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A consistent set of trial functions for conical shellsA consistent approach is developed for the determination of trial functions for a class of shells of revolution. The trial functions satisfy the in-plane and out-of-plane boundary conditions at the shell ends and include the effects of tangential inertia. The resulting expressions converge rapidly for the problem of linear free vibration
Document ID
19810029418
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
doi:10.1016/0022-460X(80)90495-2
Authors
El-Raheb, M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wagner, P. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 11, 2013
Publication Date
November 8, 1980
Publication Information
Publication: Journal of Sound and Vibration
Volume: 73
Subject Category
Structural Mechanics
Accession Number
81A13822
Distribution Limits
Public
Copyright
Other

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