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Acoustics of Fluid Media 1 is intended for undergraduate students and engineering students, as well as graduate students and professionals in the industry who are increasingly faced with the need to consider acoustic constraints in the design of new products.
The physical principles and theoretical foundations of acoustics in fluids are first developed, including reflection and refraction of plane and spherical waves. The book then introduces notions of signal processing applied to sound waves, followed by radiation from surface or volume acoustic sources and the use of Green's functions, as well as the description of diffraction and scattering phenomena. The final chapters are devoted to sound propagation in ducts and room acoustics.
Each chapter is accompanied by a limited number of exercises, ranging from the simple application of formulas to problems requiring a more advanced theoretical analysis or a numerical solution. Throughout the book, the theoretical results are illustrated with numerous figures obtained from measurements or numerical simulations resulting from the evaluation of complex formulas or from the use of a finite element solver.
Daniel Juvé is an Emeritus Professor at the École Centrale de Lyon, France, in the Fluid Mechanics and Acoustics Laboratory. His main research interests are noise generation by turbulent flows and sound propagation in the atmosphere.
Marie-Annick Galland is an Emeritus Professor at the École Centrale de Lyon, France, in the Fluid Mechanics and Acoustics Laboratory. She conducts research in noise control using active control systems and/or passive acoustic materials with an application to aircraft's nacelle liners.
Vincent Clair is an Assistant Professor at the École Centrale de Lyon, France, in the Fluid Mechanics and Acoustics Laboratory. He specializes in the numerical simulation of turbomachinery noise and acoustic propagation through turbulent flows.
List of Abbreviations, Acronyms and Symbols xi
Preface xv
Chapter 1 Equations of Linear Acoustics 1
1.1. Validity of the assumptions of linear acoustics and a perfect fluid 1
1.2. Linearized equations of fluid dynamics 3
1.3. The wave equation 5
1.3.1. The special case of ideal gases 6
1.3.2. The velocity potential 7
1.3.3. Validity conditions for the linearization of equations 8
1.4. Acoustic energy, acoustic intensity and source power 9
1.4.1. Definition of acoustic energy and acoustic intensity 9
1.4.2. Acoustic sources 10
1.5. Harmonic waves 12
1.5.1. Definition of harmonic waves 12
1.5.2. Average acoustic energy and acoustic intensity 15
1.6. Boundary conditions 16
1.6.1. Fluid-solid and fluid-fluid interfaces 16
1.6.2. Specific acoustic impedance 18
1.7. Exercises 19
Chapter 2 Plane Waves and Spherical Waves 21
2.1. Plane waves 21
2.1.1. Plane waves in the time domain 21
2.1.2. Harmonic plane waves 25
2.1.3. Evanescent plane waves 28
2.1.4. Angular spectrum of plane waves 28
2.1.5. Near-field acoustic holography 29
2.2. Spherical waves 31
2.2.1. Time-averaged intensity and power 33
2.2.2. Harmonic spherical waves 34
2.3. Cylindrical waves 36
2.4. Exercises 37
Chapter 3 Sound Levels, Spectral Analysis and Notions on Human Sound Perception 43
3.1. Energy and average power 44
3.2. Sound levels 45
3.3. Energy and power spectral densities 46
3.4. Correlation functions 47
3.5. Random signals 48
3.6. Random signals and correlations, some examples 50
3.7. Frequency bands 52
3.8. Loudness, equal loudness contours and frequency weightings 55
3.9. Characterization of non-stationary acoustic signals 58
3.9.1. Statistical levels 59
3.9.2. Equivalent level, "Day ", "Evening" and "Night" levels 60
3.9.3. Transient signals: sound exposure level and energy spectral density 61
3.10. Exercises 63
Chapter 4 Reflection and Transmission Phenomena 67
4.1. Reflection and transmission of normally incident plane waves 68
