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Modelling and Simulation in Aeroacoustics Current Practice and Future Challenges
Fred Mendonça
HVAC, ECS, Duct ventilation and discharge
AIAA2012-2068
External Aeroacoustic Excitation and
Internal Noise Transmission
Surface FFT (dB) at 500Hz (top)
and 1000Hz (bottom)
AIAA2012-2205
AIAA2012-2206
SAE2013-01-0640
Airframe and Jet noise
Turbo compressor Noise
GT2012-70028
HVAC – blower, distributor, ducts
SAE13-01-0856
Pipe singing
AIAA2012-2171
Sunroof/side-window buffeting – real vehicle effects
Uncorrected
Correlated
Aluminium
Perspex MDF
– Wall compliance effects
• Full FSI of compliant walls (below left)
• Correlations for wall compliance (below right)
– Leakages
SAE2013-01-1012
Hydroacoustics / cavitation noise
– Sound propagation in compressible liquid media
– Sound wave absorption treatments to avoid boundary reflections
– Multi-phase phenomena
Aeroacoustics in v8 towards infinite possibilities
Aeroacoustics Simulations Options
Steady state Transient
Broadband
Correlations
Synthesized
Fluctuations SNGR
CURLE surface
PROUDMAN volume
GOLDSTEIN 2D-axi
LEE
Lilley
Mesh Frequency Cut-off
LES
DES
Transient RANS
Point/Surface FFTs and iFFTs
Auto and Cross Spectra – coherence and phase
FW-H
Export commercial propagation codes
Export to
Propagation codes
Direct Noise Propagation
1D (and 2D) Wavenumber analysis
Focus on Transient and Aeroacoustics
– LES-type turbulence model • DES (options of Spalart-Allmaras, k-ε, k-ωSST)
• DES advection scheme blending
• Full LES (wall resolved or under-resolved ! )
– Advanced wall treatment • y+ insensitive
– Non-reflecting conditions for • Inflow and outflow boundaries
– Full Compressibility • Interaction between the flow and acoustics
– Especially for cavity resonance
– Very efficient commercial transient solver • 2nd order space and time discretisation
– Spectral Analysis • FFT and iFFTs at points and surfaces
• Auto and Cross spectra – coherence and phase
• Frequency and Wave Number Fourier analysis
FFT post-processing (point)
– Monitor point in mirror wake
– Tail-off in predicted spectrum at mesh cut-off frequency of ~1000 Hz
STAR
Experiment
Direct Propagation in STAR-CCM+
– Mesh requirement
• 20 cells per acoustic wavelength ( λ= c / f )
– In ambient conditions, you need cells of ~15mm to propagate a signal at 1000Hz
–Domain size = 1000D, (~10 λ )
–Double precision code
– Ideal-gas Non-reflective in/outflow boundaries
– STAR results capture the acoustic sources for propagation via
• Ffowcs Williams-Hawkings (far-field propagation of compact sources without internal reflections)
– STAR offers coupling to 3rd party propagation codes:
• FFT, ACTRAN
• LMS, Virtual.Lab.Acoustics
• ESI, VA-One
– VibroAcoustics
• Using FVS in STAR-CCM+
• Export to SEA and FEA
100 Hz 500 Hz
3150 Hz Overall
Propagation – FW-H and 3rd party code export
Introduction to 1D (line) WaveNumber Analysis
Φc(k,ѡ)
ѡ
k
k0=ѡ/c0
kc=ѡ/Uc
Φ0 (k, ѡ)
Φc(k,ѡ)
ѡ
k
k0=ѡ/c0
kc=ѡ/Uc
Φ0 (k, ѡ)
Bremner and Wilby AIAA-2002-2551
Wavenumber (rad/m)
Idealised side-view mirror
DARP acoustic tunnel open section
40ms-1 open jet
Mirror height is 15cm
Re = 2x105 based on mirror diameter (half dimensions of the original
Daimler experiment AIAA-1999-1895)
11 million cells
Refined wake and “side-glass”
2mm resolution
CFD previously validated
– AIAA-2011-2843
Southampton University Setup
1D wave number analysis on attached and separated
zones
a+ a-
u-
a+ a-
u+
2D wave number analysis at discrete frequencies
Convective ridge Acoustic circle
Separating the acoustic content
Total and acoustic power input to vibration analysis
Widely applicable modelling for flow noise prediction
Substantial investment towards
– answering current and needs
– driving future expectations
in Aeroacoustics
and
AeroVibroacoustics
THANK YOU for your KIND ATTENTION
QUESTIONS?
Summary