Sound and Vibration
n
S
und Source
This material is protected by copyright and cannot be used or reproduced in any form without the written permission from:
The Marcus Wallenberg Laboratory, KTH, SE-100 44 Stockholm, SWEDEN
Program JEP-31018-2003 based on the Swedish book “Ljud och Vibrationer” used at KTH.
Chapters 1-12 are translated from “Ljud och Vibrationer” by Hans Bodén, Ulf Carlsson,
Ragnar Glav, Hans-Peter Wallin, and Mats Åbom by Robert Hildebrand
Chapters 13, 15 and 16 are written by Hans Bodén Chapter 14 is written by Ulf Carlsson and Hans Boden Chapter 17 is written by Mats Åbom
CONTENTS
1 INTRODUCTION
1.1 The field of Sound and Vibration
1.2 Job Market for Sound and Vibration Engineers 1.3 Development
1.4 Principles, examples and countermeasures
2 FUNDAMENTAL CONCEPTS
2.1 Fundamental and applied mechanics 2.2 Definitions of sound and vibration fields 2.3 Peak value, mean value RMS-value and power 2.4 Longitudinal waves in gases and liquids
2.4.1 Longitudinal plane waves 2.4.2 Spherical waves
2.5 Diffraction
2.6 Models in room acoustics 2.6.1 Geometrical acoustics 2.7 Waves in solid media
2.8 Frequency analysis of sound
2.8.1 Time and frequency domain 2.9 Levels and DECIBEL
2.10 Filters
2.10.1 Band pass filters
2.10.2 Octave and third octave filters 2.11 Summation of sound fields, interference 2.12 Summation of frequency components 2.13 Important formulas
3 INFLUENCE OF SOUND AND VIBRATION ON MAN AND EQUIPMENT
3.1 The ear and hearing
3.1.1 The ear’s function 3.1.2 Measures of hearing 3.1.3 Measures of noise 3.1.4 Speech and masking
3.1.5 The influence of noise on man 3.1.6 Hearing injuries
3.1.7 Hearing protection 3.1.8 Sound quality 3.2 Effects of shock nd vibration
3.3 Standards 3.3.1 ISO 3740 , ISO 3747, 3.3.2 ISO 2631-1, ISO 2631-2 3.3.3 ISO 5349 3.3.4 ISO 8662 3.3.5 ISO 4866
3.4 Regulations and recommendations 3.4.1 Machines 3.4.2 Vehicles 3.4.3 Work environment 3.4.4 Buildings 3.4.5 External noise 3.5 Important formulas
4 SIGNAL ANALYSIS AND MEASUREMENT TECHNIQUES
4.1 Complex numbers and rotating vectors 4.2 Fourier methods in sound and vibration
4.2.1 Fourier series 4.2.2 Fourier transforms 4.2.3 Parseval’s relationships
4.3 Measurement systems for sound and vibration 4.3.1 The measurement chain
4.3.2 Microphones 4.3.3 Accelerometers
4.3.4 Mounting of accelerometers
4.3.5 Calibration of transducers and measurement systems 4.4 Important formulas
5 VIBRATIONS OF SIMPLE MECHANICAL SYSTEMS
5.1 Mechanical power 5.2 Linear systems
5.2.1 One degree of freedom systems 5.2.2 Two degree of freedom systems 5.2.3 Multi degree of freedom systems 5.2.4 Frequency response functions 5.2.5 Damping
5.2.6 Mechanical-electrical circuits
6 THE WAVE EQUATION AND ITS SOLUTIONS IN GASES AND LIQUIDS
6.1 The wave equation in a source-free medium 6.1.1 Equation of continuity
6.1.2 Equation of motion
6.1.3 The thermodynamic equation of state 6.1.4 The homogenous linearised wave equation 6.2 Solutions to the wave equation
6.2.2 Harmonic solution for free one-dimensional wave propagation 6.2.3 Sound intensity for free one-dimensional wave propagation 6.2.4 Energy and energy density for free one-dimensional wave propagation
6.2.5 General solution for free spherical wave propagation 6.2.6 Harmonic solution for free spherical wave propagation 6.2.7 Sound intensity for free spherical wave propagation 6.3 Important formulas
7 REFLECTION TRANSMISSION AND STANDING WAVES
7.1 Reflection and transmission of plane waves
7.1.1 Normal incidence against a rigid boundary
7.1.2 Normal incidence at a boundary between two elastic half spaces 7.1.3 Plane wave propagation in three dimensional space
7.1.4 Non-normal incidence at a boundary between two elastic half spaces
7.1.5 Non-normal incidence at a boundary between a fluid and a solid 7.2 Eigen-frequencies and eigen-modes
7.2.1 Eigen-frequencies and eigen-modes in rooms 7.3 Important formulas
8 THE WAVE EQUATION AND ITS SOLUTIONS IN SOLIDS
8.1 Introduction
8.2 Wave propagation in infinite and semi-imfinite media 8.3 Quasi-longitudinal waves in beams
8.3.1 The wave equation for quasi-longitudinal waves in beams 8.3.2 Quasi-longitudinal waves in infinite beams
8.3.3 Quasi-longitudinal waves in finite beams
8.3.4 Reflection and transmission of quasi-longitudinal waves at area changes
8.3.5 Standing quasi-longitudinal waves in beams 8.4 Torsional waves in axles
8.4.1 The wave equation for torsional waves in straight cylindrical axles 8.4.2 Torsional waves in straight axles
8.5 Bending waves in beams and plates
8.5.1 The bending wave equation for beams and plates 8.5.2 Bending waves in an infinitely long beams 8.5.3 Bending waves in finite beams
8.5.4 Dispersion
8.5.5 Reflection and transmission at a boundary between two beams 8.5.6 Standing waves in beams
8.5.7 Standing waves in plates 8.6 Mechanical impedance and mobility 8.7 Damping in solid structures
8.7.3 Losses in built up structures
8.7.4 Damping of beams and plates using absorbing material 8.7.5 Mathematical description of damping
8.7.6 Experimental determination of damping 8.8 Important formulas
9 ROOM ACOUSTICS
9.1 Energy methods
9.1.1 Energy balance for simple an coupled systems
9.1.2 Relationship between wave theory and energy based methods 9.2 Room acoustics
9.2.1 Sabine’s equation 9.2.2 Sound fields in rooms 9.2.3 Acoustic absorbers
9.2.4 Sound transmission through walls 9.3 Important formulas
10 SOUND GENERATION MECHANISMS
10.1 Monopoles 10.2 Dipoles 10.3 Quadropoles
10.3.1 Examples of quadropole sources 10.4 Influence of boundaries
10.4.1 Examples of hard and soft surfaces 10.5 Line sources
10.6 Sound radiation from vibrating structures 10.6.1 Infinite plane surfaces
10.6.2 Finite plates with bending vibrations 10.7 Point excited plates
10.8 Flow generated noise
10.8.1 Scaling laws for flow generated noise 10.8.2 Whistling
10.9 Important formulas
11 VIBRATION ISOLATION
11.1 Types of isolation
11.2 General about vibration isolation 11.3 Measures of vibration isolation 11.4 Prediction of vibration isolation
11.5 Models for prediction of vibration isolation
11.5.1 Rigid mass – ideal spring – rigid foundation 11.5.2 Flexible foundation
11.5.3 Wave propagation in the isolator 11.5.4 Non-rigid machine
11.6.1 Design of vibration isolators
11.6.2 Methods for improving vibration isolation 11.6.3 Commercial vibration isolators
11.6.4 Dynamic stiffness 11.7 Important formulas
12 SOUND IN DUCTS
12.1 Principles for sound reduction in ducts 12.1.1 Insertion and transmission loss 12.1.2 Requirements on silencers 12.2 Sound propagation in ducts
12.2.1 The modified wave equation 12.3 Reactive silencers
12.3.1 Area changes 12.3.2 Expansion chambers 12.3.3 Side branch resonators 12.4 Electrical – acoustic circuits
12.4.1 Four-pole theory 12.5 Resistive silencers
12.6 Important formulas
13 INDUSTRIAL NOISE AND VIBRATION CONTROL
13.1 Motivation for industrial noise control
13.2 Systematic approach to industrial noise control 13.3 Noise control at the source
13.3.1 Noise generated by fluctuating forces in structures 13.3.2 Noise generated by fluid flow
13.4 Noise control during the propagation path 13.4.1 Control of structure borne sound 13.4.2 Control of airborne borne sound 13.5 Noise control at the receiver
13.6 References
14 MACHINE CONDITION MONITORING
14.1 Introduction
14.2 Basic ideas of machine monitoring
