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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Groh, Rainer Mj
University of Bristol
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (45/45 displayed)
- 2024Quantifying efficient shape-shiftingcitations
- 2024Dataset for computational and experimental buckling analysis of constant-stiffness and variable-stiffness composite cylinders
- 2023Local Analysis-Test Correlation of Tow-Steered Composite Shells with Small Cutouts
- 2023Increasing reliability of axially compressed cylinders through stiffness tailoring and optimizationcitations
- 2022Probing the stability landscape of prestressed stayed columns susceptible to mode interactioncitations
- 2021Optimization of imperfection-insensitive continuous tow sheared rocket launch structurescitations
- 2021Design of Shape-Adaptive Deployable Slat-Cove Filler for Airframe Noise Reductioncitations
- 2021Manufacture and buckling test of a variable-stiffness, variable-thickness composite cylinder under axial compressioncitations
- 2021Flexural analysis of laminated beams using zigzag theory and a mixed inverse differential quadrature method
- 2020Imperfection-Insensitive Continuous Tow-Sheared Cylinderscitations
- 2020A strain-displacement mixed formulation based on the modified couple stress theory for the flexural behaviour of laminated beams.citations
- 2020An efficient semi-analytical framework to tailor snap-through loads in bistable variable stiffness laminatescitations
- 2020Newton’s method for experimental path-following of nonlinear structures
- 2020Imperfection-Insensitive Continuous Tow Sheared Cylinder
- 2019Efficient 3D Stress Capture of Variable-Stiffness and Sandwich Beam Structurescitations
- 2019A strain-displacement variational formulation for laminated composite beams based on the modified couple stress theory
- 2019Happy Catastrophecitations
- 2019On the accuracy of localised 3D stress fields in tow-steered laminated composite structurescitations
- 2018A tailored nonlinear slat-cove filler for airframe noise reduction.
- 2018Generalised path-following for well-behaved nonlinear structurescitations
- 2018Design and testing of a passively adaptive inletcitations
- 2018Three-dimensional stress analysis for laminated composite and sandwich structurescitations
- 2018Extreme mechanics in laminated shellscitations
- 2018HCI meets Material Sciencecitations
- 2017Post-buckling analysis of variable-angle tow composite plates using Koiter's approach and the finite element methodcitations
- 2017Computationally efficient beam elements for accurate stresses in sandwich laminates and laminated composites with delaminationscitations
- 2017Investigation of failure initiation in curved composite laminates using a higher-order beam modelcitations
- 2017Adaptive air inlet for fluid flow control
- 2016Deleterious localised stress fieldscitations
- 2016Morphing structures for flow regulation
- 2016A computationally efficient 2D model for inherently equilibrated 3D stress predictions in heterogeneous laminated plates. Part Icitations
- 2016Adaptive Nonlinear Structures for Flow Regulation
- 2016Higher-order beam model for stress predictions in curved beams made from anisotropic materialscitations
- 2016A computationally efficient 2D model for inherently equilibrated 3D stress predictions in heterogeneous laminated plates. Part IIcitations
- 2016Mixed shell element for static and buckling analysis of variable angle tow composite platescitations
- 2016Koiter asymptotic analysis of Variable Angle Tow composite plates
- 2015Application of the Refined Zigzag Theory to the Modeling of Delaminations in Laminated Composites
- 2015Static inconsistencies in certain axiomatic higher-order shear deformation theories for beams, plates and shellscitations
- 2015A mixed-variational, higher-order zig-zag theory for highly heterogeneous layered structures
- 2015Mass Optimisation of Variable Angle Tow, Variable Thickness Panels with Static Failure and Buckling Constraintscitations
- 2015Full-field stress tailoring of composite laminates
- 2015On displacement-based and mixed-variational equivalent single layer theories for modelling highly heterogeneous laminated beamscitations
- 2014Buckling analysis of variable angle tow, variable thickness panels with transverse shear effectscitations
- 2014Post-buckling analysis of variable angle, variable thickness panels manufactured by Continuous Tow Shearing
- 2013Buckling analysis of variable angle tow, variable thickness panels with transverse shear effects
Places of action
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article
Three-dimensional stress analysis for laminated composite and sandwich structures
Abstract
<p>Accurate stress prediction in composite laminates is crucial for safe design under different loading conditions. Classical laminated theory, i.e. those based on the Euler-Bernoulli and Kirchhoff hypotheses, respectively for beams and plates/shells are inaccurate for relatively thick laminates as three-dimensional (3D) effects such as transverse shear and normal deformations are neglected. Therefore, 3D finite element models are often employed for accurate stress analysis. However, these models are computationally expensive when used for laminates with a large number of layers, in optimisation studies, or for non-linear analyses. To address this issue, a Unified Formulation approach is presented for the analysis of laminated, slender beam-like structures. To define the kinematic field over the beam's cross-section, a recently developed hierarchical set of expansion functions, based on Serendipity Lagrange expansions, are employed and adapted to the layer-wise approach. The present formulation, which has displacements as degrees of freedom, does not ensure continuous transverse stresses across layer interfaces. Thus, an extra post-processing step is required to capture these stresses accurately. The proposed model is benchmarked against a 3D closed-form solution, 3D finite elements, and results available in the literature by means of static analyses of highly heterogeneous, laminated composite and sandwich beams. A key advantage of the present model is its ability to predict accurate 3D stress fields efficiently, including boundary layer regions, i.e. towards clamped ends. As a result, global analyses (e.g. overall displacements, buckling, etc.) and local analyses (e.g. stress concentrations) are combined within a single, computationally efficient model. The performance of the proposed approach, in terms of computational cost and precision, is assessed. Significant computational efficiency gains over 3D finite elements are observed for similar levels of accuracy.</p>