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A Transient Response Method for Linear Coupled SubstructuresA method is presented for determining the transient response of a discrete coordinate model of a linear structural system composed of substructures. The method is applicable to systems consisting of any number of substructures, both determinate and indeterminate interface boundaries, and any topological arrangement of the substructures. The method is simple to implement from a computational point of view because the equations of motion of each of the substructures are solved independently, and the interface boundary compatibility conditions are enforced at each integration time step by a matrix multiplication. The method is demonstrated for a structural system consisting of two beam segments and acted upon by a time dependent force. The numerical results from the demonstration problem validates the accuracy of the method. The application of this method to structural systems with changing interface boundary conditions between substructures is discussed.
Document ID
19900004128
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Admire, J. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Brunty, J. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1989
Subject Category
Astrodynamics
Report/Patent Number
NAS 1.60:2926
NASA-TP-2926
Report Number: NAS 1.60:2926
Report Number: NASA-TP-2926
Accession Number
90N13444
Funding Number(s)
PROJECT: RTOP 551-53-22-301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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