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Analysis of transient, linear wave propagation in shells by the finite difference methodThe applicability of the finite difference method to propagation problems in shells, and the response of a cylindrical shell with cutouts to both longitudinal and radial transient excitations are investigated. It is found that the only inherent limitation of the finite difference method is its inability to reproduce accurately response discontinuities. The short wave length limitations of thin shell theory create significant convergence difficulties may often be overcome through proper selection of finite difference mesh dimensions and temporal or spatial smoothing of the excitation. Cutouts produce moderate changes in early and intermediate time response of a cylindrical shell to axisymmetric pulse loads applied at one end. The cutouts may facilitate the undesirable late-time transfer of load-injected extensional energy into nonaxisymmetric flexural response.
Document ID
19720008223
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Geers, T. L.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Sobel, L. H.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1971
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-1885
Report Number: NASA-CR-1885
Accession Number
72N15873
Funding Number(s)
CONTRACT_GRANT: NAS1-9111
PROJECT: RTOP 134-14-04-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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