- •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
12.5 Band-Stop Resonator |
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12.5Band-Stop Resonator
A general band-stop resonator can be constructed by a main pipe with a side branch of pipeline series. The resonant of the side branch will absorb the resonant from the main pipe at the resonant frequency of the side branch. The simple band-stop resonator and a Helmholtz resonator are shown in the figure below:
Main Pipe
Side Branch
A Simple Band-Stop Resonator |
Helmholtz Resonator |
Objective
The Helmholtz resonator has a volume V connected to the remainder of the medium with a small neck of length L and an open area S, as shown in the figure below:
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12 Filters and Resonators |
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Schematic of a Helmholtz resonator
This passive acoustic system can be analyzed for a range of frequencies where |
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Show that |
the power transmission T |
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fi |
cients of the Helmholtz resonator can |
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Tw ¼ Re |
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where: |
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Step 1: Derivation of the Dynamic Equation of the Resonator
The volume of fluid in the neck area will act as a mass just as the open end of a flanged pipe for λ a, where a is the radius of opening. The effective length of the neck is assumed to be 0.85a longer than the actual length of the pipe if the pipe is terminated with a wide flange at the opening. If the pipe has an un-flanged termination, it can be assumed that the effective length is longer only by 0.6a. Since the
12.5 Band-Stop Resonator |
345 |
interior end of the neck acts like a flanged termination, the effective length of the neck with flanged and un-flanged termination to the outside medium becomes:
L0 = L |
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Using the effective length, the mass of fluid moving in the neck is:
M ¼ ρoSL0
The mass in the neck works against the stiffness of the fluid in volume V in addition to resistance from the frictional forces in the neck and the radiation impedance from the open end.
The stiffness of the fluid in volume V is calculated from the change of volume inside the container due to the motion of the mass in the neck. Hence, if ξ is the displacement of the neck mass, the change in volume V is then given by:
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ρoVo ¼ ρV ¼ MV, since the mass MV of the volume V is preserved. Thus: |
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MV |
MV |
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∙ ρo ρ |
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ρ ρo |
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ρ |
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ρo |
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ρo |
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ρo |
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ρo |
¼ |
Dividing both sides of this equation by the volume V and using the relationship above yield:
Sξ |
¼ |
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¼ |
ρ |
¼ sac |
V |
V |
ρo |
where sac is the acoustic condensation. Now, using the relationship between acoustic |
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pressure and condensation ( |
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¼ |
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and c |
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ρo |
γP0 |
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sac ¼ |
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ρoc2 |
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The acoustic pressure inside the given volume can thus be expressed as:
p ¼ ρoc2sac ¼ ρoc2 Sξ
V
346 |
12 Filters and Resonators |
The force necessary to displace the fluid in the neck is simply Sp ¼ Kξ where K is the effective stiffness of the fluid inside V. Multiplying both sides of the pressure equation above by S yields:
Sp ¼ ρoc2 S2 ξ ¼ Kξ
V
and the effective stiffness is:
K ¼ ρoc2 S2
V
In addition to the inertial and stiffness forces acting on the fluid column in the neck, there are also resistive forces that are proportional to the fluid velocity. These forces are due to the radiation resistance Rr and the viscous resistance Rω. These two constants provide damping to the mechanical system since the force they create is proportional to the velocity of the fluid in the neck. Hence, the total mechanical resistance coefficient is given by:
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Rm ¼ Rr þ Rω |
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where: |
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Rr ¼ |
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ρocSðkaÞ |
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ðflanged openingÞ |
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Rr ¼ |
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ρocSðkaÞ |
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ðun flanged openingÞ |
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4 |
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and:
Rω ¼ 2Mcαω
where αω is the absorption coefficient for wall losses.
