δN formalism
Misao SasakiMisao Sasaki
Yukawa Institute for Theoretical Physics
Yukawa Institute for Theoretical Physics
Kyoto University
Kyoto University
contents
1. Introduction
2. Linear perturbation theory
3. Linear δN formula
4. Non-linear extension
5. Non-linear ∆N formula
6. Conservation of nonlinear curvature perturbation
7. δN for ‘slowroll’ inflation
• M. Sasaki and E.D. Stewart,
A General analytic formula for the spectral index of the density perturbations produced during inflation,
Prog. Theor. Phys. 95, 71 (1996) [astro-ph/9507001].
• M. Sasaki and T. Tanaka,
Superhorizon scale dynamics of multiscalar inflation, Prog. Theor. Phys. 99, 763 (1998) [gr-qc/9801017].
• D.H. Lyth, K.A. Malik and M. Sasaki,
A General proof of the conservation of the curvature perturbation, JCAP 0505, 004 (2005) [astro-ph/0411220].
• A. Naruko and M. Sasaki,
Conservation of the nonlinear curvature perturbation in generic single-field inflation, Class. Quant. Grav. 28, 072001 (2011) [arXiv:1101.3180 [astro-ph.CO]].
• J.-O. Gong, J.-c. Hwang, W.-I. Park, M. Sasaki and Y.-S. Song, Conformal invariance of curvature perturbation,
JCAP 1109 (2011) 023 [arXiv:1107.1840 [gr-qc]].
a (highly biased) list of references
linear
quasi-nonlinear / separate universe approach
nonlinear
1. Introduction
Standard (single-field, slowroll) inflation predicts almost scale-invariant Gaussian curvature perturbations.
CMB (WMAP,PLANCK,...) is consistent with the prediction. Linear perturbation theory seems to be valid.
PLANCK 2013
PLANCK 2013
l
δ
δ
N
N
formalism for curvature perturbations
formalism for curvature perturbations
Φ=Φgauss+ fNLΦ2
gauss+ ∙∙∙
Tensor perturbations (gravitational waves) have not been detected yet.
Future CMB experiments may still detect non-Gaussianity...
M
Models need to be tested.
multi-field, non-slowroll, string theory, vacuum bubbles, … -8.9< fNL<14.3 (95%CL)
r<0.11 (95%CL) PLANCK 2013
tensor-scalar ratio:
(-)gravitational potential:
However, nature may be a bit more complicated...
PLANCK 2013
What is δN ?
•• δN is the perturbation in # of e-folds counted
backward in time from a fixed final time tf
•
δN is equal to conserved NL comoving curvatureperturbation RNLon superhorizon scales at t>tf •
• tf should be chosen such that the evolution of the universe has become unique by that time.
• δN formula is valid independent of theory of gravity
therefore it is nonlocal in time by definition
isocurvature perturbation that persists until t=tf must be dealt separately
“
3 types of δN
originally adiabatic end of/after inflation entropy/isocurvature → adiabatic f t = t φ1 φ22. Linear perturbation theory
(
)
( )
2 2 2
1 2
t(1 2 )
ij ij i jds
= − +
A dt
+
a
+
R
δ
+
H
dx dx
• propertime along xi = const.: d
τ
= +(1 A dt)• curvature perturbation on Σ(t): R (3) (3) 2
4
R
a
= −
∆ R
x xi i = const.= const. Σ Σ((tt)) Σ Σ((t+dtt+dt)) d dττ traceless• expansion (Hubble parameter):
(
)
13 (3) 1 t H = H − A + ∂ + ∆ E R ɶ
( )
( )
scalar tensor 1 3 transverse-traceless (3) ij i j ij ij H E Hδ
= ∂ ∂ − ∆ =metric (on a spatially flat background)
• comoving slicing
0
(
=
( )
for a scalar field
)
iT
µ=
φ φ
t
• flat slicing (3) (3)=0
0
24
R
a
= −
∆
R
⇔
R
=
• Newton (shear-free) slicing
( )
scalar1
0
0
0
3
(3) tH
ij i jδ
ij tE
tE
E
∂
= ∂ ∂ −
∆ ∂
=
⇔ ∂
=
⇔
=
• uniform density slicing
−
T
00≡ =
ρ ρ
( )
t
• uniform Hubble slicingChoice of gauge (time-slicing)
( )
1
0
3
(3) tH
=
H t
⇔ −
H A
+ ∂
+ ∆
E
=
R
ɶ
matter-based gauge geometry-based gaugecomoving = uniform
ρ
= uniform H on superhorizon scales ┴┴ ┴ ┴
( )
22
3
8
(3) 4 2H
O
G
a
ε
π ρ
−
∆ +
R
=
ɶ
(
)
Hubble horizon scale
on superhorizon scales
wavelength
1
ε
=
≪
at leading order in ε , Friedmann equation holds
independent of time-slicing.
