Interaction of an oblique shock wave with a pair of parallel vortices: Shock dynamics and mechanism of sound generation

Physics of Fluids

Volumn 18, Issue 12, 2006, Pages

  Zhang, Shuhai ^a   Zhang, Yong Tao ^b   Shu, Chi Wang ^c  

^a CHINA AERODYNAMICS RESEARCH AND DEVELOPMENT CENTER   (China)

^b UNIVERSITY OF NOTRE DAME   (United States)

^c BROWN UNIVERSITY   (United States)

Author keywords

Acoustic waves; Finite difference methods; Flow simulation; Mach number; Navier Stokes equations; Shock wave effects; Transonic flow; Vortices

Indexed keywords

ACOUSTIC FIELDS; ACOUSTIC WAVE REFLECTION; COMPUTER SIMULATION; FINITE DIFFERENCE METHOD; FLOW INTERACTIONS; NAVIER STOKES EQUATIONS; SHOCK WAVES; TRANSONIC FLOW; VORTEX FLOW; ACOUSTIC GENERATORS; PLASMA SHOCK WAVES;

FLOW SIMULATION; MACH NUMBER; SHOCK DYNAMICS; SOUND GENERATION; COMPRESSIBLE NAVIER-STOKES EQUATIONS; COUPLING PROCESS; FINITE DIFFERENCE SCHEME; GEOMETRY PARAMETER; OBLIQUE SHOCK WAVES; REFLECTED SHOCK WAVES; SHOCK-VORTEX INTERACTION; WEIGHTED ESSENTIALLY NONOSCILLATORY;

ACOUSTIC WAVE PROPAGATION; VORTEX FLOW;

ACOUSTIC FIELDS; ACOUSTIC WAVE PROPAGATION; ACOUSTIC WAVE REFLECTION; COMPUTER SIMULATION; FINITE DIFFERENCE METHOD; FLOW INTERACTIONS; NAVIER STOKES EQUATIONS; SHOCK WAVES; TRANSONIC FLOW; VORTEX FLOW;

EID: 33846112020     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.2391806     Document Type: Article

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