14.3 Typical defects in gears and rolling bearings 14.4 Vibrations of gears and bearings
14.4.1 Vibration characteristics of non-defective gears 14.4.2 Vibration characteristics of non-defective bearings 14.4.3 Vibrations of defective gears
14.4.4 Vibrations of defective bearings 14.5 Monitoring methods
14.5.3 Cepstral methods 14.5.4 Envelope methods 14.6 Machine condition indicators
14.6.1 RMS-value, peak-value and crest factor 14.6.2 Kurtosis
14.6.3 Defect severity index 14.7 Residual time to failure estimation 14.8 Measurement techniques
14.8.1 Instrumentation 14.8.2 Data acquisition 14.8.3 Signal filtering
14.8.4 Normalized order analysis 14.9 User interface
14.10 Signal processing tools 14.11 References
15 VEHICLE NOISE AND VIBRATION CONTROL
15.1 Motivation for vehicle noise and vibration control 15.2 Character of vehicle noise
15.3 Measurement of exterior vehicle noise 15.4 Vehicle noise sources
15.4.1 Engine noise
15.4.2 Exhaust and intake noise 15.4.3 Cooling system noise 15.4.4 Tyre-road noise 15.4.5 Aerodynamic noise 15.5 Vehicle noise and vibration control
15.5.1 Engine noise control
15.5.2 Exhaust and intake noise control 15.5.3 Interior noise and vibration control 15.6 References
16 NOISE AND VIBRATION IN PIPES AND DUCTS
16.1 Sound generation in pipes and ducts
16.1.1 Turbulent boundary layer generated sound 16.1.2 Sound generation by pipe discontinuities 16.1.3 Control valve sound generation
16.1.3.1 Classification of valves 16.1.3.2 Examples of valve types 16.1.3.3 Valve noise source mechanisms 16.2 Sound transmission in pipes
16.2.1 Fluid-borne sound 16.3.2 Structure-bone sound 16.3 Sound radiation from pipes
16.3.2 Excitation by fluid-borne sound 16.3.4 Radiation from pipe openings 16.4 Noise control techniques
16.4.1 Noise control at the source
16.4.2 Noise control during the propagation path 16.4.3 Control of structure borne sound
16.4.4 Reduction of sound radiation
17 SOUND GENERATION FROM FLUID MACHINES
17.1 Classification of fluid machines 17.2 Flow generated sound
17.2.1 The high Mach-number range 17.2.2 The case of liquids discontinuities 17.2.3 The character of the sound 17.3 Noise control
CHAPTER ONE
INTRODUCTION
Acoustics can be regarded as the science of sound and vibration. Sound today refers not only to those mechanical wave motions in air that give rise to sensations of hearing, but even to low-frequency (infrasonic) and high-frequency (ultrasonic) motions that cannot be sensed by hearing, as well as analogous wave motions in, for example, water (underwater acoustics). In solid materials, one speaks instead of vibrations or structure-borne sound.
The phenomenon of hearing has fascinated mankind all through the ages. The mathematical theory of sound propagation can be said to have begun with Isaac Newton (1642 - 1727), whose work Principia (1686) contained a mechanical interpretation of sound as pressure pulses propagating in a medium. A more solid mathematical and physical groundwork of theory was provided by Euler (1707 – 1783), Lagrange (1736 – 1813), and d’Alembert (1717 – 1783). That development took place just as continuum mechanics and field theory began to take form, and the wave equation was formulated for functions of space and time. The modern theory of sound and vibrations is the product of the efforts of these mathematical physicists.
1.1 THE FIELD OF SOUND AND VIBRATION
In today’s well-developed, technological society, the number of systems that emit sound and vibrations is steadily increasing. Examples are machines, vehicles, and processes of all types, in which driving forces and engine power are constantly. Examples are machines, vehicles, and processes of all kinds, in which driving forces and engine power are continually being increased even as simultaneous efforts are made to hold down weight and materials usage. This implies the need for an ever more intensive research and development effort to identify and alleviate noise and vibration disturbances, and satisfy the needs of mankind for an acceptable environment.
The fundamentals of Sound and Vibrations are part of the broader field of mechanics, with strong connections to classical mechanics, solid mechanics, and fluid dynamics. The subject of Sound and Vibrations encompasses the generation of sound and vibrations, the distribution and damping of vibrations, how sound propagates in a free field, and how it interacts with a closed space, as well as its effect on man and measurement equipment.
Technical applications span an even wider field, from applied mathematics and mechanics, to electrical instrumentation and analog and digital signal processing theory, to machinery and building design. Several of the more important areas are worthy of particular mention:
Figure 1-1 Acoustics spans such
diverse areas as biology, art, the natural sciences and technology. The proposed subdivision of the field (adjacent) covers, accordingly, many aspects and fields of science. The unshaded area describes the activity at
a typical university sound and vibration laboratory. (Source: From
R.B. Lindsay, who published the "acoustic wheel" in the Journal of the Acoustical Society of America 1964, vol 36)
NATURAL
SCIENCES TECHNICAL SCIENCES
LIFE
Machinery and Vehicle Acoustics deals with constructive measures to bring about
machines, vehicles, and processes that are quieter and vibrate less; that requires knowledge of how sound and vibrations are generated, and how that generation relates to such physical parameters as flow velocities, masses, stiffnesses, losses, and geometry, for example. The most common reason that sound arises, in technical applications, is that a time-varying force excites vibrations of a mechanical structure, which then radiates sound. We can convince ourselves of that by knocking on a tabletop. The surrounding air is influenced by the vibrating structure, and responds with contractions and expansions. The mechanical form of energy we call sound has arisen. Analysis of the mechanisms of sound generation helps us to answer the question of why it sounds differently when we hit a tabletop with the soft part of the index finger, than it does when we hit it with the steel tip of a ball-point pen, and why it is louder when we knock the middle of the table with our knuckles than when we do the same thing at the edge of the table.
The dull rumble of a Harley – Davidson motorcycle has become a defining characteristic – so important that the factory sought a patent on the sound to prevent competitors from plagiarizing it. That cash register click of a Mercedes door closing shut is something that other auto manufacturers strive for. The concept of Sound Quality is becoming ever more entrenched. Sound should convey a sense of product quality and reliability. The automobile industry has made pioneering efforts in this area and sound quality is given a high priority, along with such other important vehicle characteristics as road performance, safety and design. To describe sound, such subjective designators as “sharpness”, “rawness”, and “boxiness” are used. Several manufacturers have developed software packages that make it possible to modify the sound of products in order to mimic different design variations. The modified sounds are then judged by a “panel of listeners”. In the future, many consumer, industrial, and transportation products will be “sound-designed”.
