The speed of sound of the inflaton field

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SUMMARY

The speed of sound of the inflaton field is defined using the equation c_s^2 = ∂_X P / ∂_X ρ, where X = (1/2) g^{ab} ∂_a φ ∂_b φ. For a canonical scalar field, the pressure P and energy density ρ yield c_s^2 = 1. However, variations in P and ρ can lead to conflicting interpretations of c_s^2, with one method yielding c_s^2 = -1 and another yielding c_s^2 = 1. The distinction between adiabatic sound speed and effective sound speed is crucial, as the effective sound speed is defined as 𝜏_s^2 = ∂_X P / ∂_X ρ, which differs from the adiabatic sound speed derived from thermodynamic perspectives.

PREREQUISITES
  • Understanding of canonical scalar fields in cosmology
  • Familiarity with thermodynamic principles in relation to pressure and density
  • Knowledge of perturbation theory in field equations
  • Proficiency in calculus, particularly partial derivatives
NEXT STEPS
  • Study the Klein-Gordon equation for scalar field perturbations
  • Explore the differences between adiabatic sound speed and effective sound speed
  • Investigate the implications of varying definitions of sound speed in cosmological literature
  • Learn about the role of scalar fields in inflationary cosmology
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Cosmologists, theoretical physicists, and researchers studying inflationary models and scalar field dynamics will benefit from this discussion.

chronnox
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I've been reading about inflation and i encountered that one can always define the sound's speed as

[tex]c_s^2 \equiv \frac{\partial_X P}{\partial_X \rho}[/tex]

where [tex]X \equiv \frac{1}{2} g^{ab} \partial_a \phi \partial_b \phi[/tex]. In the case of a canonical scalar field [tex]P=X-V[/tex] and [tex]\rho=X+V[/tex], so [tex]c_s^2=1[/tex]. That is what is obtained by definition. But i can always consider [tex]P[/tex] and [tex]\rho[/tex] as a function of [tex]P=(X,\phi)[/tex] and [tex]\rho=(X,\phi)[/tex] so

[tex]P+\rho=2 X[/tex] and

[tex]\rho-P= 2 V[/tex]

taking variations of these last to equations i obtain

[tex]\delta P = - \delta \rho + 2 \delta X[/tex] (1) and

[tex]\delta P = \delta \rho - 2 \partial_\phi V \delta \phi[/tex] (2)


Recalling that in general [tex]P=(\rho,S)[/tex] then [tex]\delta P = c_s^2 \delta \rho + \tau \delta S[/tex]. Thus if i read the coefficient of [tex]\delta \rho[/tex] of eq. (1) one obtains that [tex]c_s^2 = -1[/tex] and [tex]\tau \delta S = 2 \delta X[/tex], but if i read the coefficient of eq. (2) one obtains [tex]c_s^2 = 1[/tex] and [tex]\tau \delta S = - 2 \partial_\phi V \delta \phi[/tex], according to the definition the correct reading would be the one done by (2) but is there another explanation of why reading the coefficient [tex]c_s^2[/tex] from (2) is the correct way, or is there a motivation for the first definition for [tex]c_s^2[/tex]?
 
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The problem is that the literature often uses [itex]c_{\rm{s}}^2[/itex] to mean two different things, sometimes simultaneously. Looking at things from a thermodynamic perspective, one can write [itex]P=P(\rho,S)[/itex], and then perturb to give
[tex]\delta P=\frac{\partial P}{\partial\rho}\delta \rho +\tau \delta S[/tex]
where [itex]\frac{\partial P}{\partial\rho}[/itex] is then identified as the adiabatic sound speed-- i.e. the speed with which perturbations travel through the background.

Now, for a scalar field we can parametrise as [itex]P=P(X,\phi)[/itex]. Then, the adiabatic sound speed can be written as
[tex]c_{\rm{s}}^2=\frac{\partial P}{\partial\rho}=\frac{\partial_X P +\partial_\phi P}{\partial_X\rho+\partial_\phi\rho}[/tex]. By writing things like this, it should be apparent that this is not the same as the first expression you quote. It turns out that, for a scalar field, the speed of propagation is not the adiabatic sound speed, but in fact a different speed (say, the "effective sound speed"), which is defined as
[tex]\tilde{c_{\rm{s}}}^2=\frac{\partial_X P}{\partial_X\rho}[/tex]. If you like, you can show this by calculating the Klein-Gordon equation for the perturbation of the field and looking at the term in front of the spatial derivative.
 

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