local ‘Hubble parameter’ given by
3
H
ɶ
2=
8
π ρ
G
+
O
( )
ε
2‘local’ means ‘measured on scales of Hubble horizon size’
Separate universe approach
0 0
0 8 0
G =
π
GTfurther, if is time-independent,
Friedmann equation holds up through O(ε2),
with local ‘curvature constant’ given by
( )
2
( )
3
(3)i i
K x
= − ∆ R
x
local Friedmann eq. holds up through O(ε2),
for adiabatic perturbations (= adiabatic limit) on comoving/uniform
ρ
/uniform H slices.( )
22
3
8
(3) 4 2H
O
G
a
ε
π ρ
−
∆ +
R
=
ɶ
( )
23
( )
2 48
iK x
H
O
G
a
ε
π ρ
+
+
=
ɶ
comoving curvature perturbation R C is conserved in the adiabatic limit:
; 2 2 2 2 2 2 2 ( ) ( ) ( ) ~ z a P O z a z H
ρ
ε
′ + ′′ + ′ = ≡ C C R R3. Linear
δN formula
Starobinsky ’85, MS & Stewart ’96, …. e-folding number perturbation between Σ(t) and Σ(tfin):
(
)
(
)
( )
( )
( )
fin fin fin fin background fin1
3
(3) 2;
t t t t t tN t t
H d
H d
E dt
t
t
O
δ
τ
τ
ε
≡
−
=
∂
+ ∆
=
−
+
∫
∫
∫
tR
R
R
ɶ
N N00((tt,,ttfinfin))δ
δ
NN((tt,,ttfinfin)) Σ Σ ((ttfinfin); ); RR((tt fin fin)) Σ Σ00 ((ttfinfin)) Σ Σ00 ((tt)) xi =const. Σ Σ ((tt); ); RR((tt)) δN=0 if both Σ(t) and Σ(tfin) are chosen to be ‘flat’ (R=0).By definition, δN(t; tfin) is t-independent.
The gauge-invariant variable ‘ζ’ used in the literature
is equal to RC on superhorizon scales (sometimes ζ = -RC) Σ(t); R(t)=0
Σ(tfin); RC(tfin)
xi =const.
Choose Σ(t) = flat (R=0) and Σ(tfin) = comoving:
(
;
fin)
( )
fin( )
C( )
finN t
t
t
t
t
δ
=
R
−
R
= R
(suffix ‘C’ for comoving) curvature perturbation on comoving slice
Example: single-field slow-roll inflation
- single-field inflation, no extra degree of freedom R
C becomes constant soon after horizon-crossing (t=th):
(
h;
fin)
( )
fin( )
hN t t
t
t
δ
=
R
C=
R
C log a log L L=H-1 t=th RC = c onst. t=tfin inflationAlso because Rc is conserved, δN = H(th) δtF→C , where δtF→C is the time difference between the comoving and flat slices at t=th.