Force
Vibrations
Acoustic radiation
Source Response Acoustic radiation
Technology Model Mathematical structure Three stages Examples: Geometries Masses Stiffnesses Losses Surface area
Mode shape (oscillation pattern) Resonances
Structure – air coupling Roughness forces
Gear tooth forces Mechanical imbalances Aerodynamic forces
Force
Roughness
Figure 1-2 Forces that cause
vibrations appear in countless situations. It can be a matter of a roller in a bearing exhibiting out-of-roundness, or perhaps small surface irregularities at the contact between a railway wheel and rail. The ability of the forces to induce vibrations depends on mechanical laws in which such parameters as the structure’s geometry, mass distribution, stiffness and losses come into play. The structure’s effectiveness as an acoustic radiator depends on the surface area, its oscillation pattern, and the coupling between the structure and the air at the surface of separation. Sound generation in connection with mechanical structures can be described in three stages:
pj Z v Sij i i Z Y F Sij ki k i k L i N i N = = = = =
∑
∑
∑
1 1 1 Figure 1-3 In a machine ascomplex as a car, the three stages of sound generation occur in many parallel chains. The velocity v at a specific point, induced by a force F at another specific point, can be described by a so-called frequency response function Y. Similarly, other frequency response functions Z can describe the relationships between the velocities on the surfaces and the sound pressure
p at an interior point. The
frequency response functions can, moreover, be combined to
describe all three stages in the propagation chain. By adding the contributions from all significant forces, via the dominant radiating surfaces, the total sound pressure at a location of interest in the interior is obtained. The noise in the interior comes mainly from three sources:
• The driveline, i.e., the engine, transmission, and drive axles. • The contact zone between the tires and the roadway. • Airflow over the car body.
Sound passes from the source into the passenger compartment in two distinct ways: as structure-borne and as air-borne sound. Structure-air-borne sound has essentially propagated in the form of vibrations from the source to the receiver, whereas air-borne sound had already radiated as sound, e.g., in the engine compartment, before its transmission into the passenger compartment (Sketch: Volvo Technology Report, nr 1 1988)
Forces Car Vibration i l Passenger Sound pressure
Flow Acoustics is the study of the direct generation of sound in an elastic gaseous or
liquid medium. The most common sound generation mechanisms are volume, force, and moment fluctuations in the medium, throughout which the elastic energy then spreads. Such phenomena are of great significance for noise from, for example, propellers, jet engines, fans, and vehicles, as well as for the propagation of sound in ducts.
Figure 1-4 Volvo’s wind
tunnel is used to find ways to reduce flow-induced sound. Mitigating such sound typically requires an even flow over the body, as well as fine tolerances and good fits, especially at doors and other seals. Airflow over projecting details can cause whistling. The small-scale turbulence around the car body gives a roaring type of noise, and if there are openings an airstream can sometimes create whistling sounds (Photos: Volvo Technology Report, nr 1 1988)
Room Acoustics, or Building Acoustics, deals with how sound fields are built up in
various types of rooms and enclosed spaces, as well as how sound is transmitted through different types of structures, such as walls and systems of joists.
Figure 1-5 Heavy
insulating surfaces effectively mitigate sound transmission from one enclosed space to another, as from, for example, the engine compartment to the cabin of a truck. For vehicles such as ships, cars, trains and aircraft, however, low weight is also a critical demand. Enormous efforts are therefore made in the transportation industry to bring about light, yet effective, designs for sound reduction. In the
picture, the roof of a passenger car has been mounted in the opening between a sound reflective “reverberant room” at MWL, KTH (seen), and an adjacent sound absorbing ”anechoic room” (not seen). Using microphones and mathematical models for the sound interaction with the measurement rooms, the sound insulating properties of the car roof can be deduced (Photo: HP Wallin, MWL)
Signal analysis is an important part of the science of sound and vibrations. The associated
experimental methodology is primarily based on transducers, such as microphones and accelerometers, that convert sound and vibrations into equivalent electrical signals for further analysis. Until the 1960’s, most acoustic measurement instrumentation was analogue; then, digital computer technology arrived on a broad front. A numerical algorithm, FFT (Fast Fourier Transform), that transformed signals from the time domain (signal strength as a function of time) to the frequency domain (signal strength as a function of frequency), was a breakthrough in experimental methodology.
The Sound and Vibration subject area offers a wealth of opportunities for both the theoretically-inclined and the more practically / experimentally-oriented who are interested in applying themselves towards the improvement of machinery and vehicle designs, or towards quieter workplaces and societal environments.
Figure 1-6 To solve a
noise problem, in which roof vibrations are suspected as the direct source, the car is driven on a chassis dynamometer.. The roof motion is registered as a function of time with the help of a motion sensor - an accelerometer. Transforming the signal to the frequency domain, i.e., expressing its strength as a function of frequency, often greatly facilitates interpretation. Such a transformation is carried out by electrical filters or by a computer. That broad subject is called signal analysis. Its mathematical foundation is derived from mathematical statistics and from Fourier methods. In the case illustrated, a poorly made transmission is to blame. A shaft in the transmission, rotating at 1800 revolutions per minute, is bent or out-of-balance, giving rise to a dominant vibration disturbance at 30 Hz.
(Sketch: Brüel & Kjær, Structural Testing, Part 1)
Signal analysis Time Amplitude
Signal
Figure 1-7 The strength of sound is often given in dB. A change of a single dB is hardly noticeable. An increase
of 8-10 dB is perceived as a doubling of the degree of disturbance. In order to adjust for variations in the sensitivity of the ear at different frequencies, corrected values are often used. The result is called Sound Level, and indicated in units of dB(A). (Diagram: ASF, ”Bullerbekämpning” [in Swedish], 1977, Illustrators: Anette Dünkelberg /Arne Karlsson)
1.2 JOB MARKET FOR SOUND AND VIBRATION ENGINEERS
The task of minimizing sound and vibration in mechanical constructions falls primarily upon those who are responsible for their design and analysis, i.e., primarily engineers with mechanical, vehicle, and machinery backgrounds.
Such issues have a great deal of relevance these days, and industry is therefore preoccupied with them. It is usually larger manufacturing companies that have the greatest need for engineers in this field. The vehicle industry employ many sound and vibration engineers but also other industrial sectors that manufacture products in which some type of energy conversion takes place (compressors, separators, turbines, fans, appliances, etc.) have a great need for this kind of knowledge.
There are, moreover, many consulting firms in the field. Others that have a need for specialists in this area include national and local authorities that have regulatory responsibilities, as well as national research organizations that have the task of dproducing new knowledge.
Normal conservation
Train 100 meters away
(100 km / h) Eccentric press Pain threshold
Manual grinding Air-cooled electric motor 50 kW Spray painting Weakest
perceivable Sound
Quiet bedroom Impact
riveting Coarse grinding Chainsaw
Near a jet plane starting up Highest sound level that can be attained Sound insulated lounge
1.3 DEVELOPMENT
Figure 1-8 Swedish billboard demonstrating the marketing value of acoustic performance, describing the
“world’s quietest dishwasher” as “Unbelievably unhearable”) (Photo: HP Wallin, MWL)
Classical acoustics was summarized by Lord Rayleigh in his fundamental treatise "The theory of sound" 1894-96. That classical theory serves as the basis for the modern science of sound and vibrations. Lord Rayleigh received the Nobel prize in physics in 1904 for his discoveries in the field of optics.
