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Introduction to Acoustics

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temperature,<br />

q =−κ∇T , (3.16)<br />

where κ is the coefficient of thermal conduction.<br />

Transport Properties of Air<br />

Regarding the values of the viscosities and the thermal<br />

conductivity that enter in<strong>to</strong> the above expressions, the<br />

values for air are approximated [3.16–18]by<br />

� �3/2 T T0 + TS<br />

µS = µ0<br />

, (3.17)<br />

T0 T + TS<br />

µB = 0.6µS , (3.18)<br />

� �3/2 T T0 + TA e<br />

κ = κ0<br />

−TB/T0<br />

. (3.19)<br />

T + TA e−TB/T T0<br />

Here TS is 110.4K, TA is 245.4K, TB is 27.6K,<br />

T0 is 300 K, µ0 is 1.846 × 10 −5 kg/(ms), and κ0 is<br />

2.624 × 10 −2 W/(mK).<br />

Transport Properties of Water<br />

The corresponding values of the viscosities and the thermal<br />

conductivity of water depend only on temperature<br />

andaregivenby[3.19, 20]<br />

µS = 1.002 × 10 −3 e −0.0248∆T , (3.20)<br />

µB = 3µS , (3.21)<br />

κ = 0.597 + 0.0017∆T − 7.5×10 −6 (∆T ) 2 .<br />

(3.22)<br />

The quantities that appear in these equations are unders<strong>to</strong>od<br />

<strong>to</strong> be in MKS units, and ∆T is the temperature<br />

relative <strong>to</strong> 283.16 K (10 ◦ C).<br />

3.2.5 Navier–S<strong>to</strong>kes–Fourier Equations<br />

The assumptions represented by (3.12, 13, 15), and<br />

(3.16) cause the governing continuum mechanics equations<br />

for a fluid <strong>to</strong> reduce <strong>to</strong><br />

∂ρ<br />

+∇·(ρv) = 0 , (3.23)<br />

∂t<br />

ρ Dv<br />

=−∇p +∇(µB∇·v)<br />

Dt<br />

+ � ∂<br />

(µφij) + gρ, (3.24)<br />

ij<br />

ij<br />

ei<br />

∂x j<br />

ρT Ds<br />

Dt = 1 �<br />

2 µ φ 2 ij + µB (∇·v) 2 +∇·(κ∇T) ,<br />

(3.25)<br />

Basic Linear <strong>Acoustics</strong> 3.2 Equations of Continuum Mechanics 31<br />

which are known as the Navier–S<strong>to</strong>kes–Fourier equations<br />

for compressible flow.<br />

3.2.6 Thermodynamic Coefficients<br />

An implication of the existence of an equation of state<br />

of the form of (3.12) is that any thermodynamic variable<br />

can be regarded as a function of any other two (independent)<br />

thermodynamic variables. The pressure p, for<br />

example, can be regarded as a function of ρ and T,orof<br />

s and ρ. In the expression of differential relations, such<br />

as that which gives dp as a linear combination of ds<br />

and dρ, it is helpful <strong>to</strong> express the coefficients in terms<br />

of a relatively small number of commonly tabulated<br />

quantities. A standard set of such includes:<br />

1. the square of the sound speed,<br />

c 2 � �<br />

∂p<br />

= , (3.26)<br />

∂ρ<br />

s<br />

2. the bulk modulus at constant entropy,<br />

BV = ρc 2 � �<br />

∂p<br />

= ρ , (3.27)<br />

∂ρ<br />

3. the specific heat at constant pressure,<br />

� �<br />

∂s<br />

cp = T , (3.28)<br />

∂T<br />

p<br />

4. the specific heat at constant volume,<br />

� �<br />

∂s<br />

cv = T , (3.29)<br />

∂T<br />

ρ<br />

5. the coefficient of thermal expansion,<br />

� �<br />

∂(1/ρ)<br />

β = ρ<br />

. (3.30)<br />

∂T<br />

p<br />

(The subscripts on the partial derivatives indicate the<br />

independent thermodynamic quantity that is kept fixed<br />

during the differentiation.) The subscript V on BV is included<br />

here <strong>to</strong> remind one that the modulus is associated<br />

with changes in volume. For a fixed mass of fluid the<br />

decrease in volume per unit volume per unit increase in<br />

pressure is the bulk compressibility, and the reciprocal<br />

of this is the bulk modulus.<br />

The coefficients that are given here are related by the<br />

thermodynamic identity,<br />

γ − 1 = Tβ 2 c 2 /cp , (3.31)<br />

where γ is the specific heat ratio,<br />

γ = cp<br />

. (3.32)<br />

cv<br />

s<br />

Part A 3.2

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