ΣF(th) : flat R=0, δφ=δφF ΣC(th) : comoving
δ
tF→C R=RC , δφ=0( )
(
)
( )
C fin h; fin F C F h dt t N t t H t H t dδ
δ
δφ
φ
→ = = = − R ··· δN formula(
)
( )
F h F C, C h i t t x tφ
+δ
→ =φ
δφ
F +φ
ɺ( )
thδ
tF→C = 0 dN = −Hdt( )
F h dN t dφ
δφ
=Only the knowledge of the background evolution is necessary to calculate RC(tfin) .
(for slow-roll, no isocurvature perturbation)
( )
( )
( )
C finδ
φ
δφ
F hδφ
F h ∂ = = ≡ ∇ ⋅ ∂∑
R a a a a a N t N t N tMS & Stewart ’96, MS & Tanaka ‘98
N.B. RC is no longer conserved:
( )
F C t H 2φ δφ
φ
⋅ = − R ɺɺ ··· time-varying even on superhorizon
( )
( )
( )
h F 2 2 2 3 4 2 2 2 2 2 3 2 4 ( ) (2 ) S H t k H P k N Nπ
δφ
π
π
π
φ
= ∇ = ∇ ≥ ɺ a a N Nφ
∂ ∇ ≡ ∂• spectrum (for mutually independent
δφ
Fa )2 2 2 2 2 2 2 a a H H φ N φ N N φ = ∇ ≤ ∇ ⇒ ∇ ≥ i ɺ ɺ
tensor-to-scalar ratio
8
16
T T s SP
n
P
≤
=
ε
• scalar spectrum:( )
( )
2( )
2π
π
=π
∇ 3 2 2 3 2 4 S k H P k N • tensor spectrum:( )
( )
4 8 2 2π
κ
π
=π
3 2 2 3 2 ( ) T k H P k• tensor spectral index: 2
1 8 2 2 2 2 2 2 2 2 2 2 s T T S H n H H P P N N
φ
κ
φ
κ
κ
φ
ε
− = ≡ − = = ≥ = ∇ ⋅∇ ɺ ɺ ɺ ɺ φ = − = − a ∇ a dN H N dt i MS & Stewart ‘96··· valid for any slow-roll models
1 s n
k
−∝
∝
k
nT 8 2 G κ = π(‘=’ for a single inflaton model)
2 s H H
ε
≡ − ɺ slow-roll parameter Einstein gravity4. Non-linear extension
;
ix
Q
t
Q
HQ H
G
ρ
∂
∂
∂
≪
∂
∼
∼
This is a consequence of causality:
Field equations reduce to ODE’s
Belinski et al. ’70, Tomita ’72, Salopek & Bond ’90, …
light cone
L »H-1
H-1
• On superhorizon scales, gradient expansion is valid:
metric on superhorizon scales
(
)(
)
( )
2 idet
1,
2 2 2 i i j j ij ijds
dt
e
dx
dt dx
dt
O
αγ
β
β
γ
β
ε
= −
+
+
+
=
=
N
ɶ
ɶ
expansion parameter
,
iε
iε
∂ → ∂
=
( )
( ,
)
( ,
exp
α
t x
i
=
a
t
ex
p
ψ
t x
i)
the only non-trivial assumption
e.g., choose
ψ
(t* ,0) = 0fiducial `background’
contains GW (~ tensor) modes
•
• gradient expansion:
•
• metric:
• Local Friedmann equation
28
2( ,
)
( ,
)
(
)
3
iG
iH t x
ɶ
=
π
ρ
t x
+
O
ε
xi : comoving (Lagrangian) coordinates.
exactly the same as the background equations.
uniform
ρ
slice = uniform Hubble slice = comoving slice(
)
3
0
d
H
p
d
τ
ρ
+
ρ
+
=
ɶ
d
τ
= N dt : proper time along fluid flowas in the case of linear theory
no modifications/backreaction due to super-Hubble perturbations.
(
)
(
)
( )
0
0 ;
2;
3
tT
u u
p g
u u
u
T
d
u
p
u
O
d
µν µ ν µν µ ν µν µ ν µ µ µ µρ
α
ρ
ρ
ε
τ
=
+
+
∇
=
∂
⇒
+ ∇
+
=
∇
=
+
N
( )
normal to
const
.
