Thie paper describes the development and application
of numerical tools for the dynamic analysis of acouetical
and structural-acoustical systems. Use is made of an
analogon between the differential equations of structural
dynamics and acoustics, which enables the use of readily
developed F.E.M.-codes (in this etudy NASTRAN). The models
on which the dynamic analyses have been performed are an
unstiffened circular cylindrical shell and its enclosed
volume of air. The types of analyses which have been implemented
are: an uncoupled acoustical modal and modal
respons analysis, a sound intensity computation on the
interface surface of the two models and a coupled structural-
acoustical modal analysis. It will be shown that it is
strictly necesaary to perform the coupled analysis for
this highly idealized fuselage model.
Original language | English |
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Title of host publication | Voorjaarsvergadering 1988 : voordrachten gehouden op de bijeenkomst van 1 maart 1988 te Utrecht |
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Place of Publication | Delft |
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Publisher | Nederlands Akoestisch Genootschap |
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Pages | 11-23 |
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Publication status | Published - 1988 |
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Name | Publikatie Nederlands Akoestisch Genootschap |
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Volume | 92 |
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