Computational aeroacoustic analysis of flow around a complex nose landing gear configuration

14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)

Volumn , Issue , 2008, Pages

  Li, Yanbing ^a   Satti, Rajani ^a   Lew, Phoi Tack ^a   Shockx, Richard ^a   Nöelting, Swen ^a  

^a EXA CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTIC ANALYSIS; BOUNDARY GEOMETRY; CARTESIAN GRID SYSTEMS; FLUID FLOW; GEAR ASSEMBLIES; GEAR COMPONENTS; INSTANTANEOUS FLOW; KINETIC EQUATIONS; LATTICE BOLTZMANN EQUATIONS; LATTICE-BOLTZMANN METHOD; LEVEL FLUCTUATION; LOCAL FLOWS; LOW AND HIGH FREQUENCIES; MACROSCOPIC FLOW; NEAR-FIELD; NOISE GENERATION; NOSE LANDING GEAR; PARTICLE DENSITY DISTRIBUTIONS; RENORMALIZATION GROUP; TIME-SCALES; TRANSPORT EQUATION;

BOLTZMANN EQUATION; COMPUTATIONAL AEROACOUSTICS; DISTRIBUTION FUNCTIONS; INCOMPRESSIBLE FLOW; INTEGRAL EQUATIONS; KINETIC ENERGY; KINETIC THEORY; KINETICS; LANDING; LANDING GEAR (AIRCRAFT); TWO PHASE FLOW;

FLOW SIMULATION;

EID: 78249282956     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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