Prediction of aeroacoustic noise from a simplified landing gear using a Lattice Boltzmann scheme

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Noelting, Swen ^a   Wessels, Michael ^a   Freed, David ^b  

^a Exa GmbH   (Germany)

^b EXA CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOLTZMANN EQUATION; COMPUTATIONAL FLUID DYNAMICS; DISTRIBUTION FUNCTIONS; INTEGRAL EQUATIONS; KINETIC THEORY; LANDING GEAR (AIRCRAFT); LARGE EDDY SIMULATION; VORTICITY;

AERO-ACOUSTIC SIMULATION; AEROACOUSTIC NOISE; LATTICE BOLTZMANN EQUATIONS; LATTICE BOLTZMANN METHOD; LATTICE BOLTZMANN METHODS (LBM); LATTICE-BOLTZMANN SCHEME; PARTICLE DENSITY DISTRIBUTIONS; VERY LARGE EDDY SIMULATION (VLES);

AEROACOUSTICS;

EID: 78149428908     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-20     Document Type: Conference Paper

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