- •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
3.8 Homework Exercises |
75 |
3.8Homework Exercises
Exercise 3.1 A complex exponential function p(x, t) is given as:
pðx, tÞ ¼ e jðωtþkx π2Þ ½CEP&
Show that when ωk ¼ c, the above complex exponential function p(x, t) satisfies the one-dimensional acoustic wave equation:
∂2 pðx, tÞ ¼ 1 ∂2 pðx, tÞ ∂x2 c2 ∂t2
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3 Solutions of Acoustic Wave Equation |
Exercise 3.2 A complex exponential function p(x, t) is given as: |
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pðx, tÞ ¼ e jðωt kx π2Þ |
½CEP& |
Show that when ωk ¼ c, the above complex exponential function p(x, t) satisfies the one-dimensional acoustic wave equation:
∂2 pðx, tÞ ¼ 1 ∂2 pðx, tÞ ∂x2 c2 ∂t2
Exercise 3.3 A complex exponential function p(x, t) is give as:
pðx, tÞ ¼ e jðωt kx π2Þ |
½CEP& |
Show that when ωk ¼ c, the above complex exponential function p(x, t) satisfies the one-dimensional acoustic wave equation:
∂2 pðx, tÞ ¼ 1 ∂2 pðx, tÞ ∂x2 c2 ∂t2
Exercise 3.4 A backward traveling wave p (x, t) with a phase shift (Form 2:REP) is given as:
p ðx, tÞ ¼ A cos ðωt þ kx þ ϕ Þ
where A is an amplitude. Show that if ωk ¼ c, the above trigonometric cosine function p(x, t) satisfies the one-dimensional acoustic wave equation:
∂2 pðx, tÞ ¼ 1 ∂2 pðx, tÞ ∂x2 c2 ∂t2
Exercise 3.5 Prove that the following relationship between a standing wave and the combination of a forward wave and a backward wave is true:
sin ðωtÞ sin ðkxÞ ¼ 21 ð cos ðωt þ kxÞ cos ðωt kxÞÞ
Exercise 3.6 Prove that the following relationship between a standing wave and the combination of a forward wave and a backward wave is true:
3.8 Homework Exercises |
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sin ðωtÞ cos ðkxÞ ¼ 12 ð sin ðωt þ kxÞ þ sin ðωt kxÞÞ
Exercise 3.7 Find the relations between phases θt, θx, ϕ+, and ϕ that satisfy the following relationship between a standing wave and the combination of a forward wave and a backward wave:
cos ðωt þ θtÞ cos ðkx þ θxÞ ¼ cos ðωt þ kx þ ϕ Þ þ cos ωt kx þ ϕþ |
ð3:2Þ |
(Answers): (You must show all of your work for full credit!)
ϕ ¼ θt þ θx ϕþ ¼ θt θx
Exercise 3.8 Find the relations between phases θt, θx, ϕ+, and ϕ that satisfy the following relationship between a standing wave and the combination of a forward wave and a backward wave:
2 sin ðωt þ θtÞ cos ðkx þ θxÞ ¼ sin ðωt þ kx þ ϕ Þ þ sin ωt kx þ ϕþ
(Answers): (You must show all of your work for full credit!)
ϕ ¼ θt þ θx ϕþ ¼ θt θx
Exercise 3.9 The following is a harmonic function p(x, t) of one-dimensional sound pressure in Cartesian coordinates:
hi
pðx, tÞ ¼ Re PsinðkxÞe jðωtÞ
where P is a real number.
a)Show that the harmonic function p(x, t) can be constructed by multiplying two trigonometric cosine functions as:
pðx, tÞ ¼ PcosðωtÞ sin ðkxÞ
78 |
3 Solutions of Acoustic Wave Equation |
b)Show that the harmonic function p(x, t) can be constructed by adding two trigonometric cosine functions as:
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Form 2.
Exercise 3.10 The following is a harmonic function p(x, t) of one-dimensional sound pressure in Cartesian coordinates:
hi
pðx, tÞ ¼ Re jP cos ðkxÞe jðωtÞ
where P is a real number.
(a)Show that the harmonic function p(x, t) can be constructed by multiplying two trigonometric cosine functions:
pðx, tÞ ¼ P sin ðωtÞ cos ðkxÞ
(b)Show that the harmonic function p(x, t) can be constructed by adding two trigonometric sine functions:
pðx, tÞ ¼ 2P ½ sin ðωt þ kxÞ þ sin ðωt kxÞ&
Note that each term in the above function has no phase and can be considered as Form 1.
Exercise 3.11 The following is a harmonic function p(x, t) of one-dimensional sound pressure in Cartesian coordinates:
pðx, tÞ ¼ Re hA sin kx |
π |
2 e jðωtÞi |
where A is a real number.
