
- •Preface
- •Objectives of the Book
- •Style
- •Prerequisites
- •The Big Picture
- •Contents
- •1.1 Review of Complex Numbers
- •1.2 Complex Numbers in Polar Form
- •1.3 Four Equivalent Forms to Represent Harmonic Waves
- •1.4 Mathematical Identity
- •1.5 Derivation of Four Equivalent Forms
- •1.5.1 Obtain Form 2 from Form 1
- •1.5.2 Obtain Form 3 from Form 2
- •1.5.3 Obtain Form 4 from Form 3
- •1.6 Visualization and Numerical Validation of Form 1 and Form 2
- •1.8 Homework Exercises
- •1.9 References of Trigonometric Identities
- •1.9.1 Trigonometric Identities of a Single Angle
- •1.9.2 Trigonometric Identities of Two Angles
- •1.10 A MATLAB Code for Visualization of Form 1 and Form 2
- •2.2 Equation of Continuity
- •2.3 Equation of State
- •2.3.1 Energy Increase due to Work Done
- •2.3.2 Pressure due to Colliding of Gases
- •2.3.3 Derivation of Equation of State
- •2.4 Derivation of Acoustic Wave Equation
- •2.5 Formulas for the Speed of Sound
- •2.5.1 Formula Using Pressure
- •2.5.2 Formula Using Bulk Modulus
- •2.5.3 Formula Using Temperature
- •2.5.4 Formula Using Colliding Speed
- •2.6 Homework Exercises
- •3.1 Review of Partial Differential Equations
- •3.1.1 Complex Solutions of a Partial Differential Equation
- •3.1.2 Trigonometric Solutions of a Partial Differential Equation
- •3.2 Four Basic Complex Solutions
- •3.3 Four Basic Traveling Waves
- •3.4 Four Basic Standing Waves
- •3.5 Conversion Between Traveling and Standing Waves
- •3.6 Wavenumber, Angular Frequency, and Wave Speed
- •3.7 Visualization of Acoustic Waves
- •3.7.1 Plotting Traveling Wave
- •3.7.2 Plotting Standing Wave
- •3.8 Homework Exercises
- •4.2 RMS Pressure
- •4.2.1 RMS Pressure of BTW
- •4.2.2 RMS Pressure of BSW
- •4.3 Acoustic Intensity
- •4.3.1 Acoustic Intensity of BTW
- •4.3.2 Acoustic Intensity of BSW
- •4.5.1 Issues with Real Impedance
- •4.6 Computer Program
- •4.7 Homework Exercises
- •4.8 References
- •4.8.1 Derivatives of Trigonometric and Complex Exponential Functions
- •4.8.2 Trigonometric Integrals
- •5.1 Spherical Coordinate System
- •5.2 Wave Equation in Spherical Coordinate System
- •5.3 Pressure Solutions of Wave Equation in Spherical Coordinate System
- •5.4 Flow Velocity
- •5.4.1 Flow Velocity in Real Format
- •5.4.2 Flow Velocity in Complex Format
- •5.5 RMS Pressure and Acoustic Intensity
- •5.7 Homework Exercises
- •6.1 Review of Pressure and Velocity Formulas for Spherical Waves
- •6.2 Acoustic Waves from a Pulsating Sphere
- •6.3 Acoustic Waves from a Small Pulsating Sphere
- •6.4 Acoustic Waves from a Point Source
- •6.4.1 Point Sources Formulated with Source Strength
- •6.4.2 Flow Rate as Source Strength
- •6.5 Acoustic Intensity and Sound Power
- •6.6 Computer Program
- •6.7 Project
- •6.8 Objective
- •6.9 Homework Exercises
- •7.1 1D Standing Waves Between Two Walls
- •7.2 Natural Frequencies and Mode Shapes in a Pipe
- •7.3 2D Boundary Conditions Between Four Walls
- •7.3.1 2D Standing Wave Solutions of the Wave Equation
- •7.3.2 2D Nature Frequencies Between Four Walls
- •7.3.3 2D Mode Shapes Between Four Walls
- •7.4 3D Boundary Conditions of Rectangular Cavities
- •7.4.1 3D Standing Wave Solutions of the Wave Equation
- •7.4.2 3D Natural Frequencies and Mode Shapes
- •7.5 Homework Exercises
- •8.1 2D Traveling Wave Solutions
- •8.1.2 Wavenumber Vectors in 2D Traveling Wave Solutions
- •8.2 Wavenumber Vectors in Resonant Cavities
- •8.3 Traveling Waves in Resonant Cavities
- •8.4 Wavenumber Vectors in Acoustic Waveguides
- •8.5 Traveling Waves in Acoustic Waveguides
- •8.6 Homework Exercises
- •9.1 Decibel Scale
- •9.1.1 Review of Logarithm Rules
- •9.1.2 Levels and Decibel Scale
- •9.1.3 Decibel Arithmetic
- •9.2 Sound Pressure Levels
- •9.2.2 Sound Power Levels and Decibel Scale
- •9.2.3 Sound Pressure Levels and Decibel Scale
- •9.2.4 Sound Pressure Levels Calculated in Time Domain
- •9.2.5 Sound Pressure Level Calculated in Frequency Domain
- •9.3 Octave Bands
- •9.3.1 Center Frequencies and Upper and Lower Bounds of Octave Bands
- •9.3.2 Lower and Upper Bounds of Octave Band and 1/3 Octave Band
- •9.3.3 Preferred Speech Interference Level (PSIL)
- •9.4 Weighted Sound Pressure Level
- •9.4.1 Logarithm of Weighting
- •9.5 Homework Exercises
- •10.1 Sound Power, Acoustic Intensity, and Energy Density
- •10.2.2 Room Constant
- •10.2.3 Reverberation Time
- •10.3 Room Acoustics
- •10.3.1 Energy Density due to an Acoustic Source
- •10.3.2 Sound Pressure Level due to an Acoustic Source
