Acoustic wave

The acoustic wave equation describes the propagation of sound waves. The acoustic wave equation for sound pressure in one dimension is given by

$${\displaystyle {\partial ^{2}p \over \partial x^{2}}-{1 \over c^{2}}{\partial ^{2}p \over \partial t^{2}}=0}$$

where

• ${\displaystyle p}$ is sound pressure in Pa
• ${\displaystyle x}$ is position in the direction of propagation of the wave, in m
• ${\displaystyle c}$ is speed of sound in m/s
• ${\displaystyle t}$ is time in s

The wave equation for particle velocity has the same shape and is given by

$${\displaystyle {\partial ^{2}u \over \partial x^{2}}-{1 \over c^{2}}{\partial ^{2}u \over \partial t^{2}}=0}$$

where

• ${\displaystyle u}$ is particle velocity in m/s

For lossy media, more intricate models need to be applied in order to take into account frequency-dependent attenuation and phase speed. Such models include acoustic wave equations that incorporate fractional derivative terms, see also the acoustic attenuation article.

D'Alembert gave the general solution for the lossless wave equation. For sound pressure, a solution would be

$${\displaystyle p=R\cos(\omega t-kx)+(1-R)\cos(\omega t+kx)}$$

where

• ${\displaystyle \omega }$ is angular frequency in rad/s
• ${\displaystyle t}$ is time in s
• ${\displaystyle k}$ is wave number in rad·m⁻¹
• ${\displaystyle R}$ is a coefficient without unit

For ${\displaystyle R=1}$ the wave becomes a travelling wave moving rightwards, for ${\displaystyle R=0}$ the wave becomes a travelling wave moving leftwards. A standing wave can be obtained by ${\displaystyle R=0.5}$.

In a travelling wave pressure and particle velocity are in phase, which means the phase angle between the two quantities is zero.

This can be easily proven using the ideal gas law

$${\displaystyle pV=nRT}$$

where

• ${\displaystyle p}$ is pressure in Pa
• ${\displaystyle V}$ is volume in m³
• ${\displaystyle n}$ is amount in mol
• ${\displaystyle R}$ is the universal gas constant with value ${\textstyle 8.314\,472(15)~{\frac {\mathrm {J} }{\mathrm {mol~K} }}}$

Consider a volume ${\displaystyle V}$. As an acoustic wave propagates through the volume, adiabatic compression and decompression occurs. For adiabatic change the following relation between volume ${\displaystyle V}$ of a parcel of fluid and pressure ${\displaystyle p}$ holds

$${\displaystyle {\partial V \over V_{m}}={-1 \over \ \gamma }{\partial p \over p_{m}}}$$

where ${\displaystyle \gamma }$ is the adiabatic index without unit and the subscript ${\displaystyle m}$ denotes the mean value of the respective variable.

As a sound wave propagates through a volume, the horizontal displacement of a particle ${\displaystyle \eta }$ occurs along the wave propagation direction.

$${\displaystyle {\partial \eta \over V_{m}}A={\partial V \over V_{m}}={-1 \over \ \gamma }{\partial p \over p_{m}}}$$

where

• ${\displaystyle A}$ is cross-sectional area in m²

From this equation it can be seen that when pressure is at its maximum, particle displacement from average position reaches zero. As mentioned before, the oscillating pressure for a rightward traveling wave can be given by

$${\displaystyle p=p_{0}\cos(\omega t-kx)}$$

Since displacement is maximum when pressure is zero there is a 90 degrees phase difference, so displacement is given by

$${\displaystyle \eta =\eta _{0}\sin(\omega t-kx)}$$

Particle velocity is the first derivative of particle displacement: ${\displaystyle u=\partial \eta /\partial t}$. Differentiation of a sine gives a cosine again

$${\displaystyle u=u_{0}\cos(\omega t-kx)}$$

During adiabatic change, temperature changes with pressure as well following

$${\displaystyle {\partial T \over T_{m}}={\gamma -1 \over \ \gamma }{\partial p \over p_{m}}}$$

This fact is exploited within the field of thermoacoustics.

The propagation speed, or acoustic velocity, of acoustic waves is a function of the medium of propagation. In general, the acoustic velocity c is given by the Newton-Laplace equation:

$${\displaystyle c={\sqrt {\frac {C}{\rho }}}}$$

where

• C is a coefficient of stiffness, the bulk modulus (or the modulus of bulk elasticity for gas mediums),
• ${\displaystyle \rho }$ is the density in kg/m³

Thus the acoustic velocity increases with the stiffness (the resistance of an elastic body to deformation by an applied force) of the material, and decreases with the density. For general equations of state, if classical mechanics is used, the acoustic velocity ${\displaystyle c}$ is given by

$${\displaystyle c^{2}={\frac {\partial p}{\partial \rho }}}$$

with ${\displaystyle p}$ as the pressure and ${\displaystyle \rho }$ the density, where differentiation is taken with respect to adiabatic change.

Interference is the addition of two or more waves that results in a new wave pattern. Interference of sound waves can be observed when two loudspeakers transmit the same signal. At certain locations constructive interference occurs, doubling the local sound pressure. And at other locations destructive interference occurs, causing a local sound pressure of zero pascals.

A standing wave is a special kind of wave that can occur in a resonator. In a resonator superposition of the incident and reflective wave occurs, causing a standing wave. Pressure and particle velocity are 90 degrees out of phase in a standing wave.

Consider a tube with two closed ends acting as a resonator. The resonator has normal modes at frequencies given by

$${\displaystyle f={\frac {Nc}{2d}}\qquad \qquad N\in \{1,2,3,\dots \}}$$

where

• ${\displaystyle c}$ is the speed of sound in m/s
• ${\displaystyle d}$ is the length of the tube in m

At the ends particle velocity becomes zero since there can be no particle displacement. Pressure however doubles at the ends because of interference of the incident wave with the reflective wave. As pressure is maximum at the ends while velocity is zero, there is a 90 degrees phase difference between them.

An acoustic travelling wave can be reflected by a solid surface. If a travelling wave is reflected, the reflected wave can interfere with the incident wave causing a standing wave in the near field. As a consequence, the local pressure in the near field is doubled, and the particle velocity becomes zero.

Attenuation causes the reflected wave to decrease in power as distance from the reflective material increases. As the power of the reflective wave decreases compared to the power of the incident wave, interference also decreases. And as interference decreases, so does the phase difference between sound pressure and particle velocity. At a large enough distance from the reflective material, there is no interference left anymore. At this distance one can speak of the far field.

The amount of reflection is given by the reflection coefficient which is the ratio of the reflected intensity over the incident intensity

$${\displaystyle R={\frac {I_{\text{reflected}}}{I_{\text{incident}}}}}$$

Acoustic waves can be absorbed. The amount of absorption is given by the absorption coefficient which is given by

$${\displaystyle \alpha =1-R^{2}}$$

where

• ${\displaystyle \alpha }$ is the absorption coefficient without a unit
• ${\displaystyle R}$ is the reflection coefficient without a unit

Often acoustic absorption of materials is given in decibels instead.

When an acoustic wave propagates through a non-homogeneous medium, it will undergo diffraction at the impurities it encounters or at the interfaces between layers of different materials. This is a phenomenon very similar to that of the refraction, absorption and transmission of light in Bragg mirrors. The concept of acoustic wave propagation through periodic media is exploited with great success in acoustic metamaterial engineering.[2]

The acoustic absorption, reflection and transmission in multilayer materials can be calculated with the transfer-matrix method.[3]