A wavenumber approach to modelling the response of a randomly excited panel, part II: Application to aircraft panels excited by a turbulent boundary layer

Journal of Sound and Vibration

Volumn 252, Issue 1, 2002, Pages 115-139

  Maury, C ^a   Gardonio, P ^a   Elliott, S J ^a  

^a UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC RADIATORS; BOUNDARY LAYERS; COMPUTER SIMULATION; PARAMETER ESTIMATION; STRUCTURAL PANELS; TURBULENT FLOW;

FLOW-INDUCED NOISE; HORIZONTAL TAILS; WAVENUMBER; WHEEL CAVITIES;

AIRCRAFT;

EID: 0038555217     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.2001.4029     Document Type: Article

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