A Wavenumber Approach to Modelling the Response of a Randomly Excited Panel, Part II. Application to Aircraft Panels Excited by a Turbulent Boundary Layer

Author： Maury C.   Gardonio P.   Elliott S.J.  

Publisher： Academic Press

ISSN： 0022-460X

Source： Journal of Sound and Vibration, Vol.252, Iss.1, 2002-04, pp. : 115-139

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