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One-Point Functions from Variation

The renormalized on-shell action is useful because it is a generating functional. Once the divergent terms have been subtracted, one-point functions are obtained by variation with respect to sources.

This page gives the practical variational dictionary. The main idea is:

holographic vevrenormalized radial canonical momentum.\text{holographic vev} \quad\longleftrightarrow\quad \text{renormalized radial canonical momentum}.

The word “renormalized” is essential. The raw canonical momentum at the cutoff surface diverges. Counterterms supply local subtraction terms. The finite limit is the one-point function, with a sign fixed by the source convention.

Sources are fixed at the conformal boundary. The bulk solution and interior condition determine the response. The regulated canonical momentum plus counterterm contribution has a finite limit, which gives the vev.

One-point functions are obtained from finite variations of SrenS_{\rm ren}. The boundary source fixes the leading asymptotic data. The interior condition selects the response. The raw cutoff momentum Πreg\Pi_{\rm reg} is divergent, but Πreg+Πct\Pi_{\rm reg}+\Pi_{\rm ct} has a finite limit. That finite renormalized momentum is the holographic vev, up to the sign convention relating WCFTW_{\rm CFT} to SrenS_{\rm ren}.

Most holographic computations eventually ask for one of the following quantities:

  • the scalar condensate O\langle\mathcal O\rangle;
  • the charge density or current Ji\langle J^i\rangle;
  • the energy density, pressure, or stress tensor Tij\langle T^{ij}\rangle;
  • the response of a state to a deformation;
  • the Ward identities obeyed by a background solution.

All of these come from varying SrenS_{\rm ren}. This is the safe rule. Reading off a subleading coefficient is a useful shortcut only after the variational normalization and counterterms are understood.

The computation has two layers:

δSren,on-shellrenormalized canonical momenta,\delta S_{\text{ren,on-shell}} \quad\Rightarrow\quad \text{renormalized canonical momenta},

and

WCFTSren,on-shellCFT one-point functions.W_{\rm CFT}\approx -S_{\text{ren,on-shell}} \quad\Rightarrow\quad \text{CFT one-point functions}.

The first layer is bulk mechanics. The second layer is the AdS/CFT sign and source convention.

Let the boundary theory live on a metric representative g(0)ijg_{(0)ij}. Let a scalar source ϕ(0)\phi_{(0)} couple to O\mathcal O, a background gauge field A(0)iA_{(0)i} couple to JiJ^i, and the metric source the stress tensor.

With the Euclidean convention

SESEddxg(0)ϕ(0)Oddxg(0)A(0)iJi+,S_E \to S_E- \int d^d x\sqrt{g_{(0)}}\,\phi_{(0)}\mathcal O - \int d^d x\sqrt{g_{(0)}}\,A_{(0)i}J^i+ \cdots,

the generating functional is

WCFT=logZCFT.W_{\rm CFT}=\log Z_{\rm CFT}.

Its variation is

δWCFT=ddxg(0)[Oδϕ(0)+JiδA(0)i+12Tijδg(0)ij+].\delta W_{\rm CFT} = \int d^d x\sqrt{g_{(0)}} \left[ \langle\mathcal O\rangle\delta\phi_{(0)} + \langle J^i\rangle\delta A_{(0)i} + \frac12\langle T^{ij}\rangle\delta g_{(0)ij} +\cdots \right].

Equivalently,

O(x)=1g(0)δWCFTδϕ(0)(x),\langle\mathcal O(x)\rangle = \frac{1}{\sqrt{g_{(0)}}} \frac{\delta W_{\rm CFT}}{\delta\phi_{(0)}(x)}, Ji(x)=1g(0)δWCFTδA(0)i(x),\langle J^i(x)\rangle = \frac{1}{\sqrt{g_{(0)}}} \frac{\delta W_{\rm CFT}}{\delta A_{(0)i}(x)},

and

Tij(x)=2g(0)δWCFTδg(0)ij(x).\langle T^{ij}(x)\rangle = \frac{2}{\sqrt{g_{(0)}}} \frac{\delta W_{\rm CFT}}{\delta g_{(0)ij}(x)}.

In the classical Euclidean holographic limit used here,

WCFTSren,on-shell.W_{\rm CFT} \approx -S_{\text{ren,on-shell}}.

