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Aeroacoustics Simulation Setup Guide
Mar 6, 2025
Aeroacoustics Noise Simulation Setup using Ansys Fluent
Introduction
This is the second part of the tutorial on calculating aeroacoustics noise using Ansys Fluent.
Focuses on setting up the simulation.
Model Setup
Initial Steps
Click on
Setup
and hit
Start
.
Green surface: inlet, black surfaces with arrows: outlets, red walls: no arrows.
Material Properties
Airflow is compressible.
Air density: Change from constant to ideal gas.
Enable
Energy
as density depends on temperature in the ideal gas model.
Boundary Conditions
Inlet
Specify velocity: 20 m/s (no mass flow or inlet velocity values).
Outlet
Default setting: 0 gauge pressure (appropriate, no changes required).
Solver Settings
Methods Section
Two schemes:
Coupled
and
PISO
(use Coupled).
Disable Pseudo time method due to low air speed.
Controls
Courant number: Adjust to increase convergence speed (demonstration purpose: initially unchanged).
Initialization
Use
Standard Initialization
for internal flows.
Select inlet and click
Initialize
.
Running Calculation
Specify 50 iterations and click
Calculate
.
Adjust Courant number to 5 due to non-convergence.
Run calculation again.
Preparing Aeroacoustics Solution
Viscous Model
Change to
LES
or
DES
(select LES for example).
Requires highly refined mesh (recommend mesh dependency investigation).
LES and DES are Transient models.
Methods Section for Aeroacoustics
Choose between
PISO
or
Coupled
(PISO recommended for lower computational cost).
Change from first order to
bounded second order
.
Run Aeroacoustics Calculation
Specify time step size.
Check solution convergence with 10 time steps.
Run and converge in one iteration using stationary solution.
Enabling Acoustics
Ffowcs-Williams-Hawkings Model
Enable acoustics and select model.
Export acoustic source data.
Identify permeable surface in internal boundaries.
Adding Microphones
Specify 4 microphones relative to air muffler (origin).
Ensure fine mesh and verify mesh independence.
Solving and Extracting Acoustic Signals
Solve for 200 time steps (0.01 seconds, frequency resolution 100 Hz).
Extract acoustic signals.
Use
FFT
to view sound pressure level versus frequency.
Select microphone (e.g., Receiver 2).
Plot sound pressure level.
Increase steps to improve frequency resolution (e.g., additional 300 steps for 40 Hz resolution).
Conclusion
Continue simulation for better frequency resolution (aim for 10 Hz).
Tutorial ends, covered aeroacoustics with Ffowcs-Williams-Hawking method.
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