The field of noise control engineering started to develop in in the 1930’s. Development on a larger scale came in thethe 1950’s in connection with for instance the effort to build quiet submarines and civil jet engine airplanes. The knowledge acquired spread to other areas of machinery acoustics. In Sweden Atlas Copco was one of the
Today, technical specifications on sound and vibration performance are made for a large share of the products that are delivered by manufacturing industry. The EU has brought about further demands on products to be sold in Europe, with respect to sound and vibration performance. Quality oriented manufacturers consider quiet, vibration-free products as a crucial quality characteristic and a marketable feature, so that all larger manufacturers tend to have departments responsible for sound and vibration performance. In the future, we will see improved and more easily used computer-based computational tools, and a continued development of cheap, personal computer-based systems for measurement and diagnostics. An example of the development of new technology is the so-called active sound and vibration control. The method is based on the use of, for example, microphones registering a disturbing sound field. Making use of automatic control methodologies, an “anti-noise” (phase inverted sound) is emitted that, under some conditions, can eliminate the disturbing field in an effective way.
Commercial systems of that type exist already in, for example, ventilation systems and for automobile interiors and airplane cabins. In the future, we can expect corresponding systems on the vibration side as well. Today, vibration isolators, primarily of rubber, are inevitably used to prevent engine vibrations in an automobile from spreading into the car body. By installing parallel electrodynamic vibrators that generate reversed-phase forces, those disturbing forces that manage to pass through the isolators can be counteracted.
Kontrollenhet
Varvtalsgivare
Signal från motor Signal från motor
Högtalare Mikrofon
Figure 1-9 Cross section of the cabin of a turbo-prop SAAB 340 airplane with active noise control. The
microphones register the sound at a number of points and transfer the electrical signals to the control unit. The signals can be treated to drive the speakers in such a way (”antiphase”) as to reduce the noise level in the cabin. The tachometer signals from the engines help to fine tune the automatic control in the control unit. (Source: Ny Teknik)
Signal From motor Signal From motor
Tachometer Controller Microphone Loudspeaker
1.4 PRINCIPLES, EXAMPLES AND COUNTERMEASURES
The following pages give some examples of principles and applications in the field of sound and vibrations. On the left side, the underlying principles are presented, and on the facing right side, examples and countermeasures. Source: Asf, Bullerbekämpning (in Swedish), 1977.
Rapidness of a process determines the high frequency content
Figure 1-10a (Sketch: Asf, Bullerbekämpning, 1977, Illustrator: Claes Folkesson).
The faster that force, pressure, or velocity changes occur, the higher the frequency content of the resulting sound. A fast ping pong ball gives a high frequency pop when it hits the table, while a slow handball bounces against the floor with a dull, low frequency sound.
Principle
Slow impact against the floor – low frequency sound
Rapid impact against the table – high frequency
Figure 1-10b (Sketch: Asf, Bullerbekämpning, 1977, Illustrator: Claes Folkesson).
Sound level
Angular gear teeth
Rounded gear teeth High-pitched Low-pitched tones
Example - Countermeasure
In the primitive tooth configuration, the teeth slap together so that the forces between them rise and fall rapidly. The high-pitched tones are then strong. The more effort is made to modify the tooth configuration, the more softly they can be made to mesh together. Finally, the forces can be made to rise and fall again slowly. The high-pitched tones are then no longer so dominant. Since the peak force
Force on a tooth Angular gear Rounded gear teeth Force on a tooth Time Time
Make vibrating surfaces as small as possible
Figure 1-11a (Sketches: Asf, Bullerbekämpning, 1977, Illustrator: Claes Folkesson).
An object with small surfaces can vibrate very strongly without radiating a great deal of noise. The lower the frequency of the disturbing tones, the greater the surface area before it becomes a disturbing noise source. Since there is practically always a risk of vibrations when dealing with machinery, the shells and housings used should be as small as possible.
Principle
The electric shaver vibrations are transmitted into the large glass shelf and the resulting noise level is high.
The vibrations are no longer transmitted and the noise diminishes.
Figure 1-11b (Sketch: Asf, Bullerbekämpning, 1977, Illustrator: Claes Folkesson). Oil tank Pump Motor Instrument panel Instrument panel moved to the wall
Example:
The hydraulic aggregate was a powerful noise source. Since the wall vibrations of the oil tank were damped by the oil itself, most of the noise was radiated by the instrument panel.
Countermeasure:
The panel was separated from the aggregate,
reducing the radiating surface area, and thereby even the noise level.
Densely perforated sheet emits little noise
Figure 1-12a (Sketch: Asf, Bullerbekämpning, 1977 Illustrator: Claes Folkesson).
Large vibrating shells cannot always be avoided. They give off a lot of noise. The reason for their sound radiation is that the vibrating sheet pumps the air to and from, like the piston of a pump. If the sheet is perforated, then it “leaks” and the pumping effect is weakened. The reduction in sound radiation is many times greater than the mere reduction in surface area. Alternatives to perforated sheet are nets and gratings.
Sound level Principle
Perforated sheet metal Unperforated sheet metal
Figure 1-12b (Sketch: Asf, Bullerbekämpning, 1977, Illustrator: Claes Folkesson).
Shield over drive belt and flywheel, of unperforated sheet
Perforated sheet
Example:
The shield over the flywheel and drive belt constituted a strong noise source. The shield was fabricated of unperforated sheet metal.
Example:
The shield over the flywheel and drive belt constituted a strong noise source. The shield was fabricated of unperforated sheet metal.
Countermeasure:
A new shield was fabricated from perforated sheet and wire netting. One of the noise sources of the press was thereby eliminated.
Wind tone is removed by a changed profile or a small disturbing element
Figure 1-13a (Sketch: Asf, Bullerbekämpning, 1977, Illustrator: Claes Folkesson).
When sound flows past an object at certain speeds, a strong pure tone called a Strouhal tone can arise. By extending the dimension of the object in the direction of the airflow, with a “tail” for example, or by disturbing the regularity of the object profile, the tone can be prevented. In a duct, a resonance can amplify a Strouhal tone so much that the duct can be damaged.
Air Flow
Regular pattern of vortices gives a strong tone
Length extension Small disturbing objects
Irregular vortex pattern Irregular vortex pattern
Figure 1-13b (Sketch: Asf, Bullerbekämpning, 1977, Illustrator: Claes Folkesson).
Wind
Sheet iron spiral Chimney
Example: The shield over the
flywheel and drive belt
constituted a strong noise
source. It was fabricated of
unperforated sheet metal.
Countermeasure: A new shield
was fabricated from perforated
sheet and wire netting. One of
the noise sources of the press
was thereby eliminated.
Pure tones can be cancelled with sound in anti-phase
L2
L1
Figure 1-14a (Sketch: Asf, Bullerbekämpning, 1977, Illustrator: Claes Folkesson).
When the sound only consists of a single tone, or several such within a narrow frequency band, it can be completely or partially cancelled out in an interference muffler. It consists of a branched duct in which sound propagates through two separate paths that subsequently recombine with different time delays. In its simplest variation, shown in the figure, the path difference L1-L2 determines the frequencies at which sound reduction
occurs. The time-delayed sound behaves as if in anti-phase.