4.2. Reflection of a harmonic plane wave on an impedance surface 69
4.3. Multilayer media 72
4.3.1. Impedance transfer 72
4.3.2. Transmission through three media 73
4.3.3. Transmission of a harmonic plane wave through a thin wall 74
4.4. Reflection and transmission of plane waves at the interface between two fluids: oblique incidence 76
4.5. Plane wave transmission through a thin wall: oblique incidence 81
4.6. Piston-tube coupling 85
4.7. Reflection of spherical waves and image sources 87
4.8. Exercises 92
Chapter 5 Sound Sources and Green's Functions 97
5.1. Volume sources 98
5.2. Green's functions for the wave equation 99
5.3. General solution of the wave equation in free-space 100
5.3.1. Monopole sources: far-field and compact source region 101
5.3.2. Dipole sources 104
5.3.3. Quadrupole sources 107
5.4. Green's functions and general solutions of the Helmholtz equation 108
5.4.1. Monopole sources 109
5.4.2. Dipole and quadrupole sources 110
5.5. One-dimensional and two-dimensional Green's functions 111
5.5.1. Two-dimensional Green's function of the wave equation 111
5.5.2. One-dimensional Green's function of the wave equation 113
5.5.3. Green's functions of the Helmholtz equation in one- and two-dimensions 113
5.6. Reciprocity of Green's functions 115
5.7. Green's functions for a fluid in uniform subsonic motion 116
5.7.1. Green's function of the convected Helmholtz equation 119
5.8. Moving sources and the Doppler effect 119
5.8.1. Point mass source in arbitrary motion 119
5.8.2. Arbitrarily moving point forces 122
5.8.3. Sources in uniform rectilinear motion 124
5.9. Exercises 126
Chapter 6 Integral Formulations for Sound Radiation and Diffraction 129
6.1. Radially oscillating sphere 130
6.1.1. Harmonic vibrations: radiation impedance 131
6.2. Acoustic radiation from bending vibrations 134
6.2.1. Radiated power and radiation impedance 138
6.2.2. Acoustic radiation from a finite plate 140
6.3. Kirchhoff-Helmholtz integral 141
6.3.1. Irregular frequencies 145
6.3.2. Expressing the surface integral in terms of pressure and velocity 146
6.3.3. Kirchhoff-Helmholtz formula and acoustic field extrapolation 147
6.4. Adapted Green's functions 148
6.5. Integral formulation associated with the wave equation 149
6.5.1. Bursting balloon 150
6.6. Radiation from planar structures: Rayleigh integral 152
6.6.1. Radiation from a circular piston 155
6.7. Rayleigh integral in the time domain 160
6.8. Exercises 161
Chapter 7 Diffraction and Scattering 163
7.1. Diffraction by a semi-infinite screen 163
7.2. Scattering by a rigid cylinder 169
7.2.1. Scattering cross-sections 173
7.3. Rayleigh scattering by a generic obstacle 177
7.4. Scattering by non-rigid obstacles and the Born approximation 180
7.4.1. Scattering by inhomogeneities 180
7.4.2. The Born approximation 183
7.4.3. Validity of the Born approximation 185
7.5. Exercises 186
Chapter 8 Guided Waves 189
8.1. Sound propagation in a duct of constant cross-section 189
8.1.1. Propagating modes and evanescent modes 191
8.2. Duct of rectangular cross-section 192
8.2.1. Phase and group velocities: dispersion of higher modes 193
8.2.2. Modes and pairs of plane waves 195
8.3. Ducts of circular cross-section 196
8.4. Point source in a duct and Green's function 198
8.5. Propagation in a duct with absorbing walls 201
8.6. Influence of a uniform flow on modal propagation 204
8.7. Exercises 208
Chapter 9 One-dimensional Propagation in Ducts 211
9.1. Ducts of piecewise constant cross-section: transfer matrices 211
9.1.1. Impedance transfer 212
9.1.2. Cross-sectional area discontinuities 212
9.1.3. Expansion chambers 215
9.1.4. Bifurcations and acoustic filters 217
9.1.5. Transmission loss and insertion loss 220
9.1.6. End corrections 221
9.1.7. Helmholtz resonators 222
9.2. Webster horn equation 226
9.2.1. Propagation in ducts with a slowly varying cross-section 226
9.2.2. Horn families: exponential horns 227
9.3. Exercises 231
Chapter 10 Acoustics of Enclosures: Room Acoustics 233
