1.3  Acoustics and the Helmholtz Equation

The governing equations in acoustics need to be prepared for the application of the boundary element method. For example the time-dependent sound pressure in the original wave equation model is replaced by a potential in the Helmholtz equation and the BEM is applied to the latter. However, eventually the results from the BEM need to be interpreted in terms of physical acoustic properties - not just the sound pressure but also the sound power, radiation ratio and also often on the decibel scale.

In this Section it is shown how the time-dependent wave equation governing the acoustic field can be simplified to the Helmholtz equation when harmonic solutions are considered. For further background to acoustic properties and acoustic modelling see texts such as Morse (1962) or Pierce (1970). The three classes of acoustic problem that form the subject of this text are formally described. The content of this Section assumes more importance towards the end of Chapters 4-6 where test problems and applications of the methods are considered. Background knowledge of vector calculus , partial differential equations and Fourier analysis is required.

1.3.1   The Wave Equation and the Helmholtz Equation

The acoustic field is assumed to be present in the domain of a homogeneous isotropic fluid. Whatever the shape and nature of the domain, the acoustic field is taken to be governed by the linear wave equation
Ñ2 Y(p, t) = 1
c2
2
t2
Y(p,t)
(1.1)
where Y(p,t) is the scalar time-dependent velocity potential related to the time-dependent particle velocity by
V(p,t) = Ñ Y(p,t)
(1.2)
and c is the propagation velocity (p and t are the spatial and time variables). The time-dependent sound pressure Q(p,t) is given in terms of the velocity potential by
Q(p,t) = - r Y
t
(p,t)
(1.3)
where r is the density of the acoustic medium.

Only periodic solutions to the wave equation are considered, thus the time-dependent velocity potential Y(p,t) can be reduced to a sum of components each of the form

y(p,t) = f(p) e-i wt
(1.4)
where w is the angular frequency (w = 2 ph, where h is the frequency in hertz) and f(p) is the (time-independent) velocity potential. The substitution of expression (1.4) into (1.1) reduces it to the Helmholtz (reduced wave) equation:
Ñ2 f(p) + k2 f(p) = 0
(1.5)
where k2 = [(w2)/( c2)] and k is the wavenumber. It follows that the wavenumber and the frequency of an acoustic medium are connected by the equation
k = 2 pn
c
 .
(1.6)

In order to carry out a complete solution, the wave equation is written as a series of Helmholtz problems, through expressing the boundary conditions as a Fourier series with components of the form (1.4). For each wavenumber and its associated boundary condition, the Helmholtz equation is then solved. The time-dependent sound pressure y(p,t) can then be constituted from the separate solutions. In practical situations, such as that considered in the example of the analysis of engine noise in Section 5.7, the wave equation is resolved into a large series of the order of hundreds or thousands of frequency components.

The sound pressure p(p) at the point p in the acoustic domain is related to the velocity potential by the formula

p(p) = i rwf(p) .
(1.7)

Often sound levels are measured on the decibel scale. The magnitude in decibels of the sound pressure can be found by the expression

log10(| p(p)
p*
|)*20 
(1.8)
where p* is the reference pressure which is taken to be 2.0 ×20-5.

The phase of the signal is also important. The phase is equivalent to the angle about the origin that is made by plotting the point corresponding to the sound pressure in the Argand plane and it can be found using the arctan or tan-1 function. In Fortran the generalised arctangent function ATAN2 is most useful for this and the phase is given by an expression of the form

ATAN2(AIMAG(p),DBLE(p)) ,
(1.9)
which will return a result in the range [-p, p]. The expression (1.9) gives the phase in radians. The phase in degrees can be found by multiplying this by 180/p.

1.3.2  Other Acoustic Properties (Exterior Problems)

At any frequency of enquiry, the sound pressure at all points in the acoustic domain describe the solution. However other acoustic properties are often of interest in practical situations. For example the acoustic intensity on the surface is
I(p) = 1
2
Re(p*(p)v(p))
(1.10)
at each point p, where the * denotes the complex conjugate.

The sound power is given by

W = ó
õ


S 
I(q) dSq 
(1.11)
or equivalently by
W = 1
2 rc
ó
õ


SF 
p*(q) p(q) dSq
(1.12)
where SF is a hypothetical closed surface in the far-field that encloses S.