Figure 1-14b (Sketch: Asf, Bullerbekämpning, 1977, Ill: Claes Folkesson).
Interference muffler
Inlet
Outlet Branches of varying lengths
Example:
When the frequency of the disturbing tone, or the temperature of the gas, varies in time, the effective frequency band of the muffler can be widened by a variation of the path length difference through multiple paths. The improvement obtained at the nominal frequency is, however, somewhat less than in the preceding variation. The interference damper is suitable for use
The ASU Sound & Vibration Lab. At the Faculty of Engineering, Ain Shams University
The Sound and Vibration Laboratory at the Faculty of Engineering, Ain Shams University was established in 2004 by a European Union Grant (JEP-31018-2003) within the TEMPUS Program. This is the first laboratory in Egypt specialized in sound and vibration teaching and research. The establishment of the laboratory and the development of the courses were done in cooperation with:
- The Marcus Wallenberg Laboratory for Sound and Vibration Research (MWL) at the Royal Institute of Technology (KTH) in Sweden.
- Institute of Sound and Vibration Research (ISVR) at the University of Southampton in United Kingdom.
Our mission is to produce a new generation of Egyptian engineers and researchers in the field of sound and vibration. ASU-SVL welcomes research institutions, industry and others to cooperate with our staff and use the laboratory facilities.
The laboratory hosts the Acoustical Society of Egypt, whose mission is to group all engineers, researchers and students in Egypt interested in the field of sound and vibration. ASU-SVL has joined the X3-Noise Aircraft External Noise Network in Europe acting as the regional focal point for MEDA Countries in this network. X3-Noise is funded within the Sixth Framework Programme.
The activities in the lab are divided into three main domains: education, research and consultancy.
The lab is equipped with the state-of-the art sound and vibration measurement equipment including different types of analyzers, transducers, calibrators, and accessories. There is an anechoic room (80 m3), a reverberation room (80 m3), and an acoustic flow facility. There is a teaching lab of 13 computers working as data acquisition systems to be used in lab exercises in different courses.
CHAPTER TWO
FUNDAMENTAL CONCEPTS
The aim of this chapter is, partly, to give an overview of the subject area of sound and vibrations, before the more detailed descriptions that follow, and partly to present and define a number of important concepts early enough that technically interesting problems may be treated in parallel with the main presentation.
In the introduction, we shall relate the subject of sound and vibration (sometimes expressed as "vibroacoustics") to the mechanical sciences as a whole, describe what types of mechanical elastic waves can arise, as well as the conditions for their existence, and define important quantities which specify sound and vibration fields. In the section “Diffraction”, we will examine the conditions under which a sound field can bend around different objects. Using models from the subject of room acoustics, we will make a short preliminary survey of different methods for analyzing how sound propagation and sound fields interact with various types of rooms.
Sound and vibration disturbances can only be tracked as functions of time, but are often more effectively analyzed and characterized as functions of frequency. Important concepts, such as the time and frequency domains, are defined, and filtering and frequency analysis are described.
2.1 BASIC AND APPLIED MECHANICS
The science of sound and vibration is a part of applied mechanics. This can be subdivided as in Figure 2-1.
Figure 2-1 Proposed subdivision of mechanics.
In statics, systems are examined in equilibrium states, i.e., the object considered is neither accelerated nor decelerated, and often has, in practice, no velocity. In particle mechanics, one studies the motion of the center of gravity of an object. The object / particle has three degrees of freedom, i.e., translations which can be described in a Cartesian coordinate system. In order to describe rigid body movement, six degrees of freedom are needed: three translations and three rotations.
In applied mechanics one studies the behavior of solid, liquid and gaseous media, including deformation, wave propagation, tension, and fracture, when these media are subjected to physical agents of various types, such as forces and temperature shifts. In strength of materials one studies strain and deformation properties with the objective of properly dimensioning a construction for good strength and stability. In fluid mechanics one describes various aspects of the motions of, above all, fluids and gases. A typical problem from this field would be to improve the lift of an airplane wing, for example, or reduce the head loss (pressure drop) across a ventilation duct. Vibroacoustics covers everything from the basics of how sound and vibrations are generated and how they propagate to the question of how vibrations in a solid structure, a combustion engine for example, give rise to acoustic radiation.
The division of the fields of mechanics as in Figure 2-1 is a mere simplification which can be adjusted and supplemented in many ways. A model from particle mechanics can, for example, be applied in vibroacoustics to explain the appearance of a certain tone when we blow over the mouth of a bottle, as in Figure 2-2.
Figure 2-2 The tone that arises
when we blow over the bottle opening can be determined by methods from particle mech-anics. The phenomenon is call-ed a Helmholz resonator. It was already employed in the amphitheaters of ancient Greece where clay pots were used as resonators, see chapter 10. (Sketch (far left):Asf, Buller-bekämpning, 1977, Ill: Claes Statics m echanicsParticle bodyR igid
m echanics
Strength of M aterials Fluid M echanics
V ibroacoustics
Fundam ental M echanics A pplied m echanics
Mass Force
Figure 2-4a A loudspeaker generates
longitudinal waves in which particles oscillate parallel to the direction of wave propagation.
Figure 2-4b The hand shaking the rope generates a
transverse wave in which particles oscillate perpendicular to the direction of wave propagation.
2.2 DEFINITION OF SOUND AND VIBRATION FIELDS
Sound and vibration waves are mechanical elastic waves, and thus the conditions for their existence are that the medium possess mass and elasticity. If a mass particle is displaced from its equilibrium position, the elastic forces will seek to return it to its original position. The particle influences the surrounding particles and, in this way, a disturbance propagates in the medium. Sound waves transport relatively little mechanical energy; thus, as is familiar to all from everyday life, speech is not a particularly exhausting activity. A speaking person sends out only a few thousandths of a Watt. Nobody is ever going to be able to cook potatoes by yelling at them. This means, on the other hand, that machines driven at high power levels have almost unlimited capacities to excite acoustic fields; small flaws can convert a share of the available mechanical power into acoustic disturbances. In vibroacoustics there are two classes of waves: longitudinal waves and transverse waves. Longitudinal waves have a particle motion which is parallel to the direction of wave propagation, see Figure 2-4a, while transverse waves have a particle motion which is perpendicular to the direction of propagation as in Figure 2-4b. These shall be described in further detail in later chapters.
Particle Displacement
Wave Propagation
Wave Propagation Particle displacement
In a gas or a fluid, at a certain point in space rG and time t, an acoustic wave can be
described by the acoustical field quantities sound pressure p( trG, )[Pa] and particle velocity uG( trG, ) [m/s]. Sound pressure variations are normally very small deviations of the
ambient pressure, and the particle velocity is small compared to the speed of sound. Figure 2-3 A disturbance in water on a pond gives rise
to a radial wave pattern. These water (or gravitation) waves are nevertheless driven, in contrast to sound and vibration waves, by a balance between the water’s inertia and gravitational effects. (Photo: Klas Persson)
pt Sound Pressure, p
Atmospheric Pressure p0
5
Figure 2-5 An acoustic field ordinarily
implies only small disturbances. Normal speech at a distance of several meters, for example, gives a sound pressure p of a few hundredths Pa superimposed upon atmospheric pressure p, which is about
2.3 PEAK VALUE, MEAN VALUE, RMS-VALUE, AND POWER
Before going any further, we recall some formulas from electrical engineering which are used to characterize signals, for example sound pressure p(t). A harmonic signal is a signal which can be described by a sine or cosine function as
p(t) = pˆsin(ω t + ϕ), (2-1)
where p(t) is the instantaneous, time-dependent sound pressure,
pˆ is the peak value or simply the amplitude,
ω = 2πf is the angular frequency, ϕ is the phase angle.