21
1
3
3
H
u
n
O
n dx
dt
t
µ µ µ µ µ µε
≡ ∇
= ∇
+
= −
N
⋅⋅⋅
=
ɶ
At leading order, local Hubble parameter is independent of the time slicing, as in linear theory
n
µu
µ t=const.( )
0 i iu
v
O
u
ε
≡
=
assumption uµ – nµ = O(ε) •• energy momentum tensor:
• local Hubble parameter:
5. Nonlinear δN formula
(
)
( )
2 3 t t t a O H p a ρ ε α ψ ρ ∂ + = −∂ = − + ∂ = − + N ɺ ɶ energy conservation:(applicable to each independent matter component)
e-folding number:
(
)
2 2 1 1 1 2 1 , ; 3 i t t i t t t x N t t x H dt dt Pρ
ρ
∂ ≡ = − +∫
ɶ N∫
where xi =const. is a comoving worldline.
(
)
(
)
2 1 1 2 1 2 1 1 2 0 2 0 , ; , ; ( , ) 1 ( , ) 3 ( ) i i t t t t t x t t x N N N dt N t t P t tρ
ρ
ρ
≡ − = ∆ ∂ − − +∫
(
2,) (
1,)
(
1, ;2)
i i i t x t xN
t t xψ
−
ψ
= ∆
whereLyth, Malik & MS ’04 Langlois & Vernizzi ’05
This definition applies to any choice of time-slicing
To summarize:
(
) (
)
(
)
2 1 2 1 1 2 0 1 2 , , , ;
1
( , )
3
( )
i i i t t t t x t xN
t t xdt
N t t
P
ψ
ψ
ρ
ρ
ρ
−
= ∆
∂
= −
−
+
∫
matter geometryrelates the evolution of matter to geometry.
Here we use ∆N for general choice of slices.
N0(t1,t2)
∆
N(t1,t2) Σ (t2); ψ(t2) ΣF (t2) ΣF (t1) xi =const. Σ (t1); ψ(t1)ΣF (t): hypersurface on which
ψ
= 0 ↔ eα = a(t); ‘flat’ slicebetween and
1 2 0 1 2 1 2
( , ; )i ( , ) F ( ) F ( )
N t t x = N t t Σ t Σ t
No need for `background’ universe
NL
δ
N - formula
Let us take slicing such that Σ(t) is ‘flat’ at t = t1 [ ΣF (t1) ] and uniform density/comoving/uniform H at t = t2 [ ΣC (t2) ]:
( ‘flat’ slice: Σ(t) on which
ψ
= 0 ↔ eα = a(t) )ΣF (t1) : flat
ΣC(t2) : uniform density
ρ
(t2)=const.ψ
(t1)=0 N0(t2,t1)∆
NCψ
(t2)=0 ΣF (t2) : flat 1 2 1 2 ( , ; )i C( , ; )i N t t x N t t x ∆ = ∆(
1,
)
0,
(
2,
)
C(
2,
)
(
1,
2;
)
i i i i
C
t x
t x
t x
N
t t x
ψ
=
ψ
=
R
= ∆
where
∆Ν
C is the e-folding number from ΣF(t2) to ΣC(t2):(
)
2 2 2 2 1 1 ( ) ( 1 2 ) ( ) ( ) ( ) ( )
1
1
3
, ;
1
3
3
C F F i F C F i t i t t t C t t t x x t tN
dt
N t t x
dt
P
t
P
P
d
ρ
ρ
ρ
ρ
δ
ρ
ρ
Σ Σ Σ Σ Σ Σ∂
∂
≡ ∆
= −
+
=
+
∂
−
+
+
∫
∫
∫
suffix C for comoving/uniform ρ/uniform H
indep of t1
ΣC(t): matter is almost homogeneous & isotropic
Then
For adiabatic case
(
p=p(ρ) ,or single-field slow-roll case),(
)
