Industries stries & A Applic licat ations ions Marine - - PowerPoint PPT Presentation

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Industries stries & A Applic licat ations ions Marine - - PowerPoint PPT Presentation

Industries stries & A Applic licat ations ions Marine Propeller noise Cavitation Hull/propeller/rudder interaction Automotive Wing mirror Sunroof noise Aerospace HVAC systems High Lift Devices


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SLIDE 1
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SLIDE 2

Industries stries & A Applic licat ations ions

Aerospace

  • High Lift Devices
  • Landing Gear
  • ECS
  • Jet and turbo noise

Automotive

  • Wing mirror
  • Sunroof noise
  • HVAC systems
  • Turbo chargers
  • Cooling fans
  • Exhaust systems
  • Interior transmission

Building Environment

  • HVAC ducting
  • Fan noise

Electronics cooling

  • Fan noise
  • Air conditioning

Power Generation

  • Pipe / duct / cavity resonances
  • Compressor / turbine / combustor

Marine

  • Propeller noise
  • Cavitation
  • Hull/propeller/rudder interaction
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SLIDE 3

STAR-CCM+ CM+ Aeroac acoust

  • ustics

ics Capabilit bilities ies

Flow & Propagation

CURLE (Surface) PROUDMAN (volume) GOLDSTEIN (2D-axisymertric) LEE Analogy LILLEY Analogy FW-H Tonal blade passing

LES DES

FW-H Propagation

Simulation Options

Steady state Unsteady

Broadband Correlations Synthesized Direct Direct Simulation of Noise Propagation

Steady-state and Transient Post- Processing

Mesh Frequency Cut-off Point & Surface FFTs Point & Surface Inverse FFTs Direct export to Acoustics and SEA codes

Aeroacoustics

Band Stop & Pass Filters and Finite Impulse Response (FIR) Wave-number analysis including Cross Spectral Analysis for Phase and Coherence Uniform grid mapping and Export to MATLAB Non-conformal mapping to structures codes

Compressible Non-reflective Turbulence

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SLIDE 4

HVAC, C, ECS, S, Duct t ventilation ilation and disc schar arge ge

AIAA2012-2068

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SLIDE 5

Deba bati tin, , K, EC ECCOMA MAS S CFD 2006 2006

ECS S and electr tronic

  • nic rack coolin

ling

Elbow with flow straightener Plenum Inlet Bulk Velocity Outlet Pressure on all holes on each shelve Restrictor

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SLIDE 6

Deba bati tin, , K, EC ECCOMA MAS S CFD 2006 2006

ECS S and electr tronic

  • nic rack coolin

ling

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SLIDE 7

Deba bati tin, , K, EC ECCOMA MAS S CFD 2006 2006

ECS S and electr tronic

  • nic rack coolin

ling

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SLIDE 8

Deba bati tin, , K, EC ECCOMA MAS S CFD 2006 2006

ECS S and electr tronic

  • nic rack coolin

ling

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SLIDE 9

Ext xtern ernal al Aeroa

  • aco

coust ustic ic Excitation itation and Intern ernal al Noise se Tran ansm smission ission (also, lso, see later) er)

Surface FFT (dB) at 500Hz (top) and 1000Hz (bottom)

AIAA2012-2205 AIAA2012-2206 SAE2013-01-0640

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SLIDE 10

Turbo bo compressor ressor Noise se

GT2012-70028

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SLIDE 11

HVAC C – blower er, , distr tribu ibutor

  • r,

, ducts, s, flaps ps

SAE13-01-0856

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Pipe e net etwor

  • rk

k singing ging

AIAA2012-2171

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Sunroo

  • of/side

f/side-windo window w buffeti eting g – real l vehicle le effects ts

Uncorrected Correlated

Alumin iniu ium Persp rspex MDF

– Wall compl mplian ance ce effec ects ts

  • Full FSI of comp

mplian ant t wal walls s (above right) ght)

  • Corre

relati tions ns for wal wall comp mplianc nce e (below right ht)