The time-averaged mean value of a signal, marked by an overbar, is dt t p T p T
∫
= 0 ) ( 1 , (2-2)where T [s]is the time over which the average value is determined. The root mean square or RMS value is marked by p~ and is defined according to
∫
= T dt t p T p 0 2() 1 ~ . (2-3)The rms-value is a very important, and oft-used, form, since it gives information about the time average of the signal power content.
T t peak-peak (t) p ~ = 2 ^ p p p ^ p
The relation between the peak value and the rms-value for an arbitrary signal is called the peak factor or crest factor
p p
TF = ˆ ~ . (2-4)
For a harmonic signal, the following relationship applies between the rms-value and the peak value:
2 ˆ
~ p
p= . (2-5)
Figure 2-6 The amplitude
characteristics of a harmonic signal, of sound pressure for example, can be described in various ways. The period T is the time required for one complete oscillation.
Exercise 2-1
Show that equation 2-5 is valid for a harmonic signal.
n
S
W
Sound Source
The instantaneous mechanical power is the product of the instantaneous force and the instantaneous velocity. In acoustics, consequently, the instantaneous acoustic power
) , ( tr
W G [W], which is transported through a surface S with a normal vector nG, as in Figure
2-7, is
∫
= S dS n t r u t r p t r W(G, ) (G, )G(G, )G . (2-6)In acoustics, we are typically interested in the time average of power quantities W(rG), see chapter 3.
2.4 LONGITUDINAL WAVES IN GASES AND FLUIDS
In gases and fluids, shear stresses are, as a rule, small enough to be neglected. Consequently, only longitudinal mechanical elastic waves can exist in such media. Longitudinal waves are characterized by a particle velocity which is parallel to the direction of wave propagation (see Figure 2-4a). Two cases are considered here for longitudinal waves: plane waves and spherical waves. More complicated wave fields can be constructed from these simple special cases.
2.4.1 Longitudinal plane waves
Longitudinal plane waves are characterized by the condition that points with the same acoustical state, i.e., the same sound pressure and particle velocity, form parallel planes. Figure 2-8 shows the acoustic field of an infinite duct with a harmonically (i.e., sinusoid-ally) oscillating piston at one end.
Direction of
Propagation
λ
Harmonic vibrational velocity
v(t) = v sin(2 ft). π
Figure 2-8 A harmonically oscillating
piston in an infinitely long duct gives rise to a plane longitudinal acoustic wave that propagates in the duct. The frequency of the wave is the same as the piston oscillating frequency. The quantity 2π f is the so-called angular
frequency, designated by ω. The distance λ between two planes in the medium with the same acoustic state is the wavelength in the medium.
Figure 2-7 The acoustic power W over
an area S in an acoustic field is the product of the sound pressure, particle velocity, and area.
When the piston begins to move forward in the cylinder, it compresses the air before it. That compression propagates at a speed completely independent of the particle velocity, hereafter referred to as the disturbance propagation speed c [m/s]. After a half period, the piston moves in the opposite direction and creates an expansion in the medium, which also moves at the speed c through the medium. After period T [s], the disturbance will have propagated the distance λ [m], so that the following elementary relation applies
f c cT = = λ (2-7) or λ f c= , (2-8)
where c is the disturbance’s propagation speed or the sound speed, f is (the disturbance’s) frequency,
λ is the wavelength.
In air at normal pressure and temperature, c ≈ 340 m/s.
For the case of a free plane longitudinal wave, i.e., wave propagation without reflections, there is a very simple relationship between the field quantities sound pressure p and particle velocity ux as well as the time average of the sound power W . Sound
pressure and particle velocity are always in phase, i.e., they attain their respective maxima and minima simultaneously. The relation between them can be expressed
) , ( ) , (xt 0cu xt p =ρ x , (2-9)
where ρ0 [kg/m3] is the density in the undisturbed medium (in air at normal pressure and
temperature ρ0 ≈ 1.21 kg/m3) and
c is the sound speed.
The time-averaged sound power W becomes, according to (2-2)
dt t W T W T
∫
= 0 ) ( 1 . (2-10)Putting (2-6) and (2-9) in (2-10) gives
dt c S t x p T W T
∫
= 0 0 2( , ) 1 ρ , (2-11)which, in accordance with (2-3), gives
c S p
W =~2 ρ0 . (2-12)
If we study the sound power per unit area, the so-called sound intensity IG [W/m2], the
time-average of the x-component is obtained as
c p S W
Ix = =~2 ρ0 . (2-13)
Thus, for a free plane wave, the time average of the sound intensity is proportional to the square of the rms-value of the sound pressure.
In linear vibroacoustics, in more general terms, the time-averaged sound power is proportional to the square of the rms-amplitude of the relevant field quantity, as
2 2 ~ ~ p p C W = ∝ . (2-14)
This important relation implies that if the constant of proportionality C is known, we can determine the time-averaged sound power from a measurement of the rms sound pressure alone, using a pressure-sensitive microphone. That is usually considerably simpler than determining the particle velocity and making use of (2-6) directly. For a free plane wave, C = S/ρ0c according to (2-12). Note that if the losses in the medium are neglected, and
since the wave doesn’t spread through an expanding volume, then time-averaged quantities are independent of distance to the source, i.e., time-averaged sound intensity and sound pressure amplitude are independent of spatial position.
2.4.2 Spherical and cylindrical waves
In the preceding section on plane waves, we were able to show that when the wave does not suffer losses, certain quantities remain independent of the distance to the source. If the source is an arbitrarily placed sphere and all points on its surface oscillate radially at the same amplitude and phase, or if the source radius a is small compared to the sound wavelength, then the source will produce spherical waves, as shown in Figure 2-9.
The mechanical power W emitted into the medium by the pulsating sphere spreads over an
ever-expanding spherical area (fig 2-10); thus, the time-averaged sound intensity is
2 4 r W Ir = π . (2-15) r 2r 3r
λ λ
aλ λ
Figure 2-9 A spherical source which
oscillates at the same amplitude and phase over its entire surface area gives rise to spherical wave propagation.
Figure 2-10 In spherical wave propagation, sound power is divided over an ever-increasing area. The intensity decreases to one fourth its original value for a doubling of the distance to the source, and to one ninth when the distance is tripled.
Examples of real phenomena giving rise to spherical wave propagation are loudspeakers and the outlets of exhaust pipes, provided that the dimensions of the source are small compared to the wavelength, i.e., at sufficiently low frequencies as implied by (2-8). As is evident from Figure 2-9, the curvature of the wave fronts decreases with increasing radius. For engineering purposes, the waves can be considered (locally) plane for radii r > λ / 3, and (2-13) is then applicable even for this spherical wave case. The rms sound pressure can then be expressed in the form
2
0 4
~ cW r
p= ρ π . (2-16)
If the source is, instead, and infinitely long cylinder, the entire surface of which oscillates with a uniform phase and amplitude, then cylindrical waves arise; see Figure 2-11.
r 2r 3r S 2S 3S
The mechanical power, often given in units of power per unit length in the case of a line source, is distributed over a cylindrical area, so that the sound intensity can be expressed
r W
Ir = '2π , (2-17)
where W' [W/m] is the sound power per unit length. Examples of sound sources that can be regarded as cylindrical are electrical distribution cables, pipes, ducts, transport belts at breweries, and heavily trafficked roads. A pre-requisite is that the distance from the source be small compared to the length of the source.
