Influence of nozzle-exit boundary-layer conditions on the flow and acoustic fields of initially laminar jets

Journal of Fluid Mechanics

Volumn 663, Issue , 2010, Pages 507-538

  Bogey, C ^a   Bailly, C ^a,b  

^a ECOLE CENTRALE DE LYON   (France)

^b INSTITUT UNIVERSITAIRE DE FRANCE   (France)

Author keywords

jet noise; shear layer turbulence; turbulence simulation

Indexed keywords

ACOUSTIC FIELD MEASUREMENT; ACOUSTIC FIELDS; ACOUSTIC NOISE; ATMOSPHERIC THERMODYNAMICS; LARGE EDDY SIMULATION; NOZZLES; REYNOLDS NUMBER; SHEAR FLOW; TURBULENCE; VELOCITY;

ACOUSTIC COMPONENTS; JET NOISE; LOW-FREQUENCY NOISE; PRESSURE DISTURBANCE; ROOT-MEAN-SQUARE (R.M.S.); SHEAR LAYER; TURBULENCE SIMULATION; TURBULENT INTENSITIES;

LAMINAR BOUNDARY LAYER;

ACOUSTICS; JET; LAMINAR FLOW; LARGE EDDY SIMULATION; REYNOLDS NUMBER; SIMULATION; TURBULENCE; VORTEX FLOW;

EID: 78649538139     PISSN: 00221120     EISSN: 14697645     Source Type: Journal    
DOI: 10.1017/S0022112010003605     Document Type: Article

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