Therefore

O=1g(0)δSren,on-shellδϕ(0)\boxed{ \langle\mathcal O\rangle = - \frac{1}{\sqrt{g_{(0)}}} \frac{\delta S_{\text{ren,on-shell}}}{\delta\phi_{(0)}} }

and similarly for currents and the stress tensor. Many papers use different Euclidean source signs or Lorentzian conventions. The invariant statement is that one-point functions are finite renormalized momenta conjugate to sources.

Let Ψ\Psi denote a bulk field. On a classical solution, the variation of the regulated action reduces to a cutoff-surface term:

δSreg,on-shell=ΣϵddxγΠregΨδΨ.\delta S_{\text{reg,on-shell}} = \int_{\Sigma_\epsilon}d^d x\sqrt\gamma\,\Pi_{\rm reg}^{\Psi}\delta\Psi.

The regulated momentum ΠregΨ\Pi_{\rm reg}^{\Psi} is the radial canonical momentum conjugate to Ψ\Psi. It usually diverges as ϵ0\epsilon\to0. The counterterm action contributes

δSct,ϵ=ΣϵddxγΠctΨδΨ.\delta S_{{\rm ct},\epsilon} = \int_{\Sigma_\epsilon}d^d x\sqrt\gamma\,\Pi_{\rm ct}^{\Psi}\delta\Psi.

Thus

ΠrenΨ=limϵ0(appropriate rescaling of ΠregΨ+ΠctΨ)\Pi_{\rm ren}^{\Psi} = \lim_{\epsilon\to0} \left( \text{appropriate rescaling of } \Pi_{\rm reg}^{\Psi}+\Pi_{\rm ct}^{\Psi} \right)

is finite. The “appropriate rescaling” converts variations of cutoff fields into variations of finite sources. For a scalar,

ϕ(ϵ,x)ϵdΔϕ(0)(x),\phi(\epsilon,x) \sim \epsilon^{d-\Delta}\phi_{(0)}(x),

so

δϕ(ϵ,x)ϵdΔδϕ(0)(x).\delta\phi(\epsilon,x) \sim \epsilon^{d-\Delta}\delta\phi_{(0)}(x).

For the metric,

γij(ϵ,x)L2ϵ2g(0)ij(x),\gamma_{ij}(\epsilon,x) \sim \frac{L^2}{\epsilon^2}g_{(0)ij}(x),

so one must rescale the Brown–York tensor before taking the boundary limit.

Take again the scalar action

Sϕ=Nϕ2dd+1xg(gMNMϕNϕ+m2ϕ2).S_\phi = \frac{\mathcal N_\phi}{2} \int d^{d+1}x\sqrt g \left( g^{MN}\partial_M\phi\partial_N\phi+m^2\phi^2 \right).

The regulated radial momentum is

Πreg=NϕnMMϕ.\Pi_{\rm reg} = \mathcal N_\phi n^M\partial_M\phi.

The near-boundary expansion in standard quantization is

ϕ(z,x)=zdΔ(ϕ(0)+z2ϕ(2)+)+zΔ(A+).\phi(z,x) = z^{d-\Delta} \left( \phi_{(0)}+z^2\phi_{(2)}+\cdots \right) + z^\Delta \left(A+\cdots\right).

After adding the scalar counterterms and varying with respect to the finite source, one obtains the schematic but very useful result

O(x)=Nϕ(2Δd)A(x)+local terms in sources\boxed{ \langle\mathcal O(x)\rangle = \mathcal N_\phi(2\Delta-d)A(x) + \text{local terms in sources} }

with the Euclidean source convention used in this course.

The local terms are determined by counterterms and possible logarithms. They vanish in many simple flat-boundary examples with constant or zero sources, but they are not optional in general.

A useful mnemonic is:

2Δd=Δ+Δ.2\Delta-d = \Delta_+-\Delta_-.

The factor multiplying AA is the difference between the two radial exponents. It comes from the radial derivative in the canonical momentum.

A particularly important case is a normalizable scalar profile with no source:

ϕ(0)=0,ϕ(z,x)=zΔA(x)+.\phi_{(0)}=0, \qquad \phi(z,x)=z^\Delta A(x)+\cdots.