- •10.4 Transmission Loss due to Acoustical Partitions
- •10.4.2 Transmission Loss (TL)
- •10.5 Noise Reduction due to Acoustical Partitions
- •10.5.1 Energy Density due to a Partition Wall
- •10.5.2 Sound Pressure Level due to a Partition Wall
- •10.5.3 Noise Reduction (NR)
- •10.6 Homework Exercises
- •11.1 Complex Amplitude of Pressure and Acoustic Impedance
- •11.1.3 Transfer Pressure
- •11.2 Complex Acoustic Impedance
- •11.3 Balancing Pressure and Conservation of Mass
- •11.4 Transformation of Pressures
- •11.5 Transformation of Acoustic Impedance
- •11.7 Numerical Method for Molding of Pipelines
- •11.8 Computer Program
- •11.9 Project
- •11.10 Homework Exercises
- •12.1.1 Equivalent Acoustic Impedance of a One-to-Two Pipe
- •12.2 Power Transmission of a One-to-Two Pipe
- •12.3 Low-Pass Filters
- •12.4 High-Pass Filters
- •12.5 Band-Stop Resonator
- •12.6 Numerical Method for Modeling of Pipelines with Side Branches
- •12.7 Project
- •12.8 Homework Exercises
- •Nomenclature
- •Appendices
- •Appendix 1: Discrete Fourier Transform
- •Discrete Fourier Transform
- •Fourier Series for Periodical Time Function
- •Formulas of Discrete Fourier Series
- •Appendix 2: Power Spectral Density
- •Power Spectral Density
- •Accumulated Sound Pressure Square
- •Sound Pressure Level in Each Band
- •References
- •Index

6.8 Objective |
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at (0, |
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at (0.1, 0, 0.1) [m] |
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at (0.1, 0, 10) [m] |
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Drawing not to scale |
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Divide the rectangular plate into m sections in the x-direction and n sections in the y-direction as:
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Use a time resolution of t ¼ 0.0001 [s] for the time history plot.
Use the function POINTSOURCE.m and the main program VibrationPlate.m to complete this project.
Write your group report and submit it as a single pdf file that includes the following items:
6.8Objective
1)Procedures
2)Your completed MATLAB script.
3)Output figures of the sound pressure at points A, B, C, and D
4)Output figures of the flow velocity at points A, B, C, and D
5)Comparison of the pressures at points A and B
6)Comparison of velocities at points A and C
7)Conclusion of the simulation results
Hint: This project is an extension of Example 6.3. You can use Example 6.3 as a reference for this project.

162 |
6 Acoustic Waves from Spherical Sources |
6.9Homework Exercises
Exercise 6.1
An acoustic pressure p(r, t) is created by a surface vibration of a spherical source with a radius a ¼ 12 ½m&. At a distance of r ¼ 10 [m], the following sound pressure is given:
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pðr ¼ 10, tÞ ¼ 0:02 cos |
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π ½Pa& ¼ |
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Answer the following questions:
a)What are the angular frequency ω and the wave number k of the radiation?
b)Calculate the sound pressure at any point in space outside of the sphere.
c)Calculate the flow velocity at any point in space outside of the sphere.
d)Calculate the surface velocity of the spherical source.
e)Calculate the sound intensity at any point outside of the sphere.
f)Calculate the sound power radiated from the source.
g)What are the period and wavelength of the radiation?
Use 415 [rayls] for the characteristic impedance (ρ0c) of air and 340 [m/s] for the speed of sound in air. Show units in the Meter-Kilogram-Second (MKS) system.
(Answers):
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ω ¼ 8 πc sec ; |
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6.9 Homework Exercises |
163 |
Exercise 6.2 (Reverse of Exercise 6.1)
A sound pressure p(r, t) is created by a surface vibration of a spherical source with a radius a ¼ 12 ½m&. Assume that the surface velocity of the sphere is given by:
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πÞh s i |
Answer the following questions:
a)What are the angular frequency ω and the wave number k of the radiation?
b)Calculate the sound pressure at any point in space outside of the sphere.
c)Calculate the flow velocity at any point in space outside of the sphere.
d)Calculate the sound pressure at r ¼ 10 [m].
e)Calculate the sound intensity at any point outside of the sphere.
f)Calculate the sound power radiated from the source.
