- •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
4.2 RMS Pressure |
89 |
Example 4.4
Use Euler’s force equation to get the flow velocity u+(x, t) from the given pressure as shown below:
|
|
|
|
|
|
|
|
pþðx, tÞ ¼ e jðωt kxÞ |
|
|
|
|
|||||
Example 4.4 Solution |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|||
|
∂ |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
||
|
|
pþðx, tÞ ¼ jk e jðωt kxÞ |
|
|
|
|
|
|
|
|
|||||||
∂x |
|
|
|
|
|
|
|
|
|||||||||
|
uþðx, tÞ ¼ |
1 |
Z |
|
∂ |
1 |
Z |
jk e |
jðωt kxÞ |
dt |
|||||||
|
ρo |
∂x p 2 |
ðx, tÞ dt ¼ ρo |
||||||||||||||
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
h |
i |
|
|
|
¼ |
k |
|
e jðωt kxÞ ¼ |
1 |
e jðωt kxÞ ¼ |
|
1 |
pþðx, tÞ |
|
|
|||||
|
|
|
|
|
|
|
|||||||||||
|
|
ρoω |
ρoc |
ρoc |
|
|
Based on the two examples above, we can conclude that:
1
u ðx, tÞ ¼ ρoc p ðx, tÞ
Remark:
Note that for general complex waves, there are no linear relationships between pressure and velocity:
uðx, tÞ 6¼ |
1 |
pðx, tÞ 6¼ |
1 |
pðx, tÞ |
ρoc |
ρoc |
4.2RMS Pressure
The root-mean-square (RMS) pressure is defined as:
Z T
p2RMS T1 0 p2dt
where T is the period of the pressure wave.
Formulas of RMS pressure for traveling waves p (x, t) and standing waves ps(x, t) will be developed based on the definition of RMS pressure shown above. The following is a summary of formulas of RMS pressure that will be derived in this section:
90 4 Acoustic Intensity and Specific Acoustic Impedance
2 |
|
|
A2 |
|
|
|
|
[BTW] |
|
p RMS |
2 |
|
|
|
|
[BSW] |
|||
psRMS2 |
¼ |
A2 |
|
cos 2ðkxÞ if |
psðx, tÞ ¼ A cos ðωtÞ cos ðkxÞ |
||||
2 |
|||||||||
2 |
¼ |
A2 |
|
sin |
2 |
ðkxÞ if |
psðx, tÞ ¼ A sin ðωtÞ sin ðkxÞ |
[BSW] |
|
psRMS |
2 |
|
|
[BSW] |
|||||
2 |
¼ |
A2 |
|
sin |
2 |
ðkxÞ if |
psðx, tÞ ¼ A cos ðωtÞ sin ðkxÞ |
||
psRMS |
2 |
|
|
[BSW] |
|||||
psRMS2 |
¼ |
A2 |
|
cos 2ðkxÞ if |
psðx, tÞ ¼ A sin ðωtÞ cos ðkxÞ |
||||
2 |
4.2.1RMS Pressure of BTW
The RMS pressure of traveling waves is defined as follows:
pþ2 |
RMS |
A2 |
2 |
||
p2 |
RMS |
A2 |
2 |
where A is the amplitude of the traveling waves of the four basic traveling waves:
p ðx, tÞ ¼ A ∙ cos ðωt þ kxÞ pþðx, tÞ ¼ A ∙ cos ðωt kxÞ p ðx, tÞ ¼ A ∙ sin ðωt þ kxÞ pþðx, tÞ ¼ A ∙ sin ðωt kxÞ
The following is an example of validating these relationships:
For forward traveling wave p+(x, t) ¼ cos (ωt kx), the RMS pressure is by definition:
pRMS2 T Z0 |
T |
p2dt ¼ T Z0 |
T |
||
|
ðA ∙ cos ðωt kxÞÞ2dt |
||||
1 |
|
|
1 |
|
|
For general traveling waves, RMS pressure is independent of the choice of location. Therefore, we can calculate the square of RMS pressure at x ¼ 0. Therefore:
pRMS2 ¼ A2 |
T Z0 |
T |
|
cos 2ðωtÞdt |
|||
|
1 |
|
|
Because ω ¼ 2Tπ, replace ω with 2Tπ to get:
4.2 RMS Pressure |
|
|
|
|
|
|
91 |
pRMS2 |
¼ A2 |
1 |
Z |
T |
cos 2 |
2π |
|
|
t dt |
||||||
|
|
|
|||||
T |
|
T |
|||||
|
|
|
0 |
|
|
|
|
This means that the square of RMS pressure is an integral over a period 2π. Note that the geometry relationship is used to yield:
pRMS2 |
¼ A2 |
1 |
Z |
T |
cos 2 |
2π |
t |
dt ¼ A2 |
1 |
¼ |
A2 |
|
T |
0 |
|
T |
2 |
2 |
|||||||
|
|
|
|
|
|
|
|
|
|
|
4.2.2 RMS Pressure of BSW
The square of the RMS pressure of standing waves can be illustrated as:
psðx, tÞ ¼ A cos ðωtÞ cos ðkxÞ ! psRMS2 |
¼ |
|
A2 |
cos 2ðkxÞ |
|
2 |
|||
psðx, tÞ ¼ A sin ðωtÞ sin ðkxÞ ! psRMS2 |
¼ |
A2 |
sin 2ðkxÞ |
|
2 |
||||
psðx, tÞ ¼ A cos ðωtÞ sin ðkxÞ ! psRMS2 |
¼ |
|
A2 |
sin 2ðkxÞ |
|
2 |
|||
psðx, tÞ ¼ A sin ðωtÞ cos ðkxÞ ! psRMS2 |
¼ |
A2 |
cos 2ðkxÞ |
|
2 |
The following is an example to validate one of the above relationships between pressure and RMS pressure:
The square of the RMS pressure is defined as:
PRMS2 ¼ T |
Z0 |
T |
p2 dt ¼ T Z0 |
T |
|
|
ðA cos ðωtÞ cos ðkxÞÞ2 dt |
||||
1 |
|
1 |
|
|
Bringing the time-independent function cos(kx) outside of the integral yields:
|
|
1 |
Z0 |
T |
A2 |
|||
PRMS2 |
¼ A2 cos 2 |
ðkxÞ |
|
cos 2ðωtÞdt ¼ |
|
cos 2ðkxÞ |
||
T |
2 |
|||||||
|
PRMS ¼ |
|
A |
|
|
|||
|
p2 cos ðkxÞ |
|
|
92 |
4 Acoustic Intensity and Specific Acoustic Impedance |
Example 4.5 (Traveling Wave with Known Velocity)
Use the following harmonic motion as velocity u(t) to answer every question of this problem:
uðtÞ ¼ Vo cos ωt þ |
π |
2 ; Vo is a real number: |
A large, rigid wall is vibrating with a velocity u(t) perpendicular to its planar surface. The motion of the wall creates plane waves that propagate into the air. Considering that the flow velocity of the plane wave on the surface of the wall (x ¼ 0) would be equal to the velocity of the wall:
= 0
a)Obtain the expressions for the flow velocity at any point in space (not just on the wall surface) of the plane wave radiating from the wall in terms of the wall vibration velocity.
b)Obtain the expressions for the sound pressure at any point in space (not just on the wall surface) of the plane wave radiating from the wall in terms of the wall vibration velocity.
c)What is the root-mean-square (RMS) pressure at any point in space if the wall velocity Vo ¼ 0.01 m/s.
Example 4.5 Solution
a) The general solution of the forward plane wave with an amplitude of A:
uðx, tÞ ¼ A cos ðωt kx þ θÞ
Find the unknown amplitude A and phase delay θ |
by the given boundary |
||
conditions at x ¼ 0: |
|
|
|
uðx ¼ 0, tÞ ¼ Vo cos ωt þ |
π |
|
|
2 |
|
Substituting the boundary condition into general solution yields:
4.2 RMS Pressure |
|
|
|
93 |
Vo cos ωt þ |
π |
¼ A cos ðωt þ θ Þ |
|
|
2 |
|
|||
Hence: |
|
|
|
|
|
|
θ ¼ |
π |
ðandÞ |
|
|
2 |
A ¼ Vo,
Therefore, the general expression of the particle velocity at any point to the right of the wall is:
uðx, tÞ ¼ Vo cos ωt kx þ |
π |
2 |
b)The acoustic pressure can be calculated from the flow velocity using Euler’s force equation.
For a forward traveling wave, the acoustic pressure is related to the flow velocity as follows:
pþðx, tÞ ¼ ρoc uðx, tÞ |
|
|
|
|
π |
|||
¼ ρocVo cos ωt kx þ |
||||||||
2 |
||||||||
c) Substituting the following known variables: |
|
|
|
|
|
|||
Vo ¼ 0:01 |
m |
|
|
|
|
|
||
|
|
|
|
|
|
|
||
s |
|
|
|
|
|
|||
|
|
|
|
s |
|
|
||
ρoc ¼ 415 ½rayles& or hPa |
|
i |
|
|
||||
m |
|
|
||||||
into pressure function p(x, t) above yields: |
|
|
|
|
|
|||
pþðx, tÞ ¼ 4:15 cos ωt kx þ |
π |
½Pa& |
|
|||||
2 |
|
For traveling waves, forward or backward, the RMS pressure is independent of space.
Hence:
|
PRMS2 |
¼ |
1 |
ð4:15Þ2 |
Pa2 |
|||
|
|
2 |
||||||
|
|
|
r |
|
|
|
||
! |
PRMS |
¼ |
|
|
ð4:15Þ2 |
½ |
Pa |
& |
|
|
|
2 |
|