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contributor authorA. A. Shabana
contributor authorJ. L. Escalona
contributor authorH. A. Hussien
date accessioned2017-05-08T23:57:23Z
date available2017-05-08T23:57:23Z
date copyrightJune, 1998
date issued1998
identifier issn1050-0472
identifier otherJMDEDB-27652#188_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120886
description abstractThere are three basic finite element formulations which are used in multibody dynamics. These are the floating frame of reference approach, the incremental method and the large rotation vector approach. In the floating frame of reference and incremental formulations, the slopes are assumed small in order to define infinitesimal rotations that can be treated and transformed as vectors. This description, however, limits the use of some important elements such as beams and plates in a wide range of large displacement applications. As demonstrated in some recent publications, if infinitesimal rotations are used as nodal coordinates, the use of the finite element incremental formulation in the large reference displacement analysis does not lead to exact modeling of the rigid body inertia when the structures rotate as rigid bodies. In this paper, a simple non-incremental finite element procedure that employs the mathematical definition of the slope and uses it to define the element coordinates instead of the infinitesimal and finite rotations is developed for large rotation and deformation problems. By using this description and by defining the element coordinates in the global system, not only the need for performing coordinate transformation is avoided, but also a simple expression for the inertia forces is obtained. The resulting mass matrix is constant and it is the same matrix that appears in linear structural dynamics. It is demonstrated in this paper that this coordinate description leads to exact modeling of the rigid body inertia when the structures rotate as rigid bodies. Nonetheless, the stiffness matrix becomes nonlinear function even in the case of small displacements. The method presented in this paper differs from previous large rotation vector formulations in the sense that the inertia forces, the kinetic energy, and the strain energy are not expressed in terms of any orientation coordinates, and therefore, the method does not require interpolation of finite rotations. While the use of the formulation is demonstrated using a simple planar beam element, the generalization of the method to other element types and to the three dimensional case is straightforward. Using the finite element procedure presented in this paper, beams and plates can be treated as isoparametric elements.
publisherThe American Society of Mechanical Engineers (ASME)
titleApplication of the Absolute Nodal Coordinate Formulation to Large Rotation and Large Deformation Problems
typeJournal Paper
journal volume120
journal issue2
journal titleJournal of Mechanical Design
identifier doi10.1115/1.2826958
journal fristpage188
journal lastpage195
identifier eissn1528-9001
keywordsRotation
keywordsDeformation
keywordsInertia (Mechanics)
keywordsFinite element analysis
keywordsModeling
keywordsPlates (structures)
keywordsDisplacement
keywordsForce
keywordsStructural frames
keywordsStructural dynamics
keywordsKinetic energy
keywordsInterpolation
keywordsStiffness AND Multibody dynamics
treeJournal of Mechanical Design:;1998:;volume( 120 ):;issue: 002
contenttypeFulltext


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