The mass-spring system described here is forced by the pressure wave of p impinging on its opening. This force is simply the pressure of the wave multiplied by the neck cross-section area. That is:
f ¼ Sp
Now the differential equation of the resonator can be written in terms of mass M, stiffness K, and the damping coefficient Rm given by the equations above as follows:
12.5 Band-Stop Resonator |
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347 |
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M |
d2ξ |
þ Rm |
dξ |
þ Kξ ¼ Sp |
d2t |
dt |
Step 2: Mechanical Impedance of the Dynamic Equation
Let ξ ¼ Ae jωt, where its complex conjugate is ξ ¼ A e jωt, and we can then solve the following two equations step-by-step as follows for p ¼ Pe jωt and p ¼ P e jωt. Note that K, M, Rm, S, and ω are all real constants:
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d2ξ |
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M |
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þ Rm |
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þ Kξ ¼ Sp ¼ SPejωt; |
p ¼ Pejωt |
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M |
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þ Rm |
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þ Kξ ¼ Sp ¼ SP e jωt; |
p ¼ P e jωt |
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dt |
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Let ξ ¼ Ae |
jωt to get (K |
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ω2M + jωR |
)Ae jωt |
SPe jωt. |
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jωt |
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m |
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¼ jωt |
¼ SP e |
jωt |
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Let ξ ¼ A e |
to get (K ω |
M jωRm)A e |
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Let:
H ¼ K ω2M þ jωRm 1
H ¼ K ω2M jωRm 1
to obtain:
A ¼ K ω2M þ jωRm 1SP ¼ HSP
A ¼ K ω2M jωRm 1SP ¼ H SP
Therefore:
ξ ¼ HSPejωt
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ξ ¼ H SP e jωt |
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dξ |
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u ¼ |
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dξ |
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u ¼ |
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PS |
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K |
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ω2M |
jωR |
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Zm ¼ |
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jωþ |
m |
¼ Rm þ j ωM |
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u |
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jωH |
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P S |
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1 |
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ω2M jωRm |
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j ωM |
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jωH |
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m |
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jω |
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348 |
12 Filters and Resonators |
Note that the equations above show that all complex values, functions, or equations always have a complex conjugate part associated with them. Therefore, we can always hide the conjugate part, but when we need a real-world solution, we must show them.
Step 3: Transmission Coefficient Induced by a Side Resonator
Neglecting Rω for wall losses, the input mechanical impedance of the resonator is:
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Zm ¼ Rr þ j ωM |
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ω |
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ρocSðkaÞ |
2 |
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ρoc2S2 |
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ckV |
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¼ 2 ρocS ðkaÞ2 |
þ j |
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kV |
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1 |
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2 k2L0V |
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Z1 ¼ |
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Z2 ¼ |
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S2 |
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S2 |
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P |
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2 Z |
1 |
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j 2ðk2L0V SÞ |
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kV |
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2Z1 þ Z2 |
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ka |
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2ðk2L0V SÞ |
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Þ þ |
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ð |
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kV |
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For ka 1, (Zi,Z2,Pi real) (Z1,P2 complex):
P2 = |
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j 2S2ðkkSV0 |
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2S2 |
ð kSV |
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2 |
þ j |
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2L V |
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k2L0V S |
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k2L0V S |
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Pi |
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2S2 |
k2L0V |
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Þ þ 1 |
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1 þ 2S2 |
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ðkkSV0 |
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L V |
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Re |
P2 |
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2S2 |
ðkkSV0 |
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2 |
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2L V |
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Pi |
1 þ |
2S2 |
k2L0V |
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kSV |
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ð kSV |
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2S2ðk2L0V SÞ |
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Zi |
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Tw ¼ Re |
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kSV |
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2S2ðk2L0V SÞ |
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12.5 Band-Stop Resonator |
349 |
= |
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1 |
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½ Zi, Z2, Pi real& |
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k2ð |
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kc |
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where: |
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2 r0 |
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¼ |
ωc2 |
¼ |
0 |
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¼ |
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k2 |
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c |
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2 S |
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SL |
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The side Helmholtz resonator behaves like a band-stop filter or notch filter. The
q maximum attenuation of the filter occurs at the resonance frequency ωc ¼ c LS0V of
the Helmholtz resonator. The bandwidth depends on the volume ratio SLV 0 and the area
ratio of the pipes, S :
S2
Tw
1 |
Power Transmission Coefficient of Band-stop Filter |
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0.9 |
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D=0 .1 |
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0.8 |
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D=1 |
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0.6 |
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D=10 |
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0.5 |
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0.4 |
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0.3 |
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0.2 |
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0.1 |
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0 |
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10-2 |
10-1 |
100 |
101 |
102 |
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/ |
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c |
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Power transmission coefficient as a function of the frequency ratio