Noise prediction of a subsonic turbulent round jet using the lattice-Boltzmann method

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

Volumn , Issue , 2007, Pages

  Lew, Phoi Tack ^a   Lyrintzis, Anastasios ^a   Crouse, Bernd ^b   Balasubramanian, Gana ^b   Freed, David ^b   Mongeau, Luc ^c  

^a Purdue University   (United States)

^b EXA CORPORATION   (United States)

^c MCGILL UNIVERSITY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

CENTERLINE VELOCITY DECAY RATE; COMPUTATIONAL COSTS; COMPUTATIONAL DOMAINS; FAR-FIELD SOUND PRESSURE; FINITE DIFFERENCE SCHEME; LATTICE-BOLTZMANN METHOD; RADIATED SOUND PRESSURE; TURBULENCE INTENSITY;

ACOUSTIC NOISE; DECAY (ORGANIC); KINETIC THEORY; LARGE EDDY SIMULATION; NOZZLES;

AEROACOUSTICS;

EID: 84884789542     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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