Entropy Splitting for High Order Numerical Simulation of Vortex Sound at Low Mach Numbers

Journal of Scientific Computing

Volumn 17, Issue 1-4, 2002, Pages 181-190

  Müller, Bernhard ^a   Yee, H C ^b  

^a UPPSALA UNIVERSITY   (Sweden)

^b NASA AMES RESEARCH CENTER   (United States)

Author keywords

Entropy splitting; Euler equations; High order difference method; Low Mach number aeroacoustics; Summation by parts

Indexed keywords

ACOUSTIC WAVES; AERODYNAMICS; COMPUTER SIMULATION; ENERGY DISSIPATION; ENTROPY; NUMERICAL METHODS; PERTURBATION TECHNIQUES; VORTEX FLOW;

ENTROPY SPLITTING; EULER EQUATIONS; HIGH ORDER DIFFERENCE METHODS; LOW MACH NUMBER AEROACOUSTICS; SUMMATION BY PARTS;

NATURAL SCIENCES COMPUTING;

EID: 1942475774     PISSN: 08857474     EISSN: None     Source Type: Journal    
DOI: 10.1023/a:1015100614522     Document Type: Conference Paper

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