Then, if no local source terms contribute,

O(x)=Nϕ(2Δd)A(x).\langle\mathcal O(x)\rangle = \mathcal N_\phi(2\Delta-d)A(x).

This is how many holographic condensates are identified. However, “source-free” must be checked in the correct quantization and scheme. In alternate quantization, or in the presence of mixed boundary conditions, the meaning of source and vev changes.

For a bulk Maxwell field,

SA=14gd+12dd+1xgFMNFMNS_A = \frac{1}{4g_{d+1}^2} \int d^{d+1}x\sqrt g\,F_{MN}F^{MN}

in Euclidean signature. On shell, the variation contains

δSA=1gd+12ΣϵddxγnMFMiδAi\delta S_A = \frac{1}{g_{d+1}^2} \int_{\Sigma_\epsilon}d^d x\sqrt\gamma\, n_M F^{Mi}\delta A_i

up to signs fixed by the orientation convention. Counterterms may contribute local pieces, especially in special dimensions.

The boundary source is

Ai(z,x)=A(0)i(x)+.A_i(z,x)=A_{(0)i}(x)+\cdots.

The current expectation value is

Ji(x)=1g(0)δSrenδA(0)i(x)\boxed{ \langle J^i(x)\rangle = - \frac{1}{\sqrt{g_{(0)}}} \frac{\delta S_{\rm ren}}{\delta A_{(0)i}(x)} }

with the Euclidean convention W=SrenW=-S_{\rm ren}.

In many finite-density solutions one writes

At(z)=μρzd2+.A_t(z)=\mu-\rho z^{d-2}+\cdots.

Then μ\mu is the chemical potential and ρ\rho is proportional to the charge density. The proportionality depends on the Maxwell normalization, the dimension, and counterterm conventions. The variational formula is what fixes it.

The boundary metric is the source for the stress tensor. The holographic stress tensor is

Tij=2g(0)δSrenδg(0)ij\boxed{ \langle T^{ij}\rangle = - \frac{2}{\sqrt{g_{(0)}}} \frac{\delta S_{\rm ren}}{\delta g_{(0)ij}} }

in the same Euclidean convention. In Lorentzian conventions many authors absorb the sign into the definition of the Brown–York tensor.

At the cutoff surface, the regulated Brown–York tensor is built from the extrinsic curvature:

TBY,ϵij1κd+12(KijKγij),T_{{\rm BY},\epsilon}^{ij} \sim \frac{1}{\kappa_{d+1}^2} \left( K^{ij}-K\gamma^{ij} \right),

with signs depending on the convention for the gravitational action and the normal vector. The counterterms contribute local curvature terms. The renormalized stress tensor is obtained by adding these terms and rescaling to the finite boundary metric.

For asymptotically AdS solutions in Fefferman–Graham gauge,

gij(z,x)=g(0)ij++zdg(d)ij+zdlogz2h(d)ij+.g_{ij}(z,x) = g_{(0)ij}+\cdots+z^d g_{(d)ij}+z^d\log z^2\,h_{(d)ij}+\cdots.

The expectation value has the schematic form

Tij=dLd12κd+12g(d)ij+local curvature and source terms.\langle T_{ij}\rangle = \frac{dL^{d-1}}{2\kappa_{d+1}^2}g_{(d)ij} + \text{local curvature and source terms}.

The local terms include anomaly contributions in even boundary dimension. For flat-boundary black branes, they are often absent or simple, so g(d)ijg_{(d)ij} directly gives energy density and pressure.

One-point functions are not arbitrary. Symmetries of the renormalized action imply Ward identities.

If SrenS_{\rm ren} is invariant under boundary gauge transformations

δA(0)i=iα,\delta A_{(0)i}=\nabla_i\alpha,

then

iJi=0\nabla_i\langle J^i\rangle=0

when there are no charged scalar sources. With charged sources, the right-hand side contains the explicit symmetry-breaking terms produced by those sources.

