=0K_{\zeta}=0, and (6) implies that a=bu=0a=b{\cdot}u=0. In other words, once the perfect-fluid constraint has been imposed when finding the inhomogeneous solution Φp\Phi_{p}, hydrodynamic field redefinitions can not generate causal frames because the latter require non-zero transport parameters in the scalar sector. Put differently, conditions (6) imply that once the frame-invariants fif_{i} vanish, the transport parameters εi,πi,νi\varepsilon_{i},\pi_{i},\nu_{i} must vanish as well, which is inconsistent with causal frames in first-order conformal hydrodynamics.

Similarly, for massive particles with Kζ0K_{\zeta}\neq 0, eqs. (7) and (6) imply

a\displaystyle a =(0)T˙+(non-zero)u+(0)α˙,\displaystyle=(0)\dot{T}+\left(\textrm{non-zero}\right)\partial{\cdot}u+(0)\dot{\alpha}\,, (8a)
bu\displaystyle b{\cdot}u =(0)T˙+(non-zero)u+(0)α˙.\displaystyle=(0)\dot{T}+\left(\textrm{non-zero}\right)\partial{\cdot}u+(0)\dot{\alpha}\,. (8b)

Again, we see that by fixing the zero modes via matching conditions (4), one is unable to generate a suitable mix of time- and space-derivatives required for hyperbolicity and causality.

The only way to generate a causal frame via the matching conditions (4) would be if Φp\Phi_{p} contained independent functions multiplying T˙/T\dot{T}/T, u\partial{\cdot}u, α˙\dot{\alpha} in the scalar sector. However, as the source term of the linearized Boltzmann equation must obey the perfect-fluid constraints, only one of these three functions is allowed in the inhomogeneous solution. The issue may be alleviated by taking moments of the full Boltzmann equation, as was done in Rocha:2021lze to study non-hydrodynamic contributions.

References

  • (1) C. Eckart, The thermodynamics of irreversible processes. III. Relativistic theory of the simple fluid, Phys. Rev. 58 (1940) 919.
  • (2) L.D. Landau and E.M. Lifshitz, Fluid Mechanics, Pergamon (1987).
  • (3) W.A. Hiscock and L. Lindblom, Generic instabilities in first-order dissipative relativistic fluid theories, Phys.Rev. D31 (1985) 725.
  • (4) W.A. Hiscock and L. Lindblom, Linear plane waves in dissipative relativistic fluids, Phys. Rev. D35 (1987) 3723.
  • (5) I. Müller, Zum paradoxon der wärmeleitungstheorie, Zeitschrift für Physik 198 (1967) 329.
  • (6) W. Israel, Nonstationary irreversible thermodynamics: A Causal relativistic theory, Annals Phys. 100 (1976) 310.
  • (7) W. Israel and J.M. Stewart, Thermodynamics of nonstationary and transient effects in a relativistic gas, Phys. Lett. A 58 (1976) 213.
  • (8) F.S. Bemfica, M.M. Disconzi, V. Hoang, J. Noronha and M. Radosz, Nonlinear Constraints on Relativistic Fluids Far from Equilibrium, Phys. Rev. Lett. 126 (2021) 222301 [2005.11632].
  • (9) F.S. Bemfica, M.M. Disconzi and J. Noronha, Causality and existence of solutions of relativistic viscous fluid dynamics with gravity, Phys. Rev. D98 (2018) 104064 [1708.06255].
  • (10) P. Kovtun, First-order relativistic hydrodynamics is stable, JHEP 10 (2019) 034 [1907.08191].
  • (11) F.S. Bemfica, M.M. Disconzi and J. Noronha, Nonlinear Causality of General First-Order Relativistic Viscous Hydrodynamics, Phys. Rev. D100 (2019) 104020 [1907.12695].
  • (12) R.E. Hoult and P. Kovtun, Stable and causal relativistic Navier-Stokes equations, JHEP 06 (2020) 067 [2004.04102].
  • (13) F.S. Bemfica, M.M. Disconzi and J. Noronha, General-Relativistic Viscous Fluid Dynamics, 2009.11388.
  • (14) J. Noronha, M. Spaliński and E. Speranza, Transient Relativistic Fluid Dynamics in a General Hydrodynamic Frame, 2105.01034.
  • (15) A. Pandya and F. Pretorius, Numerical exploration of first-order relativistic hydrodynamics, Phys. Rev. D 104 (2021) 023015 [2104.00804].
  • (16) O. Aharony, S.S. Gubser, J.M. Maldacena, H. Ooguri and Y. Oz, Large N field theories, string theory and gravity, Phys. Rept. 323 (2000) 183 [hep-th/9905111].
  • (17) P.M. Chesler and L.G. Yaffe, Numerical solution of gravitational dynamics in asymptotically anti-de Sitter spacetimes, JHEP 07 (2014) 086 [1309.1439].
  • (18) S. Bhattacharyya, V.E. Hubeny, S. Minwalla and M. Rangamani, Nonlinear Fluid Dynamics from Gravity, JHEP 02 (2008) 045 [0712.2456].
  • (19) S. De Groot, W. Van Leeuwen and C. Van Weert, Relativistic Kinetic Theory. Principles and Applications, North-Holland (1980).
  • (20) C. Cercignani and G.M. Kremer, The Relativistic Boltzmann Equation: Theory and Applications, Springer (2002).
  • (21) G.S. Rocha, G.S. Denicol and J. Noronha, Novel Relaxation Time Approximation to the Relativistic Boltzmann Equation, Phys. Rev. Lett. 127 (2021) 042301 [2103.07489].
  • (22) P. Kovtun, Lectures on hydrodynamic fluctuations in relativistic theories, J. Phys. A45 (2012) 473001 [1205.5040].
  • (23) K. Jensen, M. Kaminski, P. Kovtun, R. Meyer, A. Ritz and A. Yarom, Towards hydrodynamics without an entropy current, Phys. Rev. Lett. 109 (2012) 101601 [1203.3556].
  • (24) J. Erdmenger, M. Haack, M. Kaminski and A. Yarom, Fluid dynamics of R-charged black holes, JHEP 01 (2009) 055 [0809.2488].
  • (25) N. Banerjee, J. Bhattacharya, S. Bhattacharyya, S. Dutta, R. Loganayagam and P. Surowka, Hydrodynamics from charged black branes, JHEP 01 (2011) 094 [0809.2596].
  • (26) V.E. Hubeny, S. Minwalla and M. Rangamani, The fluid/gravity correspondence, in Theoretical Advanced Study Institute in Elementary Particle Physics: String theory and its Applications: From meV to the Planck Scale, pp. 348–383, 2012 [1107.5780].
  • (27) R. Courant and D. Hilbert, Methods of Mathematical Physics II. Partial Differential Equations, Wiley (1989).
  • (28) G.S. Rocha and G.S. Denicol, Transient fluid dynamics with general matching conditions: A first study from the method of moments, Phys. Rev. D 104 (2021) 096016 [2108.02187].