2 1 2 1 1 2 ( , ) 2 2 1 ( , ) 1 1 , ; 3 ( ) ( ) 1 ( , ) ( , ) ln 3 ( ) ( ) i i t i t t t x i i t x N t t x dt P a t d t x t x P a t ρ ρρ
ρ
ρ
ρ
ψ
ψ
ρ
ρ
∂ = − + = − = − + + ∫
∫
6. conservation of NL curvature perturbation
2 1 2 1 2 2 1 1 ( , ) ( , ) ( , ) ( , ) ( ) ( ) ( ) ( ) 2 2 1 1 1 3 ( ) 1 1 1 3 ( ) 3 ( ) 3 ( ) ( ) ( , ) ( , ) ln ( ) i i i i t x t x t x t x t t t t i i d P d d d P P P a t t x t x a t ρ ρ ρ ρ ρ ρ ρ ρ
ρ
ρ
ρ
ρ
ρ
ρ
ρ
ρ
ρ
ρ
ρ
ρ
ψ
ψ
− + = − + − + + + = − + ∫
∫
∫
∫
, dρ ≈ V d′ φ 2 2 3 V P V ρ + =φɺ ≈ ′ 1 3 d V d N P V ρ δρ φ δφ ρ φ ρ φ δ ρ + + = = ′ +
∫
∫
ex.: single-field slow-roll inflation
h 0 ( ) ψ δ = = = R NL N t t NL ( , ) ( )
1
( )
( ,
)
3
( )
i t x i i td
x
t x
P
ρ ρρ
ψ
ρ
ρ
≡
+
+
∫
R
non-linear generalization ofconserved ‘gauge’-invariant quantity ζ or R
c
(
ψ
andρ
can be evaluated on any time slice)···slice-independent 1 2 1 2 ( , ) ( , ) 1 ( ) 2 ( ) 1 1 ( , ) ( , ) 3 ( ) 3 ( ) i i t x t x i i t t d d t x t x P P ρ ρ ρ ρ
ρ
ρ
ψ
ψ
ρ
ρ
ρ
ρ
+ = + + +∫
∫
Example 2: Curvaton model
ρ
φ=ρ
γ∝
a-4 andρ
χ∝
a-3, henceΩ
χ /Ω
γ∝
a Ωχ Ωγ Ω t2-field model: inflaton (φ) + curvaton (χ)
2 2
1
( )
2
V
V
m
χφ
χ
=
+
2 28
3
GV
m
H
χπ
≈
≪
•• after inflation,
χ
begins to dominate if it does not decay. • during inflationφ
dominates.•
( , ) 1 ln 3 ( ) χ χ χ
ρ
ψ
ρ
= + R i t x t ( , ) 1 ln 4 ( ) γ γ γρ
ψ
ρ
= + R i t x t 3( ) 4( ) ( , )t xi ( , )t xi e χ ψ e γ ψ χ γ χ γρ
+ρ
=ρ
− R − +ρ
− R − •• With sudden decay approx, final curvature pert amp
ζ
is determined by 3( ) 4( )( , )
t x
i( , )
t x
ie
χ ζe
γ ζ χ γ χ γ χ γρ
+
ρ
=
ρ
− R −+
ρ
− R −=
ρ
+
ρ
•• On homogeneous total density slices,
ψ
=ζ
( A A) A C A P P ρ ζ ρ + = = +
∑
R R nonlinear version of(
)
4( ) 3( )1
e
γ ζe
χ ζ1
χ χ − −− Ω
R+ Ω
R=
Ωχ : density fraction of
χ
at the moment of its decay MS, Valiviita & Wands (2006)7
. NL δN for ‘slowroll’ inflation
• Nonlinear
δ
N for multi-component inflation :(
) ( )
1 2 1 2 1 ! δ φ δφ φ δφ δφ δφ φ φ φ = + − ∂ = ∂ ∂ ∂∑
n n A A A n A A A A A A n N N N N n ⋯ ⋯ •• In slow-roll inflation, all decaying mode solutions of the (multi-component) inflaton field
φ
die out.MS & Tanaka ’98, Lyth & Rodriguez ‘05
•
• If
φ
is slow rolling (or already at an attractor stage) when the scale of our interest leaves the horizon, N is only afunction of
φ
(independent of dφ