The radiation ratio is given by

s RAD = W
1
2
rc ó
õ


S 
v*(q) v(q) dSq
 .
(1.13)

1.3.3  Acoustic Domains and Conditions

In this text a Chapter is devoted to each of three distinct types of acoustic problems: the interior problem, the exterior problem and the interior modal analysis problem. The three distinct cases of two-, three- and axisymmetric three-dimensional problems are covered within each Chapter. The solution of interior and exterior boundary value problems is determined by the boundary condition and the shape of the boundary. Some classes of problem, for example the scattering problem, also involve an incident acoustic field.

The boundary condition specifies either the velocity potential f (that is related closely to the sound pressure by (1.7)) or the normal velocity v (the derivative of f with respect to the normal to the boundary) or some relationship between them at the boundary points. For the boundary value problems, the boundary condition takes the following form:

a(p) f(p) + b(p) v(p) = f(p)    (p Î S)
(1.14)
where a, b and f are complex-valued functions defined on S. For the modal analysis problem the boundary condition is the homogeneous form of (1.14).

In a pure radiation problem, for example, v will be specified on the boundary and there will be no incident field. In a pure scattering problem the boundary condition may be specified such that it is perfectly reflecting (v = 0), for example, or that it has an impedance boundary condition of the form f = gv where g is a constant. The general form of the boundary condition (1.14) allows different forms of condition to be specified at different regions on the boundary.

1.3.4  Condition at Infinity for Exterior Problems

For the exterior problems it is necessary to introduce a condition at infinity. This ensures the physical requirement that all scattered and radiated waves are outgoing. This is termed the Sommerfeld radiation condition:

lim
r ® ¥ 
r1/2 ( f(p)
r
- i k f(p) ) = 0    in two dimensions and
(1.15)

lim
r ® ¥ 
r ( f(p)
r
- i k f(p) ) = 0    in three dimensions,
(1.16)

where r is the distance from a fixed origin to a general field point.

1.3.5  Resonant Frequencies and Mode Shapes

An enclosed volume of fluid exhibits resonances in the same way as a structure does. At the acoustic resonances any excitation generally leads to a (theoretically) infinite response. In practical situations the resonance frequencies inform us of the frequencies at which the acoustic response appears to be significantly magnified.

Knowledge of the modal properties can be of great value. For example a particular car design may be such that that its structural resonant frequencies coincide with the acoustic resonances of the car interior, having the apparent effect of magnifying the noise. Re-designing the car so that the two sets of resonant frequencies do not coincide could significantly reduce the interior car noise.

In acoustic problems the eigenvalues of the Helmholtz equation correspond to the resonant frequencies and the corresponding eigenfunctions to the mode shapes. They are the wavenumbers k* and the mode shapes f* that satisfy the Helmholtz equation

Ñ2 f*(p) + (k*)2 f*(p) = 0     (p Î D)
subject to a homogeneous boundary condition of the form
a(p) f(p) + b(p) v(p) = 0    (p Î S) .
The solutions of the eigenvalue problem are related to the shape of the domain and the nature of the boundary condition. The numerical determination of the resonant frequencies and mode shapes of an enclosed fluid are considered in Chapter 6.

1.3.6  Units of Measurement

The units of the acoustic properties considered in this text are not always stated. Table 1.B shows the standard units that generally apply. In the case of the velocity, the velocity potential and the sound pressure, the quantities are complex-valued. These are phasar quantities; their complex value expresses both their magnitude and relative phase.

Table 1.B: Standard Units
Property Unit
mass kg
distance m
density kg/m3
sound pressure N/m2 or Pa
velocity m/s
velocity potential no units
power W
intensity W/m2
frequency Hz
wavenumber no units

1.3.7  Acoustic Media: Air and Water

In linear acoustics, different acoustic media are simply reflected in the change in scaling factors that relate quantities such as wavenumber and frequency. The scaling factors can be found from tabulated values of the density r of the fluid and the speed at which sound propagates through the fluid c. Note also the density of the fluid generally varies with other conditions such as the temperature of the medium.

The two most important acoustic media are those of air and water. Typically air at 20° celcius and one atmosphere has a density of 1.29 kg/m3 and speed of sound of 334 m/s. Water at 4° celcius has a density of 1000 kg/m3 and the speed of sound is 1524 m/s. From Section 1.3, equation (1.6) it can be deduced that n = 53.2 k for air and n = 242.6 k for water under the stated conditions. From equation (1.7) it can be deduced that p = i 431 k f for air and p = i 1524 ×103 k f for water under same conditions.


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