2.5 DIFFRACTION
Diffraction takes place in all types of wave propagation. Water waves are not noticeably affected by the presence of a thin mooring post in the water. The waves roll on as if the post did not exist. On the other hand, we know that behind a break wall in a protected harbor, or behind a narrow spit of land jutting into the water, a shadow zone free of waves develops. The relationship between the size of the hindrance and the wavelength determines how the wave motion is bent about it.
Visible light has an approximate wavelength of 10-7 m, whereas typical human
speech has a wavelength of about 1 m. For this reason, we can hear someone speaking from behind a pole without being able to see her at the same time. Thus, wave motions with wavelengths large in relation to the obstacle are little influenced by it and spread
Figure 2-11 An infinitely long cylindrical
source oscillating with uniform phase and amplitude over its entire surface gives rise to cylindrical waves.
Exercise 2-2
Go to an open area, without any reflecting objects, such as buildings and the like, in the vicinity. Ask a companion to stand about 5 meters away, facing away from you, and take turns voicing an extended
(i) ooooooo... (“oo” as in “food”, not “foot”) (ii) ssssssss...
Note: the oo-sound has a frequency of about 250 Hz and the s-sound is a hiss with a frequency around 6000 Hz. Compare the wavelengths with the diameter of the head. These diffraction phenomena, as well as the
persistence of free plane waves as planar and of free spherical waves as spherical, can be explained with the help of Huygen’s principle: "Every point on a wave front can be described as the center of a secondary wave field, a so called elementary wave. The new position [a moment later] of the wave front is the tangent to the set of these elementary waves ", see Figure 2-12.
In Figure 2-13a, it is seen that at such low frequencies that the wavelength is large in relation to the opening in the wall, Huygen’s principle implies a spherical wave propagat-ion from the opening. If the frequency is high, and the wavelength thereby small in relatpropagat-ion to the opening, as in Figure 2-13b, then the wave propagates as a beam with shadow zones on each side of it.
a) b)
Figure 2-12 Huygen’s principle can be used to show that free plane waves remain plane, and spherical waves remain spherical as they propagate. In a), the tangent to the so-called elementary waves is seen to build a plane wave front, and in b) the corresponding principle for spherical waves is shown.
λ λ λ Shadow zone a) b) Spherical propagation λ Shadow zone
Figure 2-13 a) shows sound transmission through a hole, small in comparison to the sound wavelength. From the opening, spherical wave propagation occurs. b) shows the case of hole that is large with respect to the wavelength. In the middle, the wave passes relatively unhindered, while shadow zones are built up at the sides.
Exercise 2-3
Noise from roads and railways is an enormous problem. A common attempt at a solution is to install noise walls or barriers.
How should noise barriers be placed?
a) Is it in the high or the low frequency range that noise barriers can be expected to provide the greatest benefit?
b) Is the greatest effect obtained from the barrier when the source is near or far from it? c) Where should the receiver be located with respect to the barrier, to receive the greatest benefit?
Figure 2-14 For highways with average vehicle speeds exceeding 70 km/h, the dominant noise is that generated at the contacts between tires and the road surface.
2.6 ROOM ACOUSTICS MODELS
In many situations, sound interacts with a closed space such as rooms in dwellings, concert halls, or industrial facilities, but even automobile or railway car interiors, or ship or airplane cabins. Knowledge of sound propagation and sound fields in such spaces is therefore an essential part of acoustics. When sound from a source reaches one of the room’s bounding surfaces, a share of the sound power is reflected back into the room and a share absorbed by the wall. In room acoustics, three distinct methods or models are used to describe sound propagation and the sound fields that arise.
At low enough frequencies that the wavelength of sound is of the same order of magnitude as the dimensions of the room, wave theoretical room acoustics is a powerful tool. It turns out that when some of the room’s dimensions are whole multiples of half the wavelength, the incident and reflected waves interact such as to bring about standing wave fields, which then dominate the sound field in the room. The particular frequencies at which that occurs are called eigenfrequencies, or resonance frequencies in ordinary speech. The wave pattern, with its characteristic sound maxima and minima, is called an eigenmode, or simply mode; see Figure 2-15.
Figure 2-15 When a dimension of a closed space, an airplane cabin or a vehicle interior for example, is a whole multiple of the half wavelength, then constructive interference arises between incident and reflected waves. A standing wave pattern with nodes and anti-nodes results. The frequencies at which that happens are called eigenfrequencies, and the standing wave patterns are called eigenmodes.
(Sketch: Brüel & Kjær, Technical Review).
Direct wave
Reflected wave
Observation point
Sound source
At higher frequencies, the eigenfrequencies are so tightly spaced that, for practical reasons, we must choose another mathematical description. In chapter 8, we will study statistical energy methods for so called diffuse fields, see Figure 2-16. In practice, the demands for such a field are seldom fulfilled. The actual field is then called a reverberant field. The third method, geometrical room acoustics, is described in the next section.
2.6.1 Reflections and geometrical acoustics
A free wave, incident upon a reflecting surface with irregularities much smaller than a wavelength λ, changes its direction, i.e., is reflected, in a predictable way. In Figure 2-17, the wave fronts of the incident and reflected waves are marked. It is convenient, at times, to indicate a wave by an arrow. The arrow is perpendicular to the wave fronts and points in the direction that the wave propagates. Using Huygen’s principle, we can show that: (i) Against a plane surface, a plane wave is reflected as a plane wave and a spherical
wave as a spherical wave.
(ii) The direction of the incident wave, the normal to the reflecting surface, and the direction of the reflected wave, all lie in the same plane.
(iii) The angle of incidence θi is equal to the angle of reflection θr, see Figure 2-17.
Figure 2-16 Near a source, direct
unreflect-ed sound dominates; such sound comprises the so called direct, or free field in which the power from the source is distributed over an ever expanding volume, resulting in a halv-ing of sound pressure for a doublhalv-ing of dist-ance, according to relation (2-16) between sound power and sound pressure for spheric-al waves. Further away, sound that has been reflected at least once dominates; that sound constitutes the so-called reverberant field. With a stricter demand, that sound pressure be constant and independent of distance to the source, sound must arrive at an observat-ion point from all directobservat-ions, with random phase; it then fulfills the definition of an (ideal) diffuse field.
Figure 2-17 With the help of
Huygen’s principle, we can show that a plane wave, incident on a reflecting surface, is reflected as a plane wave, and that the
angle of incidence θi is
equal to the angle of
reflection θr. θ i θ r Incident plane wave n Wave fronts Reflected plane wave Wave fronts λ λ
If the reflecting surface is rigid, the sound pressure amplitudes and phases of the incident and reflected waves are equal the point of reflection. An observer is influenced by both the direct sound from the source and the reflected sound. We can describe the sound field above the reflecting surface by a superimposition of the direct wave field direct from the actual source with the direct field of an identical, imagined mirror source, placed at the same distance from the surface, but on the opposite side; see fig 2-18.
Source Mirror source Wave fronts Rigid surface Observer d d Reflectedspherical wave Incident spherical wave
In geometrical acoustics, a sound wave is represented by an arrow in the direction of wave propagation, just as a light wave is represented in geometrical optics. We can regard a wave as a beam originating from the source. The method can be used to explain how a parabolic microphone functions; see Figure 2-19.