/dt ), no matter how complicated the subsequent evolution is.where
δφ
=δφ
F (on flat slice) at horizon-crossing.(
δφ
F may contain non-gaussianity from subhorizon interactions) eg, DBI inflationexample:
multi-brid
inflation
0φ
=
∑
exp
A(
A)
AV
V
u
1 3 1φ
φ
φ
φ
φ
∂ ∂ ′ = = = = ∂ ∂ 2 1 - ( ) A A A A A A d d V V u dN H dt H V • slow-roll eom: 1 21
2
,( )
A A AL
φg
µν µφ
νφ
V
φ
== −
∑
∂
∂
−
V φφφφ inflation 1 2,
) +
( ,
φ φ
⋅⋅⋅
φ
nχ
MS MS ‘‘0808= −
dN
Hdt
N as a time variable: 2 2 2 2 3 1 8κ
κ
=π
== − = Pl H V G M inflaton(
)
A A A A Adq
d
q
u
φ
φ
≡
′
1 cos , 2 sin , q = q θ q = q θ θ = const. •• transformation of field variables:
1
ln
Ad
q
dN
=
1
1
1
3
(
)
(
)
A A A A A A Ad
V
d
u
dN
V
u
dN
φ
φ
φ
φ
φ
∂
′
=
=
⇒
=
′
∂
set set 2 A;
1
A A Aq
=
qn
∑
n
=
d
ln
q
1
,
dn
A0
dN
=
dN
=
angular coordinates nA are conserved..
q q22 q q11
θ
θ
N N=0=0 q q 1, 2(
q q
)
N N=const.=const.trajectories are radial in space
trajectories are radial in space
1 2
(
, )
( , )
( , )
q q N
N
N q
N
θ
θ
φ φ
=
↔
=
=
1 , 0 ln d q d dN dN θ = = ( , ) ln ln ( ) f N q θ = q − q θ f f( )
q
=
q
θ
Assume that inflation ends at
g
12φ
12+
g
22φ
22=
σ
2 1 f 2 f 1 2 , cos , , sin g gσ
σ
φ
=γ
φ
=γ
Parametrize orbits by an angle at the end of inflation
2 2 2 1 2 / , A mA A q = eφ q = q + q
and the universe is thermalized instantaneously.
1 1 2 2 1,f 1 2,f 2 2 2 f 2 2 1 2 / / / ln ln ( ) ln m m m m e e N q q e e φ φ φ φ
θ
+ = − = + (
2 2 2 2)
2 2 2 2 0 1 1 2 2 1 2χ
4λ
σ
φ
φ
λ
χ
= + + − V g g realized by For exponential pot.:0 φ 0 φ = =
∑
∑
exp A( A) exp A A A A V V u V m φ φ φ = = ′ ( ) A A A A A A A dq d d q u m(
1 2)
2 2 1 1 11 22 2 2 2 21
2
/ / cos / sin /,
ln
m m g m g me
e
N
N
e
e
φ φ σ γ σ γφ φ
+
=
=
+
whereγ
=γ
(φ
1,φ
2)(
1 1,
2 2)
(
1,
2)
N
N
N
δ
=
φ δφ φ δφ
+
+
−
φ φ
• δN valid to full nonlinear order is simply given by
1 1 2 2 1 2 1 1 2 2
cos
sin
ln
q
q
m
m
g m
g m
φ
φ
σ
γ σ
γ
=
−
=
−
This determines
γ
in terms ofφ
1 &φ
2 . (∙∙∙ const of motion)1 2 f 0
1 2
exp m cos m sin
V V g g
σ
σ
γ
γ
= + • To be precise, one has to add a correction term to adjust the energy density difference at the end of inflation
f 1 2 0 1 2 1 4 ln 4 cos sin c V m m N V g g
σ
γ
γ
= = + (assuming instantaneous thermalization)
