Extension of the Strain Energy Updating Technique to a Multilayered Shell Model with Adaptive Displacements and Fixed DOF
Author:
Affiliation:
1. Associate Professor, Dipt. di Ingegneria Meccanicae Aerospaziale Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Torino, Italy.
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000184
Reference42 articles.
1. Theories for laminated and sandwich plates
2. Thick beam theory and finite element model with zig-zag sublaminate approximations
3. Modeling of delamination in composite laminates using a layer-wise plate theory
4. Assessment of computational models for sandwich panels and shells
5. A new FE model based on higher order zigzag theory for the analysis of laminated sandwich beam with soft core
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2. C0 Layerwise Model with Fixed Degrees of Freedom and Variable In- and Out-of-Plane Kinematics by Strain Energy Updating Technique;Aerospace;2015-11-17
3. C0 Fixed Degrees of Freedom Zigzag Model with Variable In-Plane and Out-of-Plane Kinematics and Quadrilateral Plate Element;Journal of Aerospace Engineering;2015-09
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