- •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
278 |
11 Power Transmission in Pipelines |
Computer Program Section in Sect. 11.7. This method will plot the power transmission coefficient vs. the frequency of the pipeline.
Section 11.7 shows three MATLAB functions that can be used for the numerical analysis of pipelines described in the previous section (Sect. 11.6). These functions are based on Formulas 1, 4, 5, and 6 derived in this chapter.
Section 11.8 includes a numerical project to calculate and plot the power transmission coefficient vs. the frequency of a pipeline with an arbitrary number of pipes in series. The procedures for this project are similar to the procedures described in the Numerical Method Section (Sect. 11.6). The solutions are not provided.
11.1Complex Amplitude of Pressure and Acoustic Impedance
We will define the complex amplitude of pressure in this section.
11.1.1 Definition of Complex Amplitude of Pressure
Complex amplitudes of sound pressure are used for frequency domain analysis of pipes. For frequency domain analysis of pipes, all time-related parts must be eliminated. Therefore, complex amplitudes must have the following two properties:
•Complex amplitudes of pressure are time-independent.
•Complex amplitudes of pressure are location-dependent.
Based on these two properties, the complex amplitude Pf xo of pressure pf(x, t) of a forward wave can be demonstrated as:
p f ðx, tÞ ¼ |
1 |
Aþe jðωt kxÞ þ cc |
|
|
2 |
||
¼ |
1 |
Aþe jkxo e jkðx xoÞejωt þ cc |
|
|
2 |
||
¼ |
1 |
Pf xo e jkðx xoÞejωt þ cc |
|
|
|
||
2 |
|||
where complex amplitude Pf xo |
of pressure pf(x, t) at x ¼ xo is defined as: |
Pf xo =Aþe jkxo
Note that:
• The time-dependent term e jωt is not included in the complex amplitude of pressure Pf xo .
11.1 Complex Amplitude of Pressure and Acoustic Impedance |
279 |
•The complex amplitude of pressure Pf xo is the amplitude of pressure at location x ¼ xo where e jkðx xoÞ ¼ 1.
We can reverse the procedures above to obtain the pressure pf(x, t) for a given complex amplitude Pf xo at x ¼ xo. It is important to indicate the location of the complex amplitude of pressure when handling any complex amplitudes.
11.1.2 Definition of Acoustic Impedance
Three types of impedances are defined below and will be explained in the following sections:
Three Types of Impedances
Three types of impedances are defined below and will be explained in the following sections:
Specific acoustic impedance:
|
zs |
pressure |
|
|
P |
|
|
|
|
|
|||||||
|
|
|
¼ |
|
|
ð zÞ |
|
||||||||||
velocity |
V |
|
|||||||||||||||
Acoustic impedance: |
|
|
|
|
|
|
|
|
|
|
|
|
|||||
Za |
pressure |
= |
P 1 |
|
P |
ð ZÞ |
|||||||||||
|
|
|
|
|
|
|
|||||||||||
volume flow rate |
V |
S |
U |
||||||||||||||
Mechanical impedance: |
|
|
|
|
|
|
|
|
|
|
|
|
|||||
|
Zm |
force |
|
|
|
|
P S |
|
|||||||||
|
|
V |
|
|
|
||||||||||||
|
velocity |
1 |
|
In the impedances above, P is the complex amplitude of pressure, V is the complex amplitude of velocity, S is the cross-section area of a pipe, and U is defined as the complex amplitude of velocity V multiplied by the cross-section area S.
Complex Acoustic Impedance
Based on the definition of acoustic impedance shown above, acoustic impedance is a complex number because both pressure and velocity are formulated in complex.
Plane waves in a pipe usually result from the addition of incident waves (forward) and reflected waves (backward). The combined acoustic impedance Zcof the combined (forward and backward waves) is a complex number and can be formulated as shown below:
Z |
c |
Uf |
|
Ub |
ð |
f forward wave, b backward wave |
Þ |
|
Pf |
þ Pb |
|
|
|||
|
|
|
þ |
|
|
|
|
280 |
11 Power Transmission in Pipelines |
where Pf, Pb, Uf, and Ub are the complex amplitudes of pressures and volume flow rates.
