Finite/boundary element assessment of a turbofan spliced intake liner at supersonic fan operating conditions

9th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2003, Pages

  McAlpine, A ^a   Wright, M C M ^a   Batard, H ^b   Thezelais, S ^b  

^a UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

^b AIRBUS   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; ACOUSTIC NOISE; AEROACOUSTICS; AIRCRAFT ENGINES; ENGINES; SUPERSONIC AIRCRAFT;

AERO-ENGINE; AZIMUTHAL MODES; ENGINE NOISE SOURCE; FAN SPEED; HIGH BYPASS RATIO; OPERATING CONDITION; WALL IMPEDANCE;

BYPASS RATIO;

EID: 85088719491     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3305     Document Type: Conference Paper

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