
- •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

12.1 Pressure in a One-to-Two Pipe |
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319 |
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1 |
Pi e jðωt kxÞ þ Pi e jðωt kxÞ |
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piðx, tÞ ¼ |
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ðforward plane waveÞ |
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2 |
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viðx, tÞ ¼ 2 |
ρoc Pi e jðωt kxÞ |
þ |
ρoc Pi |
e jðωt kxÞ |
ðforward plane waveÞ |
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1 |
1 |
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1 |
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The reflection pressure is a backward plane wave (Pr) and is shown below for reference:
prðx, tÞ ¼ |
1 |
Pr e jðωtþkxÞ þ Pr e jðωtþkxÞ |
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ðbackward plane waveÞ |
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2 |
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The velocity function is calculated by Euler’s force equation: |
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vrðx, tÞ ¼ 2 |
ρoc |
Pr e jðωtþkxÞ þ ρoc Pr |
e jðωtþkxÞ |
ðbackward plane waveÞ |
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1 |
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1 |
1 |
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•Note that pressure and velocity are functions of space and time. Also, the real
pressure, pi(x, t), is the addition of a complex conjugate pair of the pressures
12 piðx, tÞ þ pi ðx, tÞ&.
Remarks
•The incident acoustic impedance and reflected backward acoustic impedance have a simple relationship:
Zr = 2Zi
•Because transmission pressures P1 and P2 are outward only (no return), acoustic impedance Z1(=ρoc/S1) and Z2(=ρoc/S2) are real numbers.
•Because the incident and reflected pressures Pi and Pr are individual plane waves
(forward |
and |
backward), |
acoustic |
impedance |
Zi(=ρoc/Si) |
and |
Zr = 2 |
ρoc |
= 2Zi |
are real numbers. |
Si |
12.1.1 Equivalent Acoustic Impedance of a One-to-Two Pipe
The formulas for a one-to-two pipe can be compared to the formulas for a one-to-one pipe as listed below:

320 |
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12 Filters and Resonators |
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Pipe 1 |
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Pipe 0 |
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near end |
far end |
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=
P f 1R ¼ |
1 |
1 |
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Z f 1 |
PfoL |
ðFormula 8AÞ |
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þ |
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2 |
ZfoL |
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1 |
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Z f 1 |
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Pb1R ¼ |
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1 |
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PfoL |
ðFormula 8BÞ |
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2 |
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ZfoL |
Formulas 8A–8B (Equivalent Acoustic Impedance of a One-to-Two Pipe)
The dimensions and acoustic impedance of a one-to-two pipe are given as follows:
• Cross-section areas of the pipes are Si, S1, and S2.
• Acoustic impedances of the pipe are Zi, Zr,Z1, and Z2:
1 = 1 + 1
=
=
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¼ |
2Zo |
ð |
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Þ |
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Pi |
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Zo þ Zi |
P2 |
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Formula 8A |
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12.1 Pressure in a One-to-Two Pipe |
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321 |
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¼ |
2Zo |
ð |
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Þ |
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Pr |
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Zo Zi |
P2 |
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Formula 8B |
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where Zo is the equivalent acoustic impedance. This Zo is the combined impedance of Z1 and Z2 and is formulated as:
1 |
¼ |
1 |
þ |
1 |
ðFormula 12Þ |
Zo |
Z1 |
Z2 |
Proof 12: Solution
The pressure and velocity functions in the previous section are general solutions for plane wave equations. The exact reflection and transmission pressures can be solved by the boundary conditions at the intersection.
The boundary of the intersection of three pipes can be considered as a point, and the following conditions must be satisfied:
(a) All pressures are equal in amplitude at the intersection (related to Newton’s third law):
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Pi þ Pr ¼ P1 ¼ P2 |
ð1Þ |
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(b) The total flow rate inward is equal to the total flow rate outward |
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(based on the conservation of mass): |
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Sð Vi þ VrÞ ¼ S1V1 þ S2V2 |
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! Ui þ Ur ¼ U1 þ U2 |
ð2Þ |
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where the relationship between V and U is: |
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1 |
Ve jðωt kxÞ þ V e jðωt kxÞ |
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vðx, tÞ ¼ |
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2 |
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1 |
S Ve jðωt kxÞ þ V e jðωt kxÞ |
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uðx, tÞ Svðx, tÞ ¼ |
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2 |
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¼ |
1 |
Ue jðωt kxÞ þ U e jðωt kxÞ |
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2 |
The acoustic impedance (Z) gives the relationship between pressure and velocity
as shown below: |
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Z = |
P |
= |
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P |
= |
1 |
z |
z = P |
U |
SV |
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S |
V |
Use the above acoustic impedance to replace U with P/Z in Eq. (2) to obtain:

322 |
12 Filters and Resonators |
Pi 2 Pr = P1 þ P2
Zi Zi Z1 Z2
Now, Pr, P1, and P2 can be solved from Eq. (1) and Eq. (3) as follows: |
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Pi þ Pr ¼ P1 ¼ P2 |
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ð10Þ |
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Pi Pr = |
Zi |
Zi |
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P1 þ |
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P2 |
ð3Þ |
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Z1 |
Z2 |
Since P1 ¼ P2, P1 can be replaced with P2 in Eq. (3) to reduce one unknown variable ( P2):
Pi Pr ¼ Z1 P1 þ |
Z2 P2 |
¼ |
Z1 þ |
Z2 |
1 P2 |
ð4Þ |
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Zi |
Zi |
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1 |
1 |
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Zi |
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Define the equivalent acoustic impedance Zo as the combined impedance of Z1 and Z2 and computed as:
1 |
¼ |
1 |
þ |
1 |
ðFormula 12Þ |
Zo |
Z1 |
Z2 |
Based on the equivalent acoustic impedance Zo defined above, Eq. (4) becomes:
Pi Pr ¼ |
Zi |
P2 |
ð5Þ |
Zo |
Combining Eq. (1) and Eq. (5) yields Formula 8:
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¼ |
2Zo |
ð |
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Þ |
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Pi |
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Zo þ Zi |
P2 |
Formula 8A |
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¼ |
2Zo |
ð |
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Þ |
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Pr |
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Zo Zi |
P2 |
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Formula 8B |
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Note that by defining the equivalent acoustic impedance Zo as Formula 12, Formula 8 can be used to calculate pressures Pr and P2 for the one-to-two pipe. The definition of this new acoustic impedance Zo may be used in many outward pipes in a later section.