Multi-size-mesh, multi-time-step algorithm for noise computation around an airfoil in curvilinear meshes

13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)

Volumn , Issue , 2007, Pages

  Le Garrec, Thomas ^a   Gloerfelt, Xavier ^a   Corre, Christophe ^b  

^a DYNFLUID LABORATORY   (France)

^b LEGI   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; AVIATION; COMPUTATIONAL AEROACOUSTICS; INTERPOLATION; MESH GENERATION; REYNOLDS NUMBER; VORTEX FLOW;

CURVILINEAR MESHES; HIGH-ORDER FINITE DIFFERENCES; HIGH-ORDER METHODS; LOCAL GRID REFINEMENT; MASSIVELY SEPARATED FLOW; MULTIDIMENSIONAL INTERPOLATIONS; NOISE COMPUTATIONS; WAVENUMBER SPACES;

ACOUSTIC NOISE;

EID: 85086613966     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-3504     Document Type: Conference Paper

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