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Dynamic response of nonuniform structures to classes of pressure fieldsA semi-analytical method is developed for the calculation of the response of nonuniform structures to deterministic and random excitation. The method is based on parametric representations of the impulse response and input functions. With these representations, a class of structures of specified geometry and a class of pressure fields of practical concern can be considered simultaneously in a single analytical calculation of structural response. In engineering applications, the parameters in the impulse response function can be fixed once the numerical solution of the associated eigenvalue problem is available; the input function parameters can be specified given a particular input function or pressure field data. This methodology is applied to nonuniform beams and circular cylindrical shells for which parametric response solutions are derived. The computerized version of these solutions is also presented.
Document ID
19720024269
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cottis, M. G.
(KMS Technology Center Van Nuys, CA, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-122477
Report Number: NASA-CR-122477
Accession Number
72N31919
Funding Number(s)
CONTRACT_GRANT: NAS5-21516
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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