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Nonlinear vibration of cylindrical shellsThe large amplitude vibration of a thin-walled cylindrical shell is analyzed. A perturbation method is used to solve the steady-state forced vibration problem. The simply-supported boundary conditions and the circumferential periodicity condition are satisfied. The resulting solution indicates that in addition to the fundamental mode, the response contains asymmetric modes as well as axisymmetric modes with the frequency twice that of the fundamental mode. Vibrations involving a single driven mode response are investigated. The results indicate that the nonlinearity is either softening or hardening depending on the mode. The vibrations involving both a driven mode and a companion mode are also investigated. An experimental investigation is conducted, and the results are in qualitative agreement with the theory. 'Nonstationary' response is detected at some frequencies for large amplitude response in which the amplitude drifts from one value to another. Various nonlinear phenomena are observed and comparisons with the theoretical results are made.
Document ID
19750062102
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Chen, J. C.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Babcock, C. D.
(California Institute of Technology Pasadena, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1975
Publication Information
Publication: AIAA Journal
Volume: 13
Subject Category
Structural Mechanics
Accession Number
75A46174
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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