Trailing edge noise of a controlled-diffusion airfoil at moderate and high angle of attack

15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference)

Volumn , Issue , 2009, Pages

  Christophe, J ^a   Anthoine, J ^a   Moreau, S ^b  

^a VON KARMAN INSTITUTE FOR FLUID DYNAMICS   (Belgium)

^b UNIVERSITÉ DE SHERBROOKE   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC WAVE PROPAGATION; AEROACOUSTICS; AIRFOILS; BOUNDARY CONDITIONS; COMPUTATION THEORY; FORECASTING; MESH GENERATION; WAKES; WALL FLOW;

COMPUTATIONAL DOMAINS; COMPUTATIONAL RESULTS; CONTROLLED DIFFUSION AIRFOILS; EXPERIMENTAL EVIDENCE; HIGH ANGLE OF ATTACK; LOW FREQUENCY RANGE; NUMERICAL PARAMETERS; WALL PRESSURE SPECTRUM;

ANGLE OF ATTACK;

EID: 78149422686     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-3196     Document Type: Conference Paper

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