Supersonic jet noise reduction by chevrons enhanced with fluidic injection

40th AIAA Fluid Dynamics Conference

Volumn , Issue , 2010, Pages

  Heeb, Nick ^a   Munday, David ^a   Gutmark, Ephraim ^a   Liu, Junhui ^b   Kailasanath, K ^b,c  

^a UNIVERSITY OF CINCINNATI   (United States)

^b NAVAL RESEARCH LABORATORY   (United States)

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

Author keywords

[No Author keywords available]

Indexed keywords

FAR FIELD; MOMENTUM FLUX; OPERATING CONDITION; OPERATING RANGES; OVERALL SOUND PRESSURE LEVEL; SHOCK-CELL; SUPERSONIC JETS; TURBULENT KINETIC ENERGY;

ACOUSTIC FIELDS; ACOUSTIC NOISE MEASUREMENT; FLUID DYNAMICS; FLUIDICS; KINETIC ENERGY; SUPERSONIC AERODYNAMICS;

FLOW FIELDS;

EID: 78649456956     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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