Computation of wall pressure spectra from steady flow data for noise prediction

16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)

Volumn , Issue , 2010, Pages

  Remmler, S ^a,c   Christophe, J ^a,d   Anthoine, J ^a,d,e   Moreau, S ^b,f  

^a VON KARMAN INSTITUTE FOR FLUID DYNAMICS   (Belgium)

^b UNIVERSITÉ DE SHERBROOKE   (Canada)

^c TECHNICAL UNIVERSITY OF MUNICH   (Germany)

^d Environmental and Applied Fluid Dynamics Department   (Germany)

^e ONERA   (France)

^f Département de Génie Mécanique   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC NOISE MEASUREMENT; AIRFOILS; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMPUTATION THEORY; COMPUTATIONAL AEROACOUSTICS; NAVIER STOKES EQUATIONS; PRESSURE GRADIENT; TURBULENCE MODELS; WIND TUNNELS;

ADVERSE PRESSURE GRADIENT; AERO-ACOUSTIC ANALOGIES; BOUNDARY LAYER TURBULENCE; CONTROLLED DIFFUSION AIRFOILS; FLAT PLATE BOUNDARY LAYERS; REYNOLDS-AVERAGED NAVIER-STOKES; WALL PRESSURE SPECTRUM; WALL-PRESSURE FLUCTUATIONS;

WALL FLOW;

EID: 78649624515     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4000     Document Type: Conference Paper

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