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Nonlinear finite element formulation for the large displacement analysis in multibody system dynamicsA total Lagrangian finite element formulation for the deformable bodies in multibody mechanical systems that undergo finite relative rotations is developed. The deformable bodies are discretized using finite element methods. The shape functions that are used to describe the displacement field are required to include the rigid body modes that describe only large translational displacements. This does not impose any limitations on the technique because most commonly used shape functions satisfy this requirement. The configuration of an element is defined using four sets of coordinate systems: Body, Element, Intermediate element, Global. The body coordinate system serves as a unique standard for the assembly of the elements forming the deformable body. The element coordinate system is rigidly attached to the element and therefore it translates and rotates with the element. The intermediate element coordinate system, whose axes are initially parallel to the element axes, has an origin which is rigidly attached to the origin of the body coordinate system and is used to conveniently describe the configuration of the element in undeformed state with respect to the body coordinate system.
Document ID
19900013699
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rismantab-Sany, J.
(Illinois Univ. Chicago, IL, United States)
Chang, B.
(Illinois Univ. Chicago, IL, United States)
Shabana, A. A.
(Illinois Univ. Chicago, IL, United States)
Date Acquired
September 6, 2013
Publication Date
December 15, 1989
Publication Information
Publication: JPL, Proceedings of the 3rd Annual Conference on Aerospace Computational Control, Volume 1
Subject Category
Computer Programming And Software
Accession Number
90N23015
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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