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A general method for dynamic analysis of structures overviewThe presented research deals with the development of a dynamic analysis method for structural systems. The modeling approach is essentially a finite element method in the sense that the structure is divided into n elements. An element is defined as any structural unit whose degree of freedom (dofs) can be categorized as either interface or non-interface dofs. An element could be a fundamental unit such as a rod, a beam, a plate etc., or it could be an entire structural component. Furthermore, the parameters for the element could be distributed or lumped. The choice of elements is totally arbitrary and is a matter of user convenience. In particular, issues of accuracy and convergence do not enter on the level of example that bookkeeping is reduced to a minimum. Each element is modeled using a set of interface constraint modes (ICM) combined with a set of interface restrained normal models (IRNM). The next step is the solution of the system eigenvalue problem. The procedure calls for the sequential solution of a number of small eigenvalue problems based on a truncation principle for IRNM. In addition, the form of these eigenvalue problems is very simple such that an escalator type of eigenvalue problem solver can be used which is extremely cost-effective and fast.
Document ID
19870013274
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Engels, Remi C.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures
Subject Category
Structural Mechanics
Accession Number
87N22707
Funding Number(s)
CONTRACT_GRANT: F29601-85-K-0054
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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