Efficient computation of spinning modal radiation through an engine bypass duct

AIAA Journal

Volumn 46, Issue 6, 2008, Pages 1413-1423

  Huang, Xun ^a,b,c   Chen, Xiaoxian ^a,b   Ma, Zhaokai ^a,b   Zhang, Xin ^a,b,c  

^a UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

^b Aeronautics and Astronautics   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE PROPAGATION; ACOUSTICS; AIRCRAFT ENGINES; COMPUTATIONAL EFFICIENCY; CRACK PROPAGATION; DUCTS; FORECASTING; LINEAR EQUATIONS; LINEARIZATION; MESH GENERATION; PARTIAL DIFFERENTIAL EQUATIONS; PERTURBATION TECHNIQUES; PHOTOACOUSTIC EFFECT; RADIATION; TURBULENT FLOW;

ACOUSTIC PERTURBATION EQUATIONS; ADAPTIVE MESH REFINEMENT (AMR); BYPASS DUCTS; CYLINDRICAL COORDINATES; EFFICIENT COMPUTATION; EXHAUST FLOW; FAR-FIELD DIRECTIVITY; GENERAL (CO); LINEARIZED EULER EQUATIONS (LEE); MEAN FLOWS; MODEL BASED (OPC); NEAR FIELD SOUND; NEAR FIELDS; SEMI INFINITE; SHEAR LAYERS; SOUND PROPAGATION; SOUND RADIATIONS;

EULER EQUATIONS;

EID: 45849112128     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.31136     Document Type: Article

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