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Refinement of Timoshenko Beam Theory for Composite and Sandwich Beams Using Zigzag KinematicsA new refined theory for laminated-composite and sandwich beams that contains the kinematics of the Timoshenko Beam Theory as a proper baseline subset is presented. This variationally consistent theory is derived from the virtual work principle and employs a novel piecewise linear zigzag function that provides a more realistic representation of the deformation states of transverse shear flexible beams than other similar theories. This new zigzag function is unique in that it vanishes at the top and bottom bounding surfaces of a beam. The formulation does not enforce continuity of the transverse shear stress across the beam s cross-section, yet is robust. Two major shortcomings that are inherent in the previous zigzag theories, shear-force inconsistency and difficulties in simulating clamped boundary conditions, and that have greatly limited the utility of these previous theories are discussed in detail. An approach that has successfully resolved these shortcomings is presented herein. This new theory can be readily extended to plate and shell structures, and should be useful for obtaining accurate estimates of structural response of laminated composites.
Document ID
20070035078
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Tessler, Alexander
(NASA Langley Research Center Hampton, VA, United States)
DiSciuva, Marco
(Politecnico di Turin Turin, Italy)
Gherlone, Marco
(Politecnico di Turin Turin, Italy)
Date Acquired
August 24, 2013
Publication Date
November 1, 2007
Subject Category
Composite Materials
Report/Patent Number
L-19411
NASA/TP-2007-215086
Funding Number(s)
WBS: WBS 984754.02.07.07.15.04
Distribution Limits
Public
Copyright
Public Use Permitted.
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