Geometrical acoustics is primarily applied in the design of auditoriums. The purpose is to bring about an even distribution of sound, without focuses and shadow zones; see Figure 2-20. The limitation of the method is that typically only the first, or possibly even the second, reflection can be studied before it becomes impractical to follow the “sound trail”.
Figure 2-19 In a parabolic microphone, the
reflected waves are focused into a focal point, at which the microphone is located, to maximize the amplification.
Figure 2-18 A spherical wave incident upon a reflecting surface is reflected as a spherical wave. If the surface is rigid, the reflected wave can be regarded as equivalent to a direct field from an imagined mirror source, identical to the actual source, at the same distance from the surface, but on the opposite side. Parabola Microphone Incident waves Stage Roof Parquet Balcony Figure 2-20 In geometrical
acoustics, sound waves are regarded as beams. The method is often used in the design of large musical auditoriums. The limitation is that it is typically only possible to follow the first few reflections of the sound waves.
(Source: Brüel & Kjær, Measurements in Building
2.7 WAVE TYPES IN SOLID MEDIA
Solid media can sustain both normal and shear stresses, and thereby resist both volume and shape changes. That implies that in solids, in contrast to gases and liquids, not only longitudinal waves, but even transverse waves, can exist. Transverse and longitudinal waves can also, in combination with each other, build special types of waves, e.g., bending waves. Here, we will acquaint ourselves with some important special cases. Figure 2-21a illustrates a longitudinal wave and Figure 2-21b a transverse wave. When the medium is infinite in the direction of wave propagation, so that no reflections occur, we speak of free wave propagation.
Utbredningsriktning
Partikelrörelse Partikelrörelse Utbredningsriktning
a) b)
Figure 2-21 Important wave types in solid media.
a) Longitudinal wave: particle motion is parallel to the direction of disturbance propagation. b) Transverse wave: particle motion is perpendicular to the direction of disturbance propagation. In a bounded medium, reflections occur at the boundaries. At certain frequencies, the incident and reflected waves interfere, or interact, such that standing wave patterns arise. These frequencies are called, as in section 2.6, eigenfrequencies or resonance frequencies, and the oscillation pattern is called an eigenmode or mode.
Bending oscillations Longitudinal oscillations Tuning fork Bending oscillations Table-top
Figure 2-22 When a tuning fork is
stricken, bending oscillat-ions take place in the legs, essentially in the first eigenmode. That disturb-ance excites a longitudinal oscillation at the same frequency. That latter, in its turn, excites bending waves in the tabletop. As is well known, it isn’t until that large table surface has been put into contact with the tuning fork, and begun vibrating itself, that we begin to hear the tuning fork well.
Exercise 2-4
Hold a long measuring stick, extended about 1.5 m from your grasp, and shake it transversally at about 1 Hz. It will now (hopefully) be oscillating in its first eigenmode. Increase the frequency until you find the second eigenmode. Observe the antinodes, where there is a large amount of bowing, i.e., deformation, and the nodes, at which there is none.
First eigenmode Second eigenmode
Node Anti- Node
2.8 CHARACTERIZATION OF SOUND ACCORDING TO FREQUENCY
Sound can be characterized by its frequency content. For mankind, audible sound is that which falls in the 20 – 20 000 Hz range. For frequencies lower that 20 Hz, we speak of infrasound, and over 20 000 Hz of ultrasound. Most acoustic phenomena are frequency-dependent. It is well known that different sound sources have different character, see Figure 2-23. Slowly changing and “soft” events mainly generate low frequency sound, while short and fast events mainly generate high frequency sound. We can be convinced of that by slapping the soft part of the thumb against the tabletop, and then do the same with a ballpoint pen.
As is evident from Figure 2-23, the audible region spans over a range of wavelengths from 17 m to 17 mm, which is of fundamental significance for the types of noise control measures that can be undertaken. Analysis of the frequency content of a sound is therefore of great importance in the field of sound and vibration.
1 10 20 100 1000 10000 20000
17 17 10. -3
Frekvens [Hz] Våglängd [m]
Infraljud Hörbart ljud Ultraljud
Skärande bearbetning Fartygsmaskiner Luftblåsning Sågning Smältugn Vindbuller Ekolod Bilar, tåg etc Människa Hund Fladdermus Hörområden Ljudkällor 340 3,4 0,34 λ
Figure 2-23 Classification of sound according to frequency, and the relation between frequency and wavelength
in air with a sound speed c = 340 m/s. Frequency ranges of various sound generation mechanisms. (Source: Asf, Bullerbekämpning, 1977.)
2.8.1 Time and frequency domains
Figure 2-24a shows a harmonic signal of frequency f0 as a function of time. It can also be
described as a function of frequency, as in Figure 2-24b. All power in the signal is concentrated at the frequency f0. We have thus introduced the, for vibroacoustics
fundamental, concepts of the time and frequency domains. These are equivalent concepts, and we can choose to describe a signal in either of these domains. We can only record a signal as a function of time. It can thereafter be transformed into the frequency domain by frequency analysis, i.e., by methods from Fourier analysis.
T=1/f0 Signal Time Amplitude Frequency f0 a) b)
Figure 2-24 Harmonic signal in a) the time domain, and b) the frequency domain.
Infrasound Audible sound Ultrasound
Wavelength [m]
3.4
Frequency [Hz]
340 17 0.34 17*10-3
Audible range Mankind
Dogs Bats Wind noise
Ship machinery
Cars, Trains, etc. Smelting oven Cutting tools Sawing Air blasting Sound Sources: Echo
Jean Baptiste Fourier (1768-1830) demonstrated more than a century ago that all periodic signals can be described by a summation of harmonic signals. We can illustrate that by means of the three-dimensional Figure 2-25. A periodic signal, e.g., a sound pressure p(t) that repeats with period T, can be written
) ( )
(t p t nT
p = + , n = 1, 2, 3,... (2-18)
Periodic signals are very common in engineering applications. They can be sound pressures or vibrations arising from, for example, rotating machines whose sound and vibration generation is repeated in an identical fashion in cycle after cycle. In Figure 2-25, a signal is shown (heavy line) together with its harmonic components (thin line), at frequencies fn. Every periodic signal can be expressed as the sum of harmonic signals with
a so-called Fourier series (see chapter 3) according to
∑
= + = N n n n nf t p t p 1 0 ) 2 cos( ˆ ) ( π ϕ , (2-19)where pˆn is the peak value of the n-th harmonic component,
f0 = 1/T and nf0 are the frequencies of the n-th harmonic component,
n
ϕ is the phase angle.
1/T 0 Frequency [Hz] Time [s] T 2T/3 T/3 0 2/T 3/T 4/T Amplitude
The description of a signal in the frequency domain is usually called a (frequency) spectrum and each line, frequency component, is called a tone or a spectral line. In order to obtain a complete description, the phase angle of each frequency component is also required. Typically, however, we are only interested in the amplitudes of the frequency components. The frequency spectrum is very useful when the signal is to be analyzed, e.g., it provides the opportunity to distinguish every frequency component, even in cases in which a single frequency is dominant in the signal.
Figure 2-25 A periodic signal
can be described in both the time and the frequency domains. In the time domain, the signal is represented by its variation in time, and in the frequency domain by the amplitude of the harmonic signals it is built up of. Here, the phase angles ϕn are
zero for all frequency components.