1 1 2 2 1 1 2 2 2 2 2 2 1 2 / / cos / sin / ln m m c g m g m e e N N e e φ φ σ γ σ γ + = + + where
However, this correction is negligible
1
,
2 Pl1
m m
≪
M
=
• δN to 2 order in δφ : 2 2 1 2 1 1 2 2 2 1 1 2 3 1 1 2 2 1 1 2 2 2 2 cos sin ( )
cos sin ( cos sin )
g g g m m N m g m g m g g m g δφ γ δφ γ δφ δφ δ γ γ σ γ γ + − = + + +
• comoving curvature perturbation spectrum 2 2 2 2 2 1 2 2 1 1 2 2 2 γ γ γ γ π = + = + P( ) cos sin ( cos sin ) S k Ha g g H k m g m g 2 2 1 2 1 ( ) s n = − m + m 2 1 1 2 2 2 2 2 2 1 2 8 γ γ γ γ + = = + S P P ( ) ( cos sin ) ( ) cos sin T k m g m g r k g g • cf: single-field case f f mN N m
φ φ
φ
= +φ
⇔ = − No non-Gaussianity if δφ is Gaussian spectral index: tensor/scalar: 2 2 local 1 , 8 , 0 s NL n = − m r = m f =1 1 2 2 1 2 2 1
1 1 2 2 2 1 1 2
,
cos sin sin cos
cos sin cos sin
L g g g g N S m g m g m g m g δφ γ δφ γ δφ γ δφ γ δ γ γ γ γ + − ≡ ≡ + − Let
“true” entropy perturbation
2 2 2 local 1 2 2 1 1 2 2 2 2 2 2 1 2 1 1 2 2 5 6 ( cos sin )
( cos sin ) cos sin
NL g g m g m g f g g m g m g γ γ σ γ γ γ γ − = + +
(
)
local 2 3 5 NL L L N N f N Sδ
=δ
+δ
+ 2 0 for 2 A B AB L H N S δ δφ δφ δ π ⋅ = = (
)
local 1 2 1 2for
/
,
~ ( ),
,
~ ( ).
NLf
=
O gm
σ
m m
O m
g g
O g
practically any non-Gaussianity is possible
linear entropy perturbation contributes at 2nd order
local
0 ( . .,N B fNL > )
• example of parameters
model parameters: outputs: 2 2 1 ~ .0 005 , 2 ~ .0 035 m m(
)
2 4 9 5 3H =σ
4λ
~ .1 5 10 × − ⇔ PR( ) ~ .k 2 5 10× − 2 2 1 2 1 ( ) ~ .0 96 s n = − m + m 2 1 8 ~ .0 04 r ≈ m 2 local 2 1 4 1 5 40 6 ~ / NL gm g f mσ
λ
≈ 1 2 18 1= MPl = (8π
G)− / = 2 43 10 GeV. × 1cos 2 sin mγ
≫ mγ
assume 2 1 2 4 10 / ~σ
λ
× − 2 2 2 1 2 g = g ≡ g independent of waterfall fieldPlanck 2013 constraint on r & n
sexample
fNLlocal can be ~ 10
8. Conformal frame (in)dependence
why bother?
-In cosmology, we encounter various frames of the metric which are conformally equivalent.
But it is often said that there exists a unique physical frame
on which we should consider actual ‘physics.’
They are mathematically equivalent, so one can work in any frame as long as mathematical manipulations are concerned.
Einstein frame, Jordan frame, string frame, ...
How does physics depend/not depend
on choice of conformal frames?