Therefore, the complex acoustic impedance has the same two properties of the complex amplitude of pressure as shown in Sect. 11.1 as:
•Complex acoustic impedance are time-independent.
–That is, the time-dependent term is not included in the complex acoustic impedance.
•Complex acoustic impedance are location-dependent.
–That is, the complex acoustic impedance is the acoustic impedance at the evaluated location.
Acoustic Impedances of One-Way Plane Waves (Real Numbers)
In general, combined acoustic impedance Zc of forward and backward waves is a complex number.
For one-way plane waves such as forward plane waves and backward plane waves, the acoustic impedances Zf and Zb are always real numbers. The acoustic impedance Zcof the combined (forward and backward waves) is a complex number.
Acoustic impedances for both traveling waves and combined waves can be formulated according to the pressure-velocity relationship as shown in Chapter 4 as:
1
u ¼ ρoc p ðx, tÞ
Formulas 1A–1E
Acoustic impedances for traveling plane waves and combined plane waves can be formulated according to the pressure-velocity relationship above. Formulas 1A to 1C of acoustic impedances of forward plane traveling waves, backward plane traveling waves, and the combined plane waves are listed below:
|
|
|
|
|
|
|
|
|
|
|
Z f |
P f |
|
|
|
|
P f |
|
ρoc |
|
|
|
|
||||||||
|
|
|
|
|
|
|
|
|
|
|
|
|
¼ |
|
|
¼ |
|
|
|
|
|
|
|
|
|||||||
|
|
|
|
|
|
|
|
|
|
|
U f |
SV f |
S |
|
|
|
|
|
|
||||||||||||
|
|
|
|
Zb |
|
|
Pb |
|
|
|
Pb |
|
|
ρoc |
|
|
Z f |
|
|
|
|
|
|
||||||||
|
|
|
Ub |
SVb |
¼ |
¼ |
|
|
|
|
|
|
|||||||||||||||||||
|
|
|
|
|
|
S |
|
|
|
|
|
|
|
|
|
|
|
|
|||||||||||||
Z |
|
Pc |
|
P f þ Pb |
|
|
|
P f þ Pb |
|
|
P f þ Pb |
|
|
Z |
|
P f þ Pb |
|||||||||||||||
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|||||||||||||||||
|
c Uc |
U f |
þ |
Ub |
¼ |
|
P f |
|
Pb |
¼ |
P f |
|
Pb |
¼ |
|
|
f P f |
|
Pb |
||||||||||||
|
|
|
|
|
|
|
|
|
|
||||||||||||||||||||||
|
|
|
|
|
|
|
|
|
|
|
Z f þ Zb |
|
|
Z f |
Z f |
|
|
|
|
|
|
|
where:
ðFormula 1AÞ
ðFormula 1BÞ
ðFormula 1CÞ
Pc P f þ Pb |
ðFormula 1DÞ |
Uc U f þ Ub |
ðFormula 1EÞ |
11.1 Complex Amplitude of Pressure and Acoustic Impedance |
281 |
Proof of Formula 1C
Based on Formulas 1D and 1E, the acoustic impedance Zc2R at the RHS of Pipe 2 (as an example) is defined as:
Z |
c2R |
Pc2R |
¼ |
Pf 2R þ Pb2R |
||
|
Uc2R |
U f 2R |
þ |
Ub2R |
||
|
|
|
|
|
|
Based on Formulas 1A and 1B, the equation above becomes:
Z |
c2R ¼ |
P f 2R þ Pb2R |
¼ |
P f 2R þ Pb2R |
¼ |
P f 2R þ Pb2R |
¼ |
Z |
P f 2R þ Pb2R |
||||||||||
|
U f 2R |
þ |
Ub2R |
|
P f 2R |
