Response surface method optimization of uniform and axially segmented duct acoustics liners

Journal of Aircraft

Volumn 43, Issue 4, 2006, Pages 1089-1102

  Lafronza, L ^a   McAlpine, A ^a   Keane, A J ^a   Astley, R J ^a,b  

^a UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC WAVE PROPAGATION; APPROXIMATION THEORY; ATTENUATION; DUCTS; FLIGHT DYNAMICS; MATHEMATICAL MODELS; OPTIMIZATION;

ACOUSTIC LINER; AEROENGINE INLET DUCT; BROADBAND NOISE; RESPONSE SURFACE METHOD; TONAL NOISE;

AIRCRAFT ENGINES;

EID: 33748073114     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.17727     Document Type: Article

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