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Circular Duct analysis in ANSYS
workbench
Objective
1. Calculate the natural frequencies of a 3D duct with rigid walls with various end conditions.
2. Sound pressure distribution along the duct for a harmonic volume velocity excitation at one end of a duct
with finite length.
3. Pressure distribution along an infinitely long duct.
4. Pressure distribution along a duct with a finite length that has a frequency varying impedance at one end of
the duct radiating into free space.
๐‘ข1
๐‘ข2
z
x
y
L
a
Element types available for Acoustic Analyses in
ANSYS based on pressure formulation
Name 2D/3D Nodes Description
FLUID29 2D 4 Planar element
FLUID129 2D 2 Line element for simulating
an infinite boundary
FLUID30 3D 8 Brick element
FLUID130 3D 4,8 Planer element for
simulating an infinite
boundary
FLUID220 3D 20 Brick element
FLUID221 3D 10 Tetrahedral element
Natural frequencies
Description parameter Value
Diameter 2a 0.1m
Length L 3m
Speed of sound ๐‘0 343m/s
Density ฯ0 1.21 kg/m3
Velocity of piston ๐‘ข2 0.0
Velocity at rigid end ๐‘ข1 0.0
configuration schematic Mode index n= Natural frequencies Mode shape
Rigid-rigid 0,1,2 n๐‘0/2L Cos(nฯ€x/L)
Open-rigid 1,3,5 n๐‘0/4L Cos(nฯ€x/2L)
Open-open 1,2,3 n๐‘0/2L sin(nฯ€x/L)
โ€ข FLUID 30 acoustic element is used
Element per wavelength
Element size
Esize=ฮป/epw =๐‘0/f/epw
Rigid-rigid boundary condition
Natural frequency of open-rigid
Natural frequency of open-open Duct
Pressure and velocity distribution along the duct
Description parameter Value
Diameter 2a 0.1m
Length L 3m
Speed of sound ๐‘0 343m/s
Density ฯ0 1.21 kg/m3
Velocity of piston ๐‘ข2 1.0 m/s
Velocity at rigid end ๐‘ข1 0.0
Excitation frequency f 200Hz
Parameters used in the analysis of a circular duct with forced excitation at one end
-1
-0.8
-0.6
-0.4
-0.2
0
0.2
0.4
0.6
0.8
1
Particle velocity along a Piston-Rigid Duct
1 2 3
100
110
120
130
140
150
-500
-400
-300
-200
-100
0
100
200
300
400
500
Mic Position along Duct [m]
Mic Position along Duct [m]
Mic Position along Duct [m]
Soundpressurelevel[dB]ParticleVelocity[m/s]
ImaginaryPressure[Pa]
Circular duct analysis in ansys workbench
Semi-infinite duct
โ€ข Applied an absorbing boundary to the outlet of the duct to simulate a
semi-infinite duct
โ€ข The upstream inlet end provides an acoustic excitation as a surface
velocity of 1 m/s.
โ€ข Outlet end has a radiation boundary applied which is one method of
specifying an absorbing boundary.
