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Introduction to Acoustics

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Because the friction associated with the motion of<br />

the fluid with respect <strong>to</strong> the solid matrix is inherently<br />

nonconservative (i. e., energy is lost), the original version<br />

(3.119) of Hamil<strong>to</strong>n’s principle does not apply. The<br />

applicable extension includes a term that represents the<br />

time integral of the virtual work done by nonconservative<br />

forces during a variation. If such nonconservative<br />

forces are taken <strong>to</strong> be distributed over the volume, with<br />

the forces per unit volume on the fluid denoted by �<br />

and those on the solid denoted by �, then the modified<br />

version of Hamil<strong>to</strong>n’s principle is<br />

����<br />

(δÄ +�·δU + �·δu) dx dy dz dt = 0.<br />

Moreover, one infers that<br />

(3.131)<br />

� =−� , (3.132)<br />

since the virtual work associated with friction between<br />

the solid matrix and the fluid must vanish if the two are<br />

moved <strong>to</strong>gether.<br />

The Lagrange–Euler equations that result from the<br />

above variational principle are<br />

� �<br />

∂ ∂Ä<br />

+<br />

∂t ∂ (∂Ui/∂t)<br />

�<br />

�<br />

∂ ∂Ä<br />

∂x<br />

j<br />

j ∂ � �<br />

� = �i ,<br />

∂Ui/∂x j<br />

(3.133)<br />

� �<br />

∂ ∂Ä<br />

+<br />

∂t ∂ (∂ui/∂t)<br />

�<br />

�<br />

∂ ∂Ä<br />

∂x<br />

j<br />

j ∂ � �<br />

� = �i .<br />

∂ui/∂x j<br />

(3.134)<br />

Biot, in his original exposition, <strong>to</strong>ok the internal<br />

distributed forces <strong>to</strong> be proportional <strong>to</strong> the relative velocities,<br />

reminiscent of dashpots, so that<br />

� �<br />

∂Ui ∂ui<br />

�i =−�i =−b − . (3.135)<br />

∂t ∂t<br />

Here the quantity b can be regarded as the apparent<br />

dashpot constant per unit volume. This form is such that<br />

the derived equations, in the limit of vanishingly small<br />

frequencies, are consistent with Darcy’s law [3.44] for<br />

steady fluid flow through a porous medium.<br />

The equations that result from this formulation,<br />

when written out explicitly, are<br />

∂2 ∂t2 (ρ11u + ρ12U) −∇(A ′ ∇·u + Q∇·U)<br />

+∇× [N (∇×u)] = b ∂<br />

(U − u) , (3.136)<br />

∂t<br />

Basic Linear <strong>Acoustics</strong> 3.4 Variational Formulations 43<br />

∂2 ∂t2 (ρ12u + ρ22U) −∇(Q∇·u + R∇·U)<br />

=−b ∂<br />

(U − u) , (3.137)<br />

∂t<br />

with the abbreviation A ′ = A + 2N. Here, and in what<br />

follows, it is assumed that the various material constants<br />

are independent of position, although some of the derived<br />

equations may be valid <strong>to</strong> a good approximation<br />

even when this is not the case.<br />

3.4.3 Disturbance Modes in a Biot Medium<br />

Disturbances that satisfy the equations derived in the<br />

previous section can be represented as a superposition of<br />

three basic modal disturbances. These are here denoted<br />

as the acoustic mode, the Darcy mode, and the shear<br />

mode, and one writes<br />

u = uac + uD + ush , (3.138)<br />

U = Uac +UD +Ush . (3.139)<br />

At low frequencies, the motion in the acoustic mode and<br />

in the shear mode is nearly such that the fluid and solid<br />

displacements are the same,<br />

Uac ≈ uac ; Ush ≈ ush . (3.140)<br />

The lowest-order (in frequency divided by the dashpot<br />

parameter b) approximation results from taking the sum<br />

of (3.136)and(3.137) and then setting u = U, yielding<br />

∂<br />

ρeq<br />

2<br />

∂t 2 U −∇(BV,B∇·U) +∇× [GB (∇×U)] = 0 ,<br />

with the abbreviations<br />

(3.141)<br />

ρeq = ρ11 + 2ρ12 + ρ22 , (3.142)<br />

BV,B = A + 2N + 2Q + R , (3.143)<br />

GB = N , (3.144)<br />

for the apparent density, bulk modulus, and shear modulus<br />

of the Biot medium. The same equation results for<br />

the solid displacement field u in this approximation.<br />

Acoustic Mode<br />

For the acoustic mode, the curl of each displacement<br />

field is zero, so<br />

∂<br />

ρeq<br />

2<br />

∂t2 U −∇�BV,B∇·U � = 0 . (3.145)<br />

One can identify an apparent pressure disturbance associated<br />

with this mode, so that<br />

pac ≈−BV,B∇·U , (3.146)<br />

Part A 3.4

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