(a)Show that the harmonic function p(x, t) can be constructed by multiplying two trigonometric cosine functions:
pðx, tÞ ¼ A cos ðkxÞ cos ðωtÞ
(b)Show that the harmonic function p(x, t) can be constructed by adding two trigonometric cosine functions:
3.8 Homework Exercises |
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Exercise 3.12 Use the following combination of a forward wave p+(x, t) and a backward wave p (x, t) to answer every question of this problem:
p ðx, tÞ ¼ sin ωt þ kx |
π |
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pþðx, tÞ ¼ sin ðωt kxÞ
a)Calculate the standing wave (real number) produced by the forward wave and the backward.
b)Find the locations of the peaks and valleys in terms of wavelength.
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Peak: x |
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Chapter 4
Acoustic Intensity and Specific Acoustic
Impedance
In the previous chapter, we constructed the sound pressures p(x, t) of both traveling waves and standing waves based on the acoustic wave equation. In this chapter, you will learn how to calculate flow velocity u(x, t), acoustic intensity, and specific acoustic impedance for given sound pressure. These quantities are commonly used in the analysis of acoustics and noise control. This chapter is organized as follows:
First, you will learn how to calculate the flow velocity u(x, t) for a given sound pressure p(x, t) using Euler’s force equation that was derived in Chap. 2. This process can be reversed to calculate the sound pressure p(x, t) for a given flow velocity u(x, t) using Euler’s force equation as shown in the figure below:
Euler′s Force Equation:
Pressure-Velocity Relationship
Pressure: |
Velocity |
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Acoustic Intensity |
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Specific Acoustic Impedance |
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© The Author(s), under exclusive license to Springer Nature Switzerland AG 2021 |
81 |
H. Lin et al., Lecture Notes on Acoustics and Noise Control, https://doi.org/10.1007/978-3-030-88213-6_4
82 |
4 Acoustic Intensity and Specific Acoustic Impedance |
Second, you will learn how to calculate acoustic intensity I from sound pressure p(x, t) and its corresponding flow velocity u(x, t). The acoustic intensity I is simply the average of the sound pressure p(x, t) multiplied by the flow velocity u(x, t) over the period T as shown in the figure above. The formula of acoustic intensity I for both traveling waves and standing waves will be derived.
Third, you will learn how to calculate specific acoustic impedance z as real numbers. The real number specific acoustic impedance z is simply the sound pressure p(x, t) divided by the flow velocity u(x, t) as shown in the figure above. The formulas of specific acoustic impedance z for both traveling waves and standing waves will be derived. Note that the specific acoustic impedance can be formulated in either the real number format or the complex number format. Formulations of the real number specific acoustic impedance z for traveling waves and standing waves are shown in the table below and will be developed in Sect. 4.4.
Fourth, the acoustic impedance z expressed as complex numbers will be introduced in Sect. 4.5. This is an advanced topic but is important for analyzing acoustic waves in pipes. The formulas of complex number acoustic impedance will be discussed and derived. An application of complex number acoustic impedance for filter designs is applied in Chaps. 12 and 13.
4.1Pressure-Velocity Relationship
The relationship between p(x, t) and u(x, t), based on Euler’s force equation, is:
∂∂x pðx, tÞ ¼ ρo ∂∂t uðx, tÞ
4.1 Pressure-Velocity Relationship |
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For a given pressure p(x, t), the flow velocity u(x, t) can be formulated as: |
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Formulas of pressure-velocity relationships for traveling waves u (x, t)and standing waves us(x, t) will be developed based on Euler’s force equation shown above. The following is a summary of formulas of pressure-velocity relationships that will be derived in this section:
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psðx, tÞ ¼ sin ðωtÞ sin ðkxÞ |
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psðx, tÞ ¼ cos ðωtÞ sin ðkxÞ |
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psðx, tÞ ¼ sin ðωtÞ cos ðkxÞ |
(BTW) |
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Note that the flow velocity u (x, t) above was referred to as vf in Chap. 2. The u (x, t) is the macroscopic flow velocity vf and should not be confused with the microscopic colliding velocity vc. Also, (BTW) indicates basic traveling waves, and BSW indicates basic standing waves as discussed in Chap. 3.
4.1.1Pressure-Velocity Relationships for BTW
Even though there are no linear relationships between pressure and velocity for general complex waves, there are linear relationships between pressure and velocity for forward and backward traveling waves. The formulations are shown below.