– Leaka kages ges

SAE2013-01-1012

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SLIDE 14

Acoust stic ic Tramsmission amsmission Loss s - muffler flers

L lextruded Douter Dinner

1D GT-POWER STAR-CCM+ (unfiltered) STAR-CCM+ (low pass filter) Transmission Loss (dB)

Pure Acoustical Transmission Loss

– Including porous media – In the presence of flow Productio

  • duction geome
  • metry test

t by y InDeS eSa Ideali ealise sed d geome

  • metr

try test by CD-ada adapco

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Aerospa

  • space

ce: : Airframe frame and Jet et noise se

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Traili ailing ng edge self lf noise se @ Re ~ 2x105

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Propeller peller noise se – vortex x wake e interaction eraction

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Hydroac

  • acousti
  • ustics

– Sound propagation in compressible liquid media – Multi-phase phenomena (bubble growth/collapse) – Hull boundary layer noise with LES (Re~107-108)

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Focus s on Transient ansient and Aeroa

  • acoustics

coustics

– LES-type turbulence model

  • DES (opti

tions

  • ns of Spalart-Allmar

maras as, , k-ε, k-ωSST)

  • DES advecti

tion n scheme blendi ding ng

  • Full LES (wal

wall resolved) ed)

– Advanced wall treatment

  • y+ inse

nsens nsitive

– Non-reflecting boundaries for ideal gases – Acoustic far-field damping in compressible liquids – Full Compressibility

  • Intera

eracti ction n bet etween the flow and acoustics stics

– Espec ecia ially lly for cavi vity ty /duct t reson sonanc ances es

– Efficient implicit transient solver

  • 2nd

nd order

r space and time discreti scretisati sation

– Spectral Analysis

  • FFT and iFFTs at points

nts and surfac aces es

  • Auto and Cross

ss spectra ctra – coherence nce and phase se

  • Frequ

quency ncy and Wave Number r Fouri rier r analysis sis

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Direct ect Propagat pagation ion in STAR-CC CCM+

– Mesh requirement

  • 20 cells per acoustic wavelength ( λ= c / f )

– In ambient air, 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 – Compressible liquid far-field acoustic reflecting-avoidance treatments

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– STAR results capture the acoustic sources for propagation via

  • Ffowcs Williams-Hawki

wkings ngs (far-field eld pro ropagati tion n of compact sources) – STAR offers coupling to 3rd party propagation codes:

  • FFT, ACTRAN

AN

  • LMS,

, Virtu tual.L al.Lab.A .Acou

  • ustics

tics

  • ESI, VA-One

– Aero-VibroAcoustics

  • Using

ng FVS in STAR-CC CCM+

  • Export

t to SEA and FEA

100 0 Hz 500 0 Hz 3150 50 Hz Over erall all

Propagat pagation ion – FW FW-H H and 3rd

rd party

ty code expor

  • rt
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SLIDE 22

Introdu

  • duction

ction to 1D (line) ine) WaveNumber mber Analysis ysis

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)

Bremne mner and Wilby AIAA-200 2002-255 2551

Wave venumber (rad/m) /m)

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SLIDE 23

1D wave number er analysis lysis on attac ached hed and separat arated ed zones es

a+ a- u- a+ a- u+

AIAA2012-2205 AIAA2012-2206 SAE2013-01-0640

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2D wave number er analysis lysis at disc scre rete e freque uencies cies

Convectiv ctive e ridge ge Ac Acoustic tic circl cle

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Separat arating g the acoustic stic conten ent

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Total al and acoust stic ic power input ut to vibrat ration ion analysis ysis

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Widely dely applicable able modellin

  • delling

g for flow w noise se predic dicti tion

  • n

Continued ntinued invest stment ent towar ards ds

– answering current needs – driving future expectations

in n Aeroacous

  • acoustics

ics and towar ards ds AeroV

  • Vibr

ibroacou

  • acoust

stics ics THA HANK NK YOU OU for your ur KIND ND ATTEN ENTION TION

Summa mmary

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