Construction of Customized Mass-Stiffness Pairs Using TemplatesSource: Journal of Aerospace Engineering:;2006:;Volume ( 019 ):;issue: 004Author:Carlos A. Felippa
DOI: 10.1061/(ASCE)0893-1321(2006)19:4(241)Publisher: American Society of Civil Engineers
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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| contributor author | Carlos A. Felippa | |
| date accessioned | 2017-05-08T21:16:17Z | |
| date available | 2017-05-08T21:16:17Z | |
| date copyright | October 2006 | |
| date issued | 2006 | |
| identifier other | %28asce%290893-1321%282006%2919%3A4%28241%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45069 | |
| description 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. | |
| publisher | American Society of Civil Engineers | |
| title | Construction of Customized Mass-Stiffness Pairs Using Templates | |
| type | Journal Paper | |
| journal volume | 19 | |
| journal issue | 4 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2006)19:4(241) | |
| tree | Journal of Aerospace Engineering:;2006:;Volume ( 019 ):;issue: 004 | |
| contenttype | Fulltext |