Use 415 [rayls] for the characteristic impedance (ρ0c) of air and 340 [m/s] for the speed of sound in air. Show units in the Meter-Kilogram-Second (MKS) system.
(Answers):
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ω ¼ 8 πc sec |
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where cos ðϕÞ ¼ |
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Exercise 6.3
A sound pressure is created by the pulsating surface of a sphere with a radius a ¼
12 ½m&. Assume that the surface velocity of the sphere is:

164 |
6 Acoustic Waves from Spherical Sources |
uðr ¼ a, tÞ ¼ 4 cos 2πct
where c is the speed of the sound. At a distance r sphere, calculate the following:
a)Sound pressure amplitude
b)Sound intensity
c)Sound power (or sound pressure)
πh m i
2sec
¼5 [m] from the center of the
Note: This pulsating sphere cannot be treated as a small sphere source or a point source.
Use 415 [rayls] for the characteristic impedance (ρ0c) of air and 340 [m/s] for the speed of sound in air. Show units in the Meter-Kilogram-Second (MKS) system.
(Answers): (a) 158.18 [Pa]; (b) 30:15 mw2 ; (c) 9470.5 [w]
Exercise 6.4 (Point Source)
The sound pressure p(r, t) is created by a surface vibration of a spherical source with the radius a ¼ 201 ½m&. Assume that the surface velocity of the sphere is given by:
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Treat this small spherical source as a point source to answer the following questions:
a)What are the angular frequency ω and the wave number k of the radiation?
b)Calculate the source strength at r ¼ a and r ¼ 2a from the center of the sphere.
c)Use the source strength to calculate flow velocity u(r, t) at any point in space.
d)Use the source strength to calculate sound pressure p(r, t) at any point in space.
e)Calculate the sound intensity at any point.
f)Calculate the sound power radiated from the source.
Use 415 [rayls] for the characteristic impedance (ρ0c) of air and 340 [m/s] for the speed of sound in air. Show units in the Meter-Kilogram-Second (MKS) system.
(Answers):
ω ¼ 8 |
πc sec ; wave number : k ¼ |
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π m |
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6.9 |
Homework Exercises |
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w ¼ 6:3 10 4½w&
Exercise 6.5 (Point Source)
A sound pressure p(r, t) is created by a surface vibration of a small spherical source with radius a ¼ 251 ½m&. Assume the surface velocity of the sphere is:
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Treat this small spherical source as a point source to answer the following questions:
d)Calculate the source strength of the spherical source.
e)Calculate sound pressure p(r, t) at any point in space.
f)Calculate sound intensity at any point in space.
g)Calculate sound power radiated from the source.
Use 415 [rayls] for the characteristic impedance (ρ0c) of air and 340 [m/s] for the speed of sound in air. Show units in the Meter-Kilogram-Second (MKS) system.
(Answers):
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Qs ¼ 0:0603 h s |
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Chapter 7
Resonant Cavities
In the previous chapters, when we calculated the sound pressure radiated from a vibrating surface, we only considered forward waves but not returning waves. This is because we have not considered any reflecting surfaces yet.
From this chapter forward, we will study sound waves that are bouncing inside cavities, waveguides, and pipes. If we consider the pre-reflection waves as forward waves, the post-reflection waves will be backward waves. The resulting wave of the addition of a pre-reflection forward wave and its post-reflection backward wave is a standing wave because the amplitudes of the pre-reflection wave and its postreflection wave are (almost) the same.
In resonant cavities, the standing waves caused by the pre-reflection forward wave and the post-reflection backward wave will cause the air in the cavity to be resonant at certain frequencies. The resonance of air in cavities, if not considered properly, can be a serious design flaw. On the other hand, the resonance of cavities, if understood correctly, can be used as vibration absorbers in filter designs (Chapter 13).
In this chapter, natural (resonant) frequencies and their corresponding mode shapes of resonant cavities will be formulated. The discretized natural frequencies and mode shapes will be derived from standing wave solutions with constraints on boundary conditions. It can be difficult to fully comprehend and visualize standing waves in rectangular cavities because they propagate in 3D space. It is easier to first understand and formulate standing waves in 1D than in 3D. For this reason, we will first study the 1D standing waves between two walls and then extend the formulas to 2D and 3D.
A summary of formulas of 1D standing waves between two walls is listed below and will be derived in Section 7.1:
The natural frequency of an eigenmode (l, m, n) in an enclosure is:
© The Author(s), under exclusive license to Springer Nature Switzerland AG 2021 |
167 |
H. Lin et al., Lecture Notes on Acoustics and Noise Control, https://doi.org/10.1007/978-3-030-88213-6_7