Large-eddy simulations of a supersonic jet and its near-field acoustic properties

AIAA Journal

Volumn 47, Issue 8, 2009, Pages 1849-1864

  Liu, Junhui ^a   Kailasanath, K ^a   Ramamurti, Ravi ^a   Munday, David ^b   Gutmark, Ephraim ^b   Lohner, Rainald ^c  

^a NAVAL RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF CINCINNATI   (United States)

^c GEORGE MASON UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONVERGENT-DIVERGENT NOZZLE; EXPERIMENTAL DATA; EXPERIMENTAL MEASUREMENTS; JET FLOW; MACH DISK; NEAR-FIELD; NEAR-FIELD ACOUSTICS; NEAR-FIELD INTENSITY; NOISE GENERATION; NOZZLE EXITS; NOZZLE PRESSURE RATIO; NOZZLE THROAT; PRESSURE FLUCTUATION; SCREECH TONES; SHOCK-CELL; SUPERSONIC JET FLOW; SUPERSONIC JETS; THEORETICAL RESULT; TOTAL PRESSURE RATIO; UNDEREXPANDED JET; VELOCITY PROFILES; WAVY STRUCTURES;

ACOUSTIC PROPERTIES; ACOUSTICS; COMPUTATIONAL FLUID DYNAMICS; JETS; LARGE EDDY SIMULATION; NOZZLES; VELOCITY MEASUREMENT;

SUPERSONIC AERODYNAMICS;

EID: 70049092008     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.43281     Document Type: Article

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