- •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
220 |
8 Acoustic Waveguides |
Cutoff Frequency
Because
Therefore
The cutoff |
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wavenumber is the |
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LOWEST wavenumber |
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in both the x and y |
units: |
directions |
Note that any pure tone with a frequency smaller than the cutoff frequency will have only a direct wave (m ¼ 0) since the corresponding wavenumber is too small to form a circle that intercepts any transverse eigenmode kym with m > 0.
As a result, any pure tone with a frequency smaller than the cutoff frequency have only direct wave and no echoes. When there are no echoes for any frequencies, the sound will have no distortion after passing through a waveguide and will be suitable for transmitting signals or sounds.
8.5Traveling Waves in Acoustic Waveguides
The traveling time of a wave from one end of the waveguide to the other end depends on the eigenmode which carries the pure tone. Larger mode numbers have larger propagation angles and will result in longer traveling times. On the other hand, smaller mode numbers have smaller propagation angles and will result in shorter traveling times. When the pure tone is not carried by any mode (m>0), it will travel parallel to the axial direction and result in the shortest possible traveling time.
The traveling time for the wave (direct or reflected) to arrive at the other end of the waveguide can be formulated as:
Traveling Time ¼ DistanceVelocity
8.5 Traveling Waves in Acoustic Waveguides |
221 |
where:
Velocity ¼ c kkz
Example 8.4: (Traveling Time in Waveguides)
An 850 [Hz] pure tone is traveling through a waveguide. Assume the waveguide is 340 [m] long and has a rectangular cross-section of Lx ¼ 13 [m] and Ly ¼ 12 [m].
(a)Calculate the traveling time of the pure tone moving in the axial direction as a direct wave (l ¼ m ¼ 0 mode) to arrive at the other end of the waveguide along the z-axis.
(b)Calculate the traveling times of the pure tone carried by all the eigenmodes to arrive at the other end of the waveguide. Use eigenmodes calculated in Example 8.3.
Example 8.4: Solution
Part (a)
The traveling time for the direct wave to arrive at the other end of the waveguide is:
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Traveling Time |
Distance |
340 ½m& |
1 s |
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¼ Velocity ¼ |
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¼ |
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s |
Part (b)
The eigenmodes calculated in Example 8.3 are:
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ðdirect waveÞ |
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k 00 ¼ 5πbez |
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p |
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k 01 ¼ 2πey þ |
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21πe |
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k |
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3πe |
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!02 ¼ |
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bz |
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k |
3πe |
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2bπe |
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12πe |
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3πex þ |
4πez |
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k 11 ¼ |
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b |
Traveling time of (l, m, n) ¼ (0, 0, ) for the direct wave is:
time |
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1 s |
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kz |
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¼ |
340 |
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¼ |
½ & |
Traveling time of (l, m, n) ¼ (0, 1, ) for the first eigenmode in the y-direction is:
222 8 Acoustic Waveguides
time |
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Traveling time of (l, m, n) |
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y-direction is: |
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time |
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¼ |
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½ & |
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Traveling time of (l, m, n) ¼ (1, 0, ) for the first eigenmode in the x-direction is:
time |
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340 ½m& |
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Traveling time of (l, m, n) ¼ (1, 1, ) is: |
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time |
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This pure tone will travel in this waveguide with five modes. The difference in travel times between different eigenmodes and the direct wave will create echoes of the sound. A sound is usually containing many different frequencies.
When a sound is made of multiple frequencies, since the traveling times are different for different frequencies, even by the same eigenmode, the sound transmitted in the waveguide will be distorted.
Example 8.5: (Cutoff Frequency of Waveguides)
This example shows how to calculate the frequency range of an undisturbed pure tones in a narrow waveguide. Assume that a narrow waveguide has a square crosssection with the dimensions of Lx ¼ Ly¼ 0 .0085 [m].
Example 8.5: Solution
Since the dimensions in the x- and y-direction are the same, the cutoff frequencies (the lowest first transverse first mode) are the same for both directions.
The transverse frequency of the first mode can be calculated as:
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f y1 |
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ky1 |
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340 |
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1 |
¼ |
20000 |
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Hz |
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where the wavenumber ky1 is calculated using:
8.6 Homework Exercises |
223 |
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kym ¼ |
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Ly |
The transverse frequency of the first mode is called the cutoff frequency of the waveguide because it is the maximum frequency that could travel in the waveguide without an echo. Any frequency above the cutoff frequency will disturb the direct sound due to the echo carried by the transverse eigenmode, as shown in Sect. 8.3.