Pb2R |
|
|
P f 2R |
2 |
Pb2R |
|
f 2 P f 2R |
|
Pb2R |
||||
|
|
|
|
|
|
Zf 2 |
þ Zb2 |
|
|
|
Zf 2 |
Zf 2 |
|
|
|
|
11.1.3 Transfer Pressure
Formulas 2A–2G
The complex amplitude of the pressure Pf2L of the forward wave pf2(x, t) at x ¼ x1 (LHS of Pipe 2) is related to the complex amplitude of the pressure Pf2R of the forward wave pf2(x, t) at x ¼ x2 (RHS of Pipe 2) in Formula 2A below. The complex amplitude of the pressure Pb2L of the backward wave pb2(x, t) at x ¼ x1 (LHS of Pipe 2) is related to the complex amplitude of the pressure Pb2R of the backward wave pb2(x, t) at x ¼ x2 (RHS of Pipe 2) in Formula 2B:
Pipe 2
,
P f 2L ¼ P f 2RejkL2 |
ðFormula 2AÞ |
Pb2L ¼ Pb2Re jkL2 |
ðFormula 2BÞ |
P f 2R ¼ P f 2Le jkL2 |
ðFormula 2CÞ |
Pb2R ¼ Pb2LejkL2 |
ðFormula 2DÞ |
282 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
11 Power Transmission in Pipelines |
||||||
|
P |
|
|
|
|
|
|
1 |
|
|
|
|
|
|
jkL2 |
1 |
|
P |
|
|
|
|
|
|
|
P f 2L |
|
¼ |
|
|
|
|
|
|
e |
|
Pc2L |
|
ðFormula 2EÞ |
||||||||||
|
ejkL2 |
e |
|
jkL2 |
e |
jkL2 |
||||||||||||||||||
|
|
b2L |
|
|
|
|
|
|
|
|
|
|
|
1 |
|
c2R |
|
|
|
|
||||
|
P f 2R |
|
|
|
|
|
1 |
|
|
|
1 |
|
e jkL2 |
|
Pc2L |
|
|
|
|
|||||
|
P |
|
|
¼ |
|
|
|
|
|
|
ejkL2 |
P |
|
|
ðFormula 2FÞ |
|||||||||
|
b2R |
ejkL2 |
e jkL2 |
|
|
1 |
c2R |
|||||||||||||||||
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|||
|
Uc2L |
|
|
|
|
j |
|
|
|
cosðkL2Þ |
1 |
|
Pc2L |
|
Formula 2G |
|
||||||||
f |
|
|
|
|
|
|
|
|
&f Pc2R g |
ð |
Þ |
|||||||||||||
Uc2R g ¼ |
|
Z f 2sinðkL2Þ ½ |
|
|
1 |
|
cosðkL2Þ |
|
Proof of Formulas 2A and 2C
In Pipe 2 as shown in the figure above, the pressure pf2(x, t) of a forward wave and the pressure pb2(x, t) of a backward wave are formulated in terms of complex amplitudes of the pressures Pf2L and Pb2L at x ¼ x1 (LHS of Pipe 2) as:
pf 2ðx, tÞ ¼ 12 nP f 2Le jkðx x1Þejωt þ cco
pb2ðx, tÞ ¼ 12 nPb2Lejkðx x1Þejωt þ cco
The pressure pf2(x, t) of the forward wave as a function of space and time in terms of the complex amplitude of pressure Pf2L at x ¼ x1 (LHS of Pipe 2) is:
p f 2ðx, tÞ ¼ 12 nP f 2Le jkðx x1Þejωt þ cco
The pressure pf2(x, t) of the forward wave as a function of space and time in terms of the complex amplitude of pressure Pf2R at x ¼ x2 (RHS of Pipe 2) is:
p f 2ðx, tÞ ¼ 12 nP f 2Re jkðx x2Þejωt þ cco
Comparing the two identical equations above yields:
Pf 2Le jkðx x1Þ ¼ P f 2Re jkðx x2Þ
!P f 2L ¼ P f 2Rejkðx2 x1Þ ¼ P f 2RejkL2
!P f 2R ¼ P f 2Le jkðx2 x1Þ ¼ P f 2Le jkL2
Proof of Formulas 2E and 2F
Based on Formula 1D, Pc2L ¼ Pf2L + Pb2L and Pc2R ¼ Pf2R + Pb2R, and using Formula 2C–2D or 2A–2B gets: