Large-eddy simulation of a supersonic jet and its near-field acoustic properties - Methodology & validation

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Liu, Junhui ^a   Kailasanath, K ^a,d   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)

^d Center for Reactive Flow and Dynamical Systems   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

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

ACOUSTIC PROPERTIES; AEROSPACE ENGINEERING; ATMOSPHERIC BOUNDARY LAYER; LARGE EDDY SIMULATION; NOZZLES; VELOCITY MEASUREMENT;

SUPERSONIC AERODYNAMICS;

EID: 78649272710     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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