Therefore, the non-echo effect frequency range of this waveguide is 0–20 [kHz]. And the frequency range of sounds that will not disturb the direct sound due to the echo of the sound carried by the transverse eigenmode of the waveguide is 0–20 [kHz].
Remarks: Stethoscopes Are Waveguides with a Very High Cutoff Frequency
Typical stethoscopes have diameters around 0 .0085 [m]. Based on the example above, the cutoff frequency of stethoscopes is around 20 [kHz].
Since the human audible range is 20 [Hz] to 20 [kHz] and there are no echoes with frequencies below 20 [kHz] in this waveguide, any sound waves such as heartbeats can be clearly heard on the other side of a stethoscope. Frequencies above the cutoff frequency of 20 [kHz] will still result in echoes, but these echoes cannot be heard by a human. Stethoscopes are designed with a diameter less than 8.5 [mm] in order to eliminate/disable echo sound with frequencies below the cutoff frequency of 20 [kHz].
8.6Homework Exercises
Exercise 8.1: (2D Traveling Wave Velocity: Forward)
!
Derive the 2D forward flow velocity vector u þðx, y, tÞ of a 2D plane forward traveling wave from the 2D acoustic pressure p+(x, y, t) using Euler’s force equation:
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þð |
pþðx, y, tÞ ¼ Aþ cos |
ωt |
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kxx þ kyy þ θ |
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Þ ¼ |
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ρ0c b |
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nxex þ nyey |
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where: |
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kx2 þ ky2 |
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Euler’s force equation: |
pðx, y, tÞ ¼ ρo |
∂ |
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Exercise 8.2: (Calculations of Wavenumber Vectors and Natural Frequencies) |
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The dimensions of a resonant cavity are Lx ¼ 1 [m], Ly |
¼ 31 |
[m] and Lz ¼ 21 [m]. |
224 |
8 Acoustic Waveguides |
!
(a)Calculate the wavenumber vectors k lmn of the eigenmodes (l, m, n) ¼ (2, 1, 3).
(b)Calculate the natural frequencies flmn of the eigenmodes (l, m, n) ¼ (2, 1, 3).
Use 340 [m/s] for the speed of sound (c) in air. Show units in the Meter-Kilogram- Second (MKS) system.
(Answers): (a) !k 213 |
¼ 2π m1 |
ex þ 3π m1 |
ey þ 6π m1 |
ez; (b) f 213 ¼ |
27 m1 c |
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Exercise 8.3: (3D Mode Shapes in a Rectangular Cavity)
The dimensions of a rectangular resonant cavity are given as (Lx, Ly, Lz) ¼ (3, 9, 24) [m]:
= 9 [ ]
(a)Plot nodal lines and indicate peaks and valleys of eigenmode (l, m, n) ¼ (0, 3, 6).
(b)Plot peak lines and valley lines, and draw four wavenumber vectors (without
values) of eigenmode (l, m, n) ¼ (0, 3, 6).
!
(c)Calculate the wavenumber vector k 036 and natural frequency f036 of eigenmode (l, m, n) ¼ (0, 3, 6).
!
(d)Sketch a wavenumber grid, and draw the wavenumber vector k 036 of eigenmode (l, m, n) ¼ (0, 3, 6) in the wavenumber grid.
Use 340 [m/s] for the speed of sound (c) in air. Show units in the Meter-Kilogram- Second (MKS) system.
Exercise 8.4: (Wavenumber Vectors in a Waveguide)
Awaveguide has a rectangular cross-section of Lx ¼ 0.75 [m] and Ly ¼ 1.5 [m].
(a)Calculate all the possible transverse eigenmodes that can carry a 283.33 [Hz]
!
pure tone in the waveguide. State the wavenumber vectors as k lm ¼
kxlbex þ kymbey þ kz bez.
(b)Calculate the cutoff frequency of the waveguide.
Use 340 [m/s] for the speed of sound (c) in air. Show units in the Meter-Kilogram- Second (MKS) system.
