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 and pressure 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 and respectively
| (B.1) | ||||
| (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
| (B.3) |
which is called the adiabatic speed of sound.
Further on for an adiabatic change of state it applies
| (B.4) | ||||
| (B.5) | ||||
| (B.6) | ||||
| (B.7) |
Using this we get
| (B.8) |
With this result the adiabatic speed of sound for an ideal, compressible, homogeneous fluid yields
| (B.9) |
Using equation (A.4) we can compute the sound speed for an ideal gas directly from the internal energy
| (B.10) |
The Machnumber of a flow is defined as
| (B.11) |
The Machnumber can also be interpreted as the ratio of the kinetic and internal energy, because
| (B.12) |
So, the Machnumber where for some values of can be found in the following table:
| = 1.5 |