• Einstein frame
“gravitational” part : R+L(
φ
) ~ minimal coupling between g andφ
matter part: G(φ
)L(ψ
, A,…)ψ
: fermion, A : vector, ...Two typical frames in scalar-tensor theory
• Jordan(-Brans-Dicke) frame
“gravitational” part : F(
φ
)R+L(φ
)matter part: L(
ψ
, A,…) ~ minimal coupling with g matter assumed to be universally coupled with g∙∙∙ for baryons, experimentally consistent
φ
φ
φ
φ
++++ g
if non-universal coupling: ( ( ); , , . A A A A A Gφ
L Q Qψ
A ⇒∑
) = ⋅⋅⋅conformal transformation
2 gµν → ɶgµν = Ω gµν 2 2 ( 1) 2 ( 4) R → R = − R − D − Ω − D − gµν ∂ Ω∂ Ω µ ν Ω Ω Ω □ ɶ• metric and scalar curvature
• matter fields ( for D = 4 )
(
)
(D 2) / 2 2φ
→φ
= Ω− −φ
= Ω−φ
ɶ(
)
(D 1) / 2 -3/ 2ψ
→ψ
= Ω− −ψ
= Ωψ
ɶ(
)
(D 4) / 2 Aµ → Aɶµ = Ω− − Aµ =Aµ scalar vector fermioncosmological perturbations
Makino & MS ‘91, Komatsu &Futamase ’99,...
• tensor-type perturbation
Definition of hij is apparently Ω-independent.
0 ij j jh h j ∂ = =
(
)
(
)
2 2 2 2 2 ( ) ( ) i j ij ij j ij ij i ds dt a t dx dx a d x h d h dxδ
η
η
δ
= − + + = − + + (
)
2 2 2 2 2 2 ( ) ( ) ij ij i j ds ds x aµη
dη
δ
h dx dx = Ω = Ω − + + ɶ• vector-type perturbation
(
)
2 2 2
2Bj j ij iH j j i i j
ds = a −d
η
+ dx dη
+δ
+ ∂ + ∂ H dx dx Definitions of Bj and Hj are aslo Ω-independent.
0 j j jB jH ∂ = ∂ =
(
)
2 2 2 2 2 2 2 j j ij i j j i i j ds ds a dη
B dx dη
δ
∂ H + ∂ H dx dx = Ω = Ω − + + + ɶ(spatial) tensor & vector are conformal frame-independent
This means in particular PT(k) formula (~H2) from inflation
• scalar-type perturbation
(
)
2 2 2 ( ) (1 2 ) 2 (1 2 ) 2 j i j j i j ij ds a d dx d dx x A d B Eη
η
η
δ
= − + + + + + ∂ ∂ ∂ RDefinitions of B and E are Ω-independent.
( )
, 0( )
1 ( , ) i i t x t ω
t x Ω = Ω + (
)
2 2 2 2 2 2 (1 2 ) 2 (1 2 ) 2 j i j i j i j j ds ds a d dx d d A B E x dxη
η
δ
= Ω = Ω − + + + + ∂ ∂ ∂ + R ɶ , A → A +ω
R → R + ωFor scalar-tensor theory with
1 1
( ) ( , ) ,
2 f R K X X 2
L =
φ
+φ
≡ − gµν ∂ ∂µφ φ
νThe important, curvature perturbation R
c , conserved on
superhorizon scales, is defined on comoving hypersurfaces.
R
c= R
δφ=0is Ω-independent!
Nevertheless, if we haveΩ = Ω
( )
φ
1 c H da a dδφ
δφ
φ
φ
≡ − = − R R R ɺ uniformφ
(δφ
= 0) frame-independent( )
φ
Ω = Ω
Rc is conformal-frame independent in the adiabatic limit
⇔if not in the adiabatic limit, the notion of adiabatic perturbation depends on choice of conformal frames
generalization to NL perturbation
Generalization is straightforward for perturbations on superhorizon scales
δN formalism:
Gong, Hwang, Park, Song & MS ‘11
R
c(tf) = δN between the final comoving surface (t=tf)
and an initial flat surface
although the number of e-folds N depends on conformal frames, δN is frame-independent in the adiabatic limit
White, Minamitsuji & MS ‘13 ....