Effects of moderate Reynolds numbers on subsonic round jets with highly disturbed nozzle-exit boundary layers

Physics of Fluids

Volumn 24, Issue 10, 2012, Pages

  Bogey, Christophe ^a   Marsden, Olivier ^a   Bailly, Christophe ^a,b  

^a ECOLE CENTRALE DE LYON   (France)

^b INSTITUT UNIVERSITAIRE DE FRANCE   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; BOUNDARY LAYERS; LARGE EDDY SIMULATION; NOZZLES; REYNOLDS NUMBER; TURBULENCE; TURBULENT FLOW; VELOCITY;

CONTROLLED CONDITIONS; FINE-SCALE STRUCTURES; MEAN VELOCITY PROFILES; MODERATE REYNOLDS NUMBERS; SOUND PRESSURE LEVEL; TURBULENCE INTENSITY; TURBULENT BOUNDARY LAYERS; VELOCITY FLUCTUATIONS;

FIGHTER AIRCRAFT;

EID: 84868624333     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.4757667     Document Type: Article

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