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On an integro-differential equation model for the study of the response of an acoustically coupled panelThe response of a clamped panel to supersonically convected turbulence is considered. A theoretical model in the form of an integro-differential equation is employed that takes into account the coupling between the panel motion and the surrounding acoustic medium. The kernels of the integrals, which represent induced pressures due to the panel motion, are Green's functions for sound radiations under various moving and stationary sources. An approximate analysis is made by following a finite-element Ritz-Galerkin procedure. Preliminary numerical results, in agreement with experimental findings, indicate that the acoustic damping is the controlling mechanism of the response.
Document ID
19750041702
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yen, D. H. Y.
(Michigan State University East Lansing, Mich., United States)
Maestrello, L.
Padula, S.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1975
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 75-508
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aero-Acoustics Conference
Location: Hampton, VA
Start Date: March 24, 1975
End Date: March 26, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A25774
Distribution Limits
Public
Copyright
Other

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