TECHNICAL PAPERS
Oct 1, 2006

Construction of Customized Mass-Stiffness Pairs Using Templates

Publication: Journal of Aerospace Engineering
Volume 19, Issue 4

Abstract

This paper is a tutorial exposition of the template approach to the construction of customized mass-stiffness pairs for selected applications in structural dynamics. The exposition focuses on adjusting the mass matrix while a separately provided stiffness matrix is kept fixed. Two well known kinetic-energy discretization methods described in finite-element method (FEM) textbooks since the mid-1960s lead to diagonally lumped and consistent mass matrices, respectively. These two models are sufficient to cover many engineering applications. Occasionally, however, they fall short. The gap can be filled with a more general approach that relies on the use of templates. These are algebraic forms that carry free parameters. This approach is discussed in this paper using one-dimensional structural elements as examples. Templates have the virtue of producing a set of mass matrices that satisfy certain a priori constraint conditions such as symmetry, nonnegativity, invariance, and momentum conservation. In particular, the diagonally lumped and consistent versions can be obtained as instances. Thus those standard models are not excluded. Availability of free parameters, however, allows the mass matrix to be customized to special needs, such as high precision vibration frequencies or minimally dispersive wave propagation. An attractive feature of templates for FEM programming is that only one element implementation as module with free parameters is needed, and need not be recoded when the application problem class changes.

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Acknowledgments

The pioneering contributions of Professor Noor to two of the tools heavily used in this paper: continuification of dynamic lattices as surveyed in Noor (1988) and the use of CAS in computational mechanics as discussed in Noor and Andersen (1979), are gratefully acknowledged. Preparation of this paper has been supported by the National Science Foundation under Grant No. NSFCMS–0219422.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 19Issue 4October 2006
Pages: 241 - 258

History

Received: Oct 20, 2005
Accepted: Jan 6, 2006
Published online: Oct 1, 2006
Published in print: Oct 2006

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Carlos A. Felippa
Dept. of Aerospace Engineering Sciences and Center for Aerospace Structures, Campus Box 429, Univ. of Colorado, Boulder, CO 80309-0429. E-mail: [email protected]

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