10.1. Simple-shaped cavities 234
10.2. Modal approach 235
10.2.1. Distribution of the natural frequencies 238
10.2.2. Room acoustic response to a point source 240
10.3. Energy approach: Sabine's theory 241
10.3.1. Global energy balance 242
10.3.2. Diffuse field 242
10.3.3. Steady-state level: reverberation time 244
10.3.4. Eyring's formula 246
10.4. Influence of the atmospheric absorption 247
10.5. Random incidence absorption coefficient 247
10.6. Schröder frequency 248
10.7. Room critical distance 249
10.8. Coupled rooms: transmission loss of a panel 250
10.9. Measurements in the reverberation room of École Centrale de Lyon 251
10.10. Geometric room acoustics 253
10.11. Subjective effects 256
10.12. Exercises 261
Appendices 267
Appendix 1 Basic Fluid Mechanics and Thermodynamics 269
Appendix 2 Math Refresher 281
References 293
Index 297
In this chapter, we establish the equations that govern the propagation of small-amplitude acoustic waves in fluids under the simplest possible conditions. The fluid is considered as perfect, that is non-viscous and non-heat-conductive. Acoustic disturbances are regarded as small-amplitude perturbations of the ambient state of a time-independent homogeneous fluid at rest. External forces, such as gravity, are not taken into account.
These assumptions may seem very strong, and we will have to relax some of them in later chapters. However, they offer considerable advantages in terms of simplicity, while often remaining unrestrictive in practice. This simplicity makes it possible to emphasize the fundamental properties of acoustic waves, which are generally only slightly modified in more complex situations where, for example, the inhomogeneous nature of the medium will have to be taken into account. They also allow the construction of analytical solutions with very wide applications, which also serve as references for the numerical simulations that become necessary when the geometries of the problems under consideration become complex.
It is important to form a first qualitative idea on the legitimacy of the assumptions of a perfect fluid and linearization of fluid dynamics equations by performing order-of-magnitude analyses in a simplified situation. We thus consider a wave of frequency f chosen within the range of audible sounds, for instance, f = 1 kHz, and propagating through the air in the x1 direction only.
To evaluate the validity conditions of the linearization process, we consider the two components of acceleration in the Navier-Stokes equations (these equations are recalled in Appendix 1):
where u1 is the component in the x1 direction of the velocity associated with the propagation of an acoustic wave. The partial derivative of velocity with respect to time ?u1/?t is linear with respect to fluctuations, while its convective derivative u1?u1/?x1 exhibits a quadratic nonlinearity. The order of magnitude of the linear term is ?u1, where ? = 2pf is the angular frequency of the wave. That of the nonlinear term is , where ? is the spatial scale of the wave, called the wavelength. The wavelength is related to the angular frequency by ? = 2pc0/?, where c0 denotes the speed of propagation of acoustic waves in the medium under consideration; in air, the speed of sound is about 340 m.s-1. The ratio of the orders of magnitude of the nonlinear term to the linear term is therefore u1/c0 = Ma; this ratio defines the acoustic Mach number. We will see in Chapter 3 that a sound wave with a 94 dB level, which is perceived by humans as very intense and painful, is only associated with a root-mean-square (rms) value of pressure fluctuations of only 1 Pa. For this wave, the acoustic Mach number is extremely low, being about 10-5. In the most unfavorable situations, it will hardly exceed 10-3, which fully justifies why terms composed of products of fluctuations in the equations of motion can be neglected, and thus validates the linearization process of the equations.
