Numerical investigation of tonal airfoil self-noise generated by an acoustic feedback-loop

16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)

Volumn , Issue , 2010, Pages

  Jones, Lloyd E ^a,b   Sandberg, Richard D ^a,b  

^a UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

^b Research Institute for Industry   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; AIRFOILS; ANGLE OF ATTACK; BOUNDARY LAYERS; FEEDBACK; LINEAR STABILITY ANALYSIS;

ACOUSTIC FEEDBACK; ANGLES OF ATTACK; BROADBAND NOISE; FEED-BACK LOOP; INSTABILITY WAVES; NUMERICAL INVESTIGATIONS; TIME-AVERAGED; TRAILING EDGES;

ACOUSTIC NOISE;

EID: 78649571515     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-3701     Document Type: Conference Paper

References (17)

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