Equations of fluid dynamics

Appendix B The speed of sound

The speed of sound is defined as the speed of propagation of small pertubations in density and pressure in a fluid in a compressible fluid. For the derivation of the sound speed it is also assumed that the fluid is homogeneous, i.e. the average value of density ρ0 and pressure p0 are spatially (and temporarily ?) constant. Then we can split the local value of density and pressure in a spatially constant average value and a small spatially an temporarily varying pertubation ρ and p respectively

ρ =ρ0+ρ(x,t),ρρ0 (B.1)
p =p0+p(x,t),pp0 (B.2)

For an ideal fluid a temporal change in density or pressure has to adiabatic, i.e. with constant entropy. The derivation of the equation of motion for a small pertubation in density and pressure then leads us to a wave equation with a propagation speed

c=(p0ρ0)S (B.3)

which is called the adiabatic speed of sound.

Further on for an adiabatic change of state it applies

pVγ =const.=C|1Mγ (B.4)
p(VM)γ =CMγ (B.5)
p(1ρ)γ =C* (B.6)
p =C*ργpρ=C*ργ-1 (B.7)

Using this we get

p0ρ0=γC*ρ0γ-1=γp0ρ0. (B.8)

With this result the adiabatic speed of sound for an ideal, compressible, homogeneous fluid yields

c=γp0ρ0 (B.9)

Using equation (A.4) we can compute the sound speed for an ideal gas directly from the internal energy

c=γ(γ-1)u0 (B.10)

B.1 Machnumber

The Machnumber of a flow is defined as

Ma=vc (B.11)

The Machnumber can also be interpreted as the ratio of the kinetic and internal energy, because

Ma2=v2γ(γ-1)u=1γ(γ-1)ekineint (B.12)

So, the Machnumber Ma=xekin/eint where x for some values of γ can be found in the following table:

γ γ(γ-1) x=[γ(γ-1)]-1/2
53 109 3100.949
75 1425 5141.336
43 49 32 = 1.5