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Transient Response of Shells of Revolution by Direct Integration and Modal Superposition MethodsThe results of an analytical effort to obtain and evaluate transient response data for a cylindrical and a conical shell by use of two different approaches: direct integration and modal superposition are described. The inclusion of nonlinear terms is more important than the inclusion of secondary linear effects (transverse shear deformation and rotary inertia) although there are thin-shell structures where these secondary effects are important. The advantages of the direct integration approach are that geometric nonlinear and secondary effects are easy to include and high-frequency response may be calculated. In comparison to the modal superposition technique the computer storage requirements are smaller. The advantages of the modal superposition approach are that the solution is independent of the previous time history and that once the modal data are obtained, the response for repeated cases may be efficiently computed. Also, any admissible set of initial conditions can be applied.
Document ID
19740015337
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stephens, W. B.
(NASA Langley Research Center Hampton, VA, United States)
Adelman, H. M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
L-9216
NASA-TM-X-2916
Report Number: L-9216
Report Number: NASA-TM-X-2916
Accession Number
74N23450
Funding Number(s)
PROJECT: RTOP 502-32-01-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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