Identification of the effects of the nozzle-exit boundary-layer thickness and its corresponding Reynolds number in initially highly disturbed subsonic jets

Physics of Fluids

Volumn 25, Issue 5, 2013, Pages

  Bogey, Christophe ^a   Marsden, Olivier ^a  

^a ECOLE CENTRALE DE LYON   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; FIGHTER AIRCRAFT; LARGE EDDY SIMULATION; MIXING; NOZZLES; REYNOLDS NUMBER; SHEAR FLOW; TURBULENCE; VELOCITY;

BOUNDARY LAYER THICKNESS; DISTURBANCE LEVEL; EMISSION ANGLE; HIGH REYNOLDS NUMBER; JET VELOCITIES; MEAN VELOCITY PROFILES; SPREADING RATE; TURBULENCE INTENSITY;

LAMINAR BOUNDARY LAYER;

EID: 84878543412     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.4807071     Document Type: Article

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