Cavity noise control through upstream mass injection from a Coanda surface

2nd AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 1996, Pages

  Mendoza, J M ^a,b   Ahuja, K K ^a,c  

^a GEORGIA TECH RESEARCH INSTITUTE   (United States)

^b SCHOOL OF AEROSPACE ENGINEERING   (United States)

^c Aerospace Sciences Laboratory   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AEROACOUSTICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; NOISE ABATEMENT;

BOUNDARY LAYER THICKNESS; BOUNDARY LAYER VELOCITY; CAVITY LENGTH; CAVITY TONES; COMPLETE CONTROL; FLOW DIRECTION; MASS INJECTION; PROOF OF CONCEPT;

FIGHTER AIRCRAFT;

EID: 33748304563     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1767     Document Type: Conference Paper

References (11)

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