Flow structure and acoustics of supersonic jets from conical convergent-divergent nozzles

Physics of Fluids

Volumn 23, Issue 11, 2011, Pages

  Munday, D ^a   Gutmark, E ^a   Liu, J ^b   Kailasanath, K ^b  

^a UNIVERSITY OF CINCINNATI   (United States)

^b NAVAL RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; ACOUSTIC NOISE; FIGHTER AIRCRAFT; LARGE EDDY SIMULATION; MACH NUMBER; NOZZLES; SUPERSONIC AERODYNAMICS; SURVEYS; VELOCITY MEASUREMENT;

CONVERGENT-DIVERGENT NOZZLE; METHOD OF CHARACTERISTICS; MONOTONICALLY INTEGRATED LARGE-EDDY SIMULATIONS; NEAR-FIELD ACOUSTICS; OPERATING CONDITION; PARTICLE IMAGE VELOCIMETRIES; SHOCK ASSOCIATED NOISE; SIMULATIONS AND MEASUREMENTS;

NOZZLE DESIGN;

EID: 82855169570     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.3657824     Document Type: Article

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