Under a boundary diffeomorphism generated by ξi\xi^i,

δg(0)ij=iξj+jξi,δϕ(0)=ξiiϕ(0),δA(0)i=LξA(0)i.\delta g_{(0)ij}=\nabla_i\xi_j+\nabla_j\xi_i, \qquad \delta\phi_{(0)}=\xi^i\partial_i\phi_{(0)}, \qquad \delta A_{(0)i}=\mathcal L_\xi A_{(0)i}.

Invariance gives the schematic identity

iT ji=Ojϕ(0)+F(0)jiJi+.\nabla_i\langle T^i_{\ j}\rangle = \langle\mathcal O\rangle\partial_j\phi_{(0)} + F_{(0)ji}\langle J^i\rangle + \cdots.

The stress tensor is conserved only when external sources do not inject momentum.

Under a boundary Weyl transformation,

δg(0)ij=2σg(0)ij,δϕ(0)=(Δd)σϕ(0),\delta g_{(0)ij}=2\sigma g_{(0)ij}, \qquad \delta\phi_{(0)}=(\Delta-d)\sigma\phi_{(0)},

one obtains

T ii=(dΔ)ϕ(0)O+A+.\langle T^i_{\ i}\rangle = (d-\Delta)\phi_{(0)}\langle\mathcal O\rangle +\mathcal A + \cdots.

Here A\mathcal A is the conformal anomaly. In odd boundary dimensions and without anomaly-generating sources, A\mathcal A is often zero.

These Ward identities are among the best checks of a holographic computation. If your counterterms or normalizations are wrong, the Ward identities usually know before you do.

For a classical solution, use the following workflow:

  1. Choose the sources. Identify g(0)ijg_{(0)ij}, ϕ(0)\phi_{(0)}, A(0)iA_{(0)i}, and any other boundary data.
  2. Solve the bulk equations. Impose the correct interior condition: regularity, incoming waves, horizon smoothness, or another state/ensemble condition.
  3. Expand near the boundary. Determine the coefficients through the order that contributes to the desired vev.
  4. Write the regulated variation. Compute the radial canonical momentum at z=ϵz=\epsilon.
  5. Add counterterm variations. Include Πct\Pi_{\rm ct}, not only SctS_{\rm ct}.
  6. Convert to source variations. Replace variations of cutoff fields by variations of finite sources.
  7. Take ϵ0\epsilon\to0. Extract the finite renormalized momentum.
  8. Apply the W=SrenW=-S_{\rm ren} sign. Translate the bulk variation into the CFT one-point function.
  9. Check Ward identities. Conservation, trace, and gauge identities are strong consistency tests.

This algorithm is more reliable than memorizing coefficient rules.

Example: flat-boundary scalar with no source derivatives

Section titled “Example: flat-boundary scalar with no source derivatives”

Suppose the source is slowly varying or constant enough that derivative counterterms do not contribute, and ignore logarithmic cases. The scalar expansion is

ϕ(z,x)=zdΔϕ(0)(x)+zΔA(x)+.\phi(z,x)=z^{d-\Delta}\phi_{(0)}(x)+z^\Delta A(x)+\cdots.

The renormalized variation has the finite form

δSren,on-shell=Nϕ(2Δd)ddxg(0)A(x)δϕ(0)(x)+local source terms.\delta S_{\text{ren,on-shell}} = - \mathcal N_\phi(2\Delta-d) \int d^d x\sqrt{g_{(0)}}\,A(x)\delta\phi_{(0)}(x) + \text{local source terms}.

Therefore

O(x)=Nϕ(2Δd)A(x)+local source terms.\langle\mathcal O(x)\rangle = \mathcal N_\phi(2\Delta-d)A(x) + \text{local source terms}.

The sign in the first equation is compensated by W=SrenW=-S_{\rm ren}.

For an asymptotically AdS black brane with flat boundary metric, the near-boundary metric contains a coefficient g(d)ijg_{(d)ij} determined by the horizon scale. The holographic stress tensor is proportional to g(d)ijg_{(d)ij}:

Tij=dLd12κd+12g(d)ij\langle T_{ij}\rangle = \frac{dL^{d-1}}{2\kappa_{d+1}^2}g_{(d)ij}

up to signs and index placements fixed by the metric convention, and up to local terms that vanish for flat sources.

