On the noise and wake flow of an airfoil with broken and serrated trailing edges

17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference)

Volumn , Issue , 2011, Pages

  Chong, Tze Pei ^a   Vathylakis, Alexandros ^a   Joseph, Phillip ^b   Gruber, Mathieu ^b  

^a BRUNEL UNIVERSITY   (United Kingdom)

^b UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOSS; ANGLES OF ATTACK; COUNTER-ROTATING VORTICES; EXPERIMENTAL PROGRAM; LOW REYNOLDS NUMBER FLOW; NOISE MECHANISMS; SERRATED TRAILING EDGES; TOLLMIEN-SCHLICHTING WAVES;

AEROACOUSTICS; AIRFOILS; ANGLE OF ATTACK; NOISE ABATEMENT; REYNOLDS NUMBER; STABILITY; VORTEX FLOW; VORTEX SHEDDING; WAKES;

ACOUSTIC NOISE;

EID: 84878765835     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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12. th AIAA/CEAS Aeroacoustic Conference, Stockholm, Sweden.
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18. th AIAA/CEAS Aeroacoustic Conference, Stockholm, Sweden.