Linearized perturbed compressible equations for low Mach number aeroacoustics

Journal of Computational Physics

Volumn 218, Issue 2, 2006, Pages 702-719

  Seo, Jung H ^a   Moon, Young J ^a  

^a Korea University   (South Korea)

Author keywords

Computational aeroacoustics; Hybrid method; Low Mach number; Perturbed compressible equations

Indexed keywords

AEROACOUSTICS; AERODYNAMICS; CIRCULAR CYLINDERS; HYDRODYNAMICS; LINEARIZATION; MACH NUMBER; REYNOLDS NUMBER; SHEAR FLOW; VORTEX FLOW;

ACOUSTIC SPLITTING METHOD; AEROACOUSTIC COMPUTATION; COUPLING EFFECT; HYBRID METHOD; LINEARIZED PERTURBED COMPRESSIBLE EQUATIONS; LOW MACH NUMBERS; PERTURBED COMPRESSIBLE EQUATIONS; PERTURBED VELOCITY; REYNOLD NUMBER; VORTICITY TRANSPORT EQUATIONS;

VORTICITY;

EID: 33748905907     PISSN: 00219991     EISSN: 10902716     Source Type: Journal    
DOI: 10.1016/j.jcp.2006.03.003     Document Type: Article

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