To evaluate the validity of the perfect fluid assumption, we simply analyze the influence of viscous terms, since the thermal effects are typically of the same order of magnitude as them. The viscous term in the Navier-Stokes equations:
has an order of magnitude ?u1/?2, where ? is the kinematic viscosity of the fluid. The ratio of the linear acceleration term to the viscous term is therefore of the order , or c0?/?, some sort of local acoustic Reynolds number. For air, ? ~ 15×10-6 m2.s-1 and for a 1 kHz frequency, this number is about 106. This very high value of the Reynolds number ensures that viscous effects are negligible for the usual range of frequencies.
It is important to note, however, that the above reasoning is qualitative and only has a local value, that is to say on the scale of a wavelength. Viscous, thermal and nonlinear effects are cumulative, and their consequences can be significant if the distances traveled by waves correspond to a large number of wavelengths. As a case in point, very high frequency acoustic waves (greater than a hundred kilohertz) propagating in the air are very quickly attenuated by visco-thermal effects over distances of only a few meters. It will therefore sometimes be necessary to take into account dissipative effects, often in an approximate way by an a posteriori correction of a calculation made for a perfect fluid. This is, for example, the case in room acoustics, as we shall see in Chapter 10.
Since the fluid is now considered perfect and external forces are neglected, the equations of fluid dynamics are reduced to the system of Euler's equations (see Appendix A1.4):
where p, ?, s and Ui denote fluid pressure, density, entropy and velocity, respectively1.
The propagation medium is assumed to be time independent, homogeneous and at rest. The variables describing the ambient state (i.e. when there is no acoustic disturbance) are therefore uniform; they will be expressed using a "0" subscript. Since the medium is at rest, the ambient velocity is zero, U0 = 0. Acoustic disturbances, which are time and space dependent, will be indicated by a "prime" symbol. During the propagation of an acoustic wave, the different variables will thus be decomposed according to:
The disturbances are assumed to be small enough so that the products of fluctuations that will appear when the above decompositions are introduced into the equations of fluid dynamics can be neglected. This constitutes the fundamental assumption of linear acoustics.
We now outline the linearization procedure on the conservation of mass equation (or "continuity equation"):
which reduces to:
The last term of the left hand side of [1.10] is of second order as the divergence of a product of fluctuations. It is therefore neglected in the linear approximation, and the linearized continuity equation is finally written as:
To linearize the equations in which the total time-derivative appears, it can be observed that the total derivative of a fluctuation can be reduced to its partial derivative with respect to time, because:
by neglecting terms of order greater than or equal to 2. To obtain the linearized equations, thanks to the assumptions of homogeneity of the medium and the absence of ambient flow, any total derivative can therefore be replaced by a simple partial derivative with respect to time.
The system of linearized Euler's equations is thus written as:
The last equation shows that the entropy fluctuation associated with an acoustic disturbance is identically zero, which leads to an important simplification. The pressure then depends only on the density and the equation of state takes the simple form p = p(?, s0)= p(?).
For the equation of state [1.4], the process of linearization must be carried out differently insofar as there is no explicit form for it, except for the special but important case of ideal gases to which we will return later. The idea is to consider that the presence of acoustic waves only slightly modifies the ambient state; the perturbed variables can then be obtained through a Taylor-series expansion around the ambient state that is limited to the first order. It thus follows that:
Partial derivatives are taken at constant entropy (as recalled by the subscript "s") and evaluated at the ambient state. By definition, p(?0,s0) = p0 and only considering the first order in the linearization assumption, a simple relation of proportionality between pressure and density fluctuations is therefore obtained.
It is important to understand that the coefficient (?p/??)s,0 is a thermodynamic quantity characteristic of the medium in which acoustic waves propagate (but that it is independent of them, since it is evaluated at the ambient state). In thermodynamics, it is shown that this coefficient is strictly positive and it will later be seen that it is equal to the square of the propagation speed of acoustic waves (the speed of sound), denoted by c0:
We therefore have a linear system of three first-order equations for three variables, p', ?' and . These equations are generally rearranged to eliminate fluctuations in...
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