Forward Traveling Waves
pþðx, tÞ ¼ cos ðωt kx þ ϕÞ
Or:
1
! uþðx, tÞ ¼ þ ρoc pþðx, tÞ
! pþðx, tÞ ¼ ρoc uþðx, tÞ
84 |
4 Acoustic Intensity and Specific Acoustic Impedance |
Sound Pressure |
Molecular Flow Velocity |
Backward Traveling Waves
p ðx, tÞ ¼ cos ðωt þ kx þ ϕÞ
Or:
1
! u ðx, tÞ ¼ ρoc p ðx, tÞ ! p ðx, tÞ ¼ ρoc u ðx, tÞ
The following is an example of how to prove the formulations above. The pressure of a backward traveling wave is:
p ðx, tÞ ¼ cos ðωt þ kx þ ϕÞhor ¼ |
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e jðωtþkxþϕÞ þ e jðωtþkxþϕÞi |
2 |
According to Euler’s force equation, the velocity can be calculated by first taking the derivative of the pressure with respect to x and then taking its integration with respect to time t as:
∂
∂x p ðx, tÞ ¼ k sin ðωt þ kx þ ϕÞ
4.1 Pressure-Velocity Relationship |
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So, for backward traveling waves, the pressure and velocity relationship is:
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u ðx, tÞ ¼ ρoc p ðx, tÞ
Sound Pressure |
Molecular Flow Velocity |
Similarly, the relationship between pressure and velocity for forward traveling waves can be derived as:
1
uþðx, tÞ ¼ ρoc pþðx, tÞ
Therefore, we get the relationship between pressure and velocity as:
! u ðx, tÞ ¼ |
1 |
½BTW& |
ρoc p ðx, tÞ |
86 |
4 Acoustic Intensity and Specific Acoustic Impedance |
4.1.2Pressure-Velocity Relationships for BSW
The pressure-velocity relationships for standing waves are different from the pressure-velocity relationships for the previous traveling waves.
The relationships between pressure and velocity for basic standing waves are:
1
psðx, tÞ ¼ cos ðωtÞ cos ðkxÞ ! uðx, tÞ ¼ ρoc sin ðωtÞ sin ðkxÞ
1
psðx, tÞ ¼ sin ðωtÞ sin ðkxÞ ! uðx, tÞ ¼ ρoc cos ðωtÞ cos ðkxÞ
1
psðx, tÞ ¼ sin ðωtÞ cos ðkxÞ ! uðx, tÞ ¼ ρoc cos ðωtÞ sin ðkxÞ
1
psðx, tÞ ¼ cos ðωtÞ sin ðkxÞ ! uðx, tÞ ¼ ρoc sin ðωtÞ cos ðkxÞ
The following is an example to validate the statement above.
Example 4.1
Given a basic standing wave with two cosine functions:
psðx, tÞ ¼ cos ðωtÞ cos ðkxÞ
Find the corresponding particle velocity using Euler’s force equation.
Example 4.1 Solution
The flow velocity can be calculated using Euler’s force equation:
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4.1 Pressure-Velocity Relationship |
87 |
1k
¼ρo ω sin ðkxÞ sin ðωtÞ
1
¼ ρoc sin ðkxÞ sin ðωtÞ
From the results above, we can conclude that:
1
usðx, tÞ ¼6 ρoc pðx, tÞ
Sound Pressure |
Molecular Flow Velocity |
The following is another example of validating these pressure-velocity relationships.
Example 4.2
Given a basic standing wave with cosine and sine functions: psðx, tÞ ¼ cos ðωtÞ sin ðkxÞ
Find the corresponding particle velocity using Euler’s force equation.
Example 4.2 Solution
The flow velocity can be calculated using Euler’s force equation:
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88 |
4 Acoustic Intensity and Specific Acoustic Impedance |
4.1.3Pressure-Velocity Relationships in Complex Function Form
The general complex solution of sound pressure for acoustic waves is:
p(x, t) ¼ A1B1e |
j(ωt + kx) |
A1B2e |
j(ωt kx) |
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or: |
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pðx, tÞ ¼ Pþe jðωt kxÞ þ Pþe jðωt kxÞ |
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þP 2 e jðωtþkxÞ þ P 2 e jðωtþkxÞ |
The general complex solution of the corresponding velocity can be expressed as:
uðx, tÞ ¼ |
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Pþe jðωt kxÞ þ Pþe jðωt kxÞ P2 e jðωtþkxÞ P 2 e jðωtþkxÞ |
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where each term of the velocity can be calculated from the above pressure equation using Euler’s force equation:
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u ðx, tÞ ¼ ρoc p ðx, tÞ
The following two examples prove the formula above by substituting one term of the complex pressure p into the Euler’s force equation to calculate one term of the complex velocity u .
Example 4.3
Assume that a pressure function is constructed with only the first term of the general solution of sound pressure as shown at the beginning of this section and that the other coefficients (complex numbers) are all zero. In this case:
p 2 ðx, tÞ ¼ e jðωtþkxÞ
Use Euler’s force equation to get the flow velocity u2(x, t) from the given pressure p2(x, t).
Example 4.3 Solution
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