For a conformal plasma, the result must obey

T ii=0,ϵ=(d1)p,\langle T^i_{\ i}\rangle=0, \qquad \epsilon=(d-1)p,

when no anomaly or deformation is present. This provides a quick check of the calculation.

Example: chemical potential and charge density

Section titled “Example: chemical potential and charge density”

For a finite-density state, the near-boundary Maxwell field is often written as

At(z)=μρzd2+.A_t(z)=\mu-\rho z^{d-2}+\cdots.

The source is μ\mu. The response is the electric flux. The current is not defined by the symbol ρ\rho alone; it is defined by

Jt=1g(0)δSrenδA(0)t.\langle J^t\rangle = - \frac{1}{\sqrt{g_{(0)}}} \frac{\delta S_{\rm ren}}{\delta A_{(0)t}}.

For simple Maxwell normalizations and flat boundary sources, this is proportional to ρ\rho. In complicated models with Chern–Simons terms, dilaton couplings, or finite counterterms, the flux formula must be modified accordingly.

The variational dictionary is:

SourceBulk fieldRenormalized momentumBoundary one-point function
scalar source ϕ(0)\phi_{(0)}scalar ϕ\phifinite scalar radial momentumO\langle\mathcal O\rangle
gauge field A(0)iA_{(0)i}bulk gauge field AiA_ifinite electric fluxJi\langle J^i\rangle
metric g(0)ijg_{(0)ij}bulk metric gMNg_{MN}renormalized Brown–York tensorTij\langle T^{ij}\rangle

The most compact formula is

δSren,on-shell=δWCFT\delta S_{\text{ren,on-shell}} = - \delta W_{\rm CFT}

in Euclidean signature with the source convention used here.

“The vev is always the coefficient of zΔz^\Delta.”

Section titled ““The vev is always the coefficient of zΔz^\DeltazΔ.””

Only after choosing standard quantization, fixing the normalization, adding counterterms, and accounting for local terms. The zΔz^\Delta coefficient is often the state-dependent part of the answer, but the actual definition is variational.

“A nonzero normalizable mode always means spontaneous symmetry breaking.”

Section titled ““A nonzero normalizable mode always means spontaneous symmetry breaking.””

No. It means a nonzero expectation value for the dual operator, provided the source is zero in the chosen quantization. To call it spontaneous symmetry breaking, the operator must transform under a symmetry and the source must not explicitly break that symmetry.

“The electric flux is automatically the charge density.”

Section titled ““The electric flux is automatically the charge density.””

It is the charge density after normalization and counterterm choices are accounted for. In the presence of Chern–Simons terms or higher-derivative interactions, the correct conserved current can differ from the naive Maxwell flux.

“The stress tensor is just g(d)ijg_{(d)ij}.”

Section titled ““The stress tensor is just g(d)ijg_{(d)ij}g(d)ij​.””

The coefficient g(d)ijg_{(d)ij} is the nonlocal state-dependent part, but local curvature terms and anomaly terms can contribute. For flat boundary metrics these local terms often vanish, which is why the shortcut is so tempting.

“Ward identities are extra assumptions.”

Section titled ““Ward identities are extra assumptions.””

They are consequences of the invariance of SrenS_{\rm ren} under boundary gauge transformations, diffeomorphisms, and Weyl transformations. They are built into the bulk constraints.

Exercise 1: Scalar momentum and the factor 2Δd2\Delta-d

Section titled “Exercise 1: Scalar momentum and the factor 2Δ−d2\Delta-d2Δ−d”

Assume

ϕ(z,x)=zdΔϕ(0)(x)+zΔA(x)+\phi(z,x)=z^{d-\Delta}\phi_{(0)}(x)+z^\Delta A(x)+\cdots

and ignore derivative counterterms. Explain why the finite vev is proportional to (2Δd)A(2\Delta-d)A rather than simply to AA.

Solution

The two independent exponents are

Δ=dΔ,Δ+=Δ.\Delta_-=d-\Delta, \qquad \Delta_+=\Delta.

The radial canonical momentum involves a radial derivative, so it distinguishes the two powers. After subtracting the divergent source-branch contribution, the finite cross-term in the variation is proportional to the difference

Δ+Δ=Δ(dΔ)=2Δd.\Delta_+-\Delta_-=\Delta-(d-\Delta)=2\Delta-d.