SPL of semi-infinite duct= 20log10
ฯ0โˆ—๐‘0โˆ—๐‘ข
20๐‘’โˆ’6โˆ— 2
=143.3 dB
Radiation from an Open-ended Duct
Piston
velocity
Free-field
FLUID 130 element
Transition region for the acoustic
finite elements
Applied force
magnitude of
1e-3
Circular duct analysis in ansys workbench
Commands which will couple all the nodes associated with inlet axis
which will create a rigid piston face and motion in the other direction
will be zero
Circular duct analysis in ansys workbench
Circular duct analysis in ansys workbench
Circular duct analysis in ansys workbench
Imaginary part of mechanical impedance of piston attached to a Duct
Frequency [Hz]
Imaginaryimpedance[Ns/m]
Mechanical power of piston Attached to the Duct
Frequency [Hz]
Power[Watts]
Real part of mechanical impedance of piston attached to a Duct
Frequency [Hz]
Realimpedance[Ns/m]
Circular duct analysis in ansys workbench

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Circular duct analysis in ansys workbench

  • 1. Circular Duct analysis in ANSYS workbench
  • 2. Objective 1. Calculate the natural frequencies of a 3D duct with rigid walls with various end conditions. 2. Sound pressure distribution along the duct for a harmonic volume velocity excitation at one end of a duct with finite length. 3. Pressure distribution along an infinitely long duct. 4. Pressure distribution along a duct with a finite length that has a frequency varying impedance at one end of the duct radiating into free space. ๐‘ข1 ๐‘ข2 z x y L a
  • 3. Element types available for Acoustic Analyses in ANSYS based on pressure formulation Name 2D/3D Nodes Description FLUID29 2D 4 Planar element FLUID129 2D 2 Line element for simulating an infinite boundary FLUID30 3D 8 Brick element FLUID130 3D 4,8 Planer element for simulating an infinite boundary FLUID220 3D 20 Brick element FLUID221 3D 10 Tetrahedral element
  • 4. Natural frequencies Description parameter Value Diameter 2a 0.1m Length L 3m Speed of sound ๐‘0 343m/s Density ฯ0 1.21 kg/m3 Velocity of piston ๐‘ข2 0.0 Velocity at rigid end ๐‘ข1 0.0 configuration schematic Mode index n= Natural frequencies Mode shape Rigid-rigid 0,1,2 n๐‘0/2L Cos(nฯ€x/L) Open-rigid 1,3,5 n๐‘0/4L Cos(nฯ€x/2L) Open-open 1,2,3 n๐‘0/2L sin(nฯ€x/L)
  • 5. โ€ข FLUID 30 acoustic element is used
  • 6. Element per wavelength Element size Esize=ฮป/epw =๐‘0/f/epw
  • 8. Natural frequency of open-rigid
  • 9. Natural frequency of open-open Duct
  • 10. Pressure and velocity distribution along the duct Description parameter Value Diameter 2a 0.1m Length L 3m Speed of sound ๐‘0 343m/s Density ฯ0 1.21 kg/m3 Velocity of piston ๐‘ข2 1.0 m/s Velocity at rigid end ๐‘ข1 0.0 Excitation frequency f 200Hz Parameters used in the analysis of a circular duct with forced excitation at one end
  • 11. -1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.8 1 Particle velocity along a Piston-Rigid Duct 1 2 3 100 110 120 130 140 150 -500 -400 -300 -200 -100 0 100 200 300 400 500 Mic Position along Duct [m] Mic Position along Duct [m] Mic Position along Duct [m] Soundpressurelevel[dB]ParticleVelocity[m/s] ImaginaryPressure[Pa]
  • 13. Semi-infinite duct โ€ข Applied an absorbing boundary to the outlet of the duct to simulate a semi-infinite duct โ€ข The upstream inlet end provides an acoustic excitation as a surface velocity of 1 m/s. โ€ข Outlet end has a radiation boundary applied which is one method of specifying an absorbing boundary.
  • 14. SPL of semi-infinite duct= 20log10 ฯ0โˆ—๐‘0โˆ—๐‘ข 20๐‘’โˆ’6โˆ— 2 =143.3 dB
  • 15. Radiation from an Open-ended Duct Piston velocity Free-field FLUID 130 element Transition region for the acoustic finite elements
  • 18. Commands which will couple all the nodes associated with inlet axis which will create a rigid piston face and motion in the other direction will be zero
  • 22. Imaginary part of mechanical impedance of piston attached to a Duct Frequency [Hz] Imaginaryimpedance[Ns/m]
  • 23. Mechanical power of piston Attached to the Duct Frequency [Hz] Power[Watts]
  • 24. Real part of mechanical impedance of piston attached to a Duct Frequency [Hz] Realimpedance[Ns/m]