8.6 Homework Exercises |
225 |
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(Answers): (a) |
k 01 |
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πey |
9 |
πez; k 02 |
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k 10 |
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πex |
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Exercise 8.5: (Cutoff Frequency in Ventilation Fans)
A ventilation fan is installed on a long pipeline with a rectangular cross-section, generating a single-frequency noise that can be adjusted by modifying the speed of the fan motor. If the cross-section dimensions of the pipeline are Lx ¼0.75 [m], Ly ¼1.5[m]:
(a)Which transverse mode of the pipeline will carry the acoustic energy if the fan produces a noise signal at 115 [Hz]? State the mode number.
(b)What should the maximum frequency of the fan be so that the noise is not carried to long distances with any one of the transverse modes of the pipeline?
Use 340 [m/s] for the speed of sound (c) in air. Show units in the Meter-Kilogram- Second (MKS) system.
(Answers): (a) (l, m) ¼ (0, 1) mode; (b) 113.3 [Hz]
Exercise 8.6: (Echo Effect in Waveguides)
A 170 Hz pure tone travels in a cross-section waveguide with the dimensions of (Lx, Ly) ¼ (3, 4) [m].
Assuming that the length of the waveguide is 170 [m], calculate the:
(a)Traveling time of a direct wave (l, m) ¼ (0, 0) of the pure tone to arrive at the other end of the waveguide along the x-axis.
(b)Traveling time of the pure tone carried by the first transverse eigenmode in the x-direction (l, m) ¼ (1, 0) to arrive at the other end of the waveguide.
(c)Traveling time of the pure tone carried by the first transverse eigenmode in the y-direction (l, m) ¼ (0, 1) to arrive at the other end of the waveguide.
(d)What is the cutoff frequency of this waveguide?
Use 340 [m/s] for the speed of sound (c) in air. Show units in the Meter-Kilogram- Second (MKS) system.
(Answers): (a) 0.5 [s]; (b) 0.530 [s]; (c) 0.516 [s]; (d) 42.5 [Hz]
Exercise 8.7: (Echo Effect in Waveguide)
An 85 Hz pure tone travels in a cross-section waveguide with the dimensions of (Lx, Ly) ¼ (4, 5) [m].
Assume the length of the waveguide is 240 [m], calculate the:
(a)Traveling time of a direct wave ( m ¼ n ¼ 0 mode) of the pure tone to arrive at the other end of the waveguide along the x-axis.
(b)Traveling time of the pure tone carried by the first transverse eigenmode in the x-direction (l, m) ¼ (1, 0) to arrive at the other end of the waveguide.
226 |
8 Acoustic Waveguides |
(c)Traveling time of the pure tone carried by the first transverse eigenmode in the y-direction (l, m) ¼ (0, 1) to arrive at the other end of the waveguide.
(d)What is the cutoff frequency of this waveguide?
Use 340 [m/s] for the speed of sound (c) in air. Show units in the Meter-Kilogram- Second (MKS) system.
(Answers): (a) 0.706 [s]; (b) 0.815 [s]; (c) 0.770 [s]; (d) 34 [Hz]
Chapter 9
Sound Pressure Levels and Octave Bands
In the field of noise control, noise is quantified by sound pressure level (SPL). SPL can be either unweighted or weighted. In this chapter, you will learn how to calculate both unweighted SPL and weighted SPL. This chapter is divided into four sections and is summarized as follows:
Section 9.1 introduces and defines the decibel scale. The decibel scale is used for sound pressure level (SPL) and other power-like physical quantities in vibrations. In this section, you will learn how to calculate the combined level from separated levels of n incoherent radiating source using the formula below:
Ltot ¼ 10 log 10 |
10 |
L1 ½dB& |
þ 10 |
L2 ½dB& |
þ þ 10 |
Ln10½dB& |
½dB& |
10 |
10 |
Section 9.2 introduces and defines the sound pressure level (SPL). Parseval’s theorem will be used to derive the formula for calculating SPL in the frequency domain. Parseval’s theorem is important because it allows us to formulate RMS pressure in the frequency domain as shown in the flowchart below:
TIME DOMAIN |
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Pressure in Time Domain |
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Pressure in Frequency Domain |
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Unweighted RMS Pressure |
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Parsevals Theorem
Sound Pressure Level (SPL)
© The Author(s), under exclusive license to Springer Nature Switzerland AG 2021 |
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H. Lin et al., Lecture Notes on Acoustics and Noise Control, https://doi.org/10.1007/978-3-030-88213-6_9