Thus, with action normalization Nϕ\mathcal N_\phi,

O=Nϕ(2Δd)A+local source terms\langle\mathcal O\rangle = \mathcal N_\phi(2\Delta-d)A + \text{local source terms}

in the Euclidean convention of this course.

Exercise 2: Current conservation from gauge invariance

Section titled “Exercise 2: Current conservation from gauge invariance”

Let

δW=ddxg(0)JiδA(0)i.\delta W=\int d^d x\sqrt{g_{(0)}}\,\langle J^i\rangle\delta A_{(0)i}.

Assume WW is invariant under δA(0)i=iα\delta A_{(0)i}=\nabla_i\alpha for arbitrary α(x)\alpha(x). Derive iJi=0\nabla_i\langle J^i\rangle=0.

Solution

Gauge invariance gives

0=δW=ddxg(0)Jiiα.0=\delta W =\int d^d x\sqrt{g_{(0)}}\,\langle J^i\rangle\nabla_i\alpha.

Integrating by parts and ignoring boundary terms on the boundary spacetime,

0=ddxg(0)αiJi.0= - \int d^d x\sqrt{g_{(0)}}\,\alpha\nabla_i\langle J^i\rangle.

Since α(x)\alpha(x) is arbitrary,

iJi=0.\nabla_i\langle J^i\rangle=0.

Exercise 3: Trace Ward identity with a scalar source

Section titled “Exercise 3: Trace Ward identity with a scalar source”

Suppose a scalar source has dimension dΔd-\Delta. Under an infinitesimal Weyl transformation with the source treated as a spurion,

δg(0)ij=2σg(0)ij,δϕ(0)=(Δd)σϕ(0).\delta g_{(0)ij}=2\sigma g_{(0)ij}, \qquad \delta\phi_{(0)}=(\Delta-d)\sigma\phi_{(0)}.

Using the variation of WW, derive the trace identity without an anomaly.

Solution

The Weyl variation of WW is

δW=ddxg(0)[12Tij(2σg(0)ij)+O(Δd)σϕ(0)].\delta W = \int d^d x\sqrt{g_{(0)}} \left[ \frac12\langle T^{ij}\rangle(2\sigma g_{(0)ij}) + \langle\mathcal O\rangle(\Delta-d)\sigma\phi_{(0)} \right].

Therefore

δW=ddxg(0)σ[T ii+(Δd)ϕ(0)O].\delta W = \int d^d x\sqrt{g_{(0)}}\,\sigma \left[ \langle T^i_{\ i}\rangle +(\Delta-d)\phi_{(0)}\langle\mathcal O\rangle \right].

With the variation convention above, Weyl invariance gives

T ii=(dΔ)ϕ(0)O.\langle T^i_{\ i}\rangle =(d-\Delta)\phi_{(0)}\langle\mathcal O\rangle.

The important point is that a dimensionful source explicitly breaks Weyl invariance and appears in the trace Ward identity. An anomaly term should be added when logarithmic counterterms are present.

Exercise 4: Why finite counterterms affect one-point functions

Section titled “Exercise 4: Why finite counterterms affect one-point functions”

Let

Sfinite=cddxg(0)ϕ(0)2.S_{\rm finite}=c\int d^d x\sqrt{g_{(0)}}\,\phi_{(0)}^2.

How does this change O\langle\mathcal O\rangle in the convention W=SrenW=-S_{\rm ren}?

Solution

The finite counterterm changes the renormalized action by

ΔSren=cddxg(0)ϕ(0)2.\Delta S_{\rm ren}=c\int d^d x\sqrt{g_{(0)}}\,\phi_{(0)}^2.

Thus

1g(0)δΔSrenδϕ(0)=2cϕ(0).\frac{1}{\sqrt{g_{(0)}}} \frac{\delta \Delta S_{\rm ren}}{\delta\phi_{(0)}} =2c\phi_{(0)}.

Since W=SrenW=-S_{\rm ren},

ΔO=2cϕ(0).\Delta\langle\mathcal O\rangle =-2c\phi_{(0)}.

This is a local scheme-dependent shift. It changes contact terms and local one-point-function pieces, not the nonlocal part of correlators at separated points.