Date of Award
Fall 1995
Document Type
Thesis
Degree Name
Master of Science (MS)
Department
Mechanical & Aerospace Engineering
Program/Concentration
Engineering Mechanics
Committee Director
Mohammad A. Aminpour
Committee Member
Chuh Mei
Committee Member
Norman F. Knight, Jr.
Call Number for Print
Special Collections; LD4331.E57 P316
Abstract
A three-node curved and twisted beam element is developed for linear analysis of structures modeled with curved and pre-twisted beams. A set of governing equations consisting of kinematic relations, constitutive relations, and equilibrium equations is derived. The beam element has three rotational and three displacement degrees of freedom at each node. The differential equations of kinematics are solved exactly for linearly varying longitudinal strains, constant transverse shear strains, linearly varying twist, and quadratically varying curvature changes to obtain the description of rotation and displacement modes. These rotation and displacement modes are then used as the basis functions for development of the finite element model. Constitutive relations for the beam are developed for general anisotropic materials and then specialized for isotropic materials. The results of the present element are compared with theoretical solutions available in the literature. Due to compatible assumptions for rotations and displacements and exact representation of rigid-body modes, the beam element is free from spurious modes and exhibits fast convergence to theoretical solutions.
Rights
In Copyright. URI: http://rightsstatements.org/vocab/InC/1.0/ This Item is protected by copyright and/or related rights. You are free to use this Item in any way that is permitted by the copyright and related rights legislation that applies to your use. For other uses you need to obtain permission from the rights-holder(s).
DOI
10.25777/1j2j-mh45
Recommended Citation
Padhye, Umesh V..
"Finite Element Formulation of a Three-Node Spatially Curved and Twisted Beam"
(1995). Master of Science (MS), Thesis, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/1j2j-mh45
https://digitalcommons.odu.edu/mae_etds/643