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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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Geijselaers, Hubert
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (31/31 displayed)
- 2023Computing Sheet Rolling Instabilities with a Shell Finite Element Model
- 2022Discontinuous Galerkin FEM with Hot Element Addition for the Thermal Simulation of Additive Manufacturing
- 2021Efficient thermal simulation of large-scale metal additive manufacturing using hot element additioncitations
- 2021Efficient analysis of dense fiber reinforcement using a reduced embedded formulationcitations
- 2020Optimization of the Interacting StiffenedSkins and Ribs Made of Composite Materialscitations
- 2020A New in-Plane Bending Test to Determine Flow Curves for Materials with Low Uniform Elongationcitations
- 2019Experimental investigation of pinching phenomena in cold rolling of thin steel sheetscitations
- 20191D squeeze flow analysis of chopped long fibre thermoplastic composite
- 2018A level-set-based strategy for thickness optimization of blended composite structurescitations
- 2018Deformation mechanism in compression molding of discontinuous thermoplastic composites
- 2017Effect of flake distribution in mold on the flow during compression molding of unidirectional long fiber thermoplastic flakes
- 2016Interpolation of final geometry and result fields in process parameter spacecitations
- 2016The softened heat-affected zone in resistance spot welded tailor hardened boron steel: a material model for crash simulation
- 2016Plasticity and fracture modeling of the heat-affected zone in resistance spot welded tailor hardened boron steelcitations
- 2016Parameter Study for Friction Surface Cladding of AA1050 on AA2024-T351
- 2015Friction Surface Cladding of AA1050 on AA2024-T351; influence of clad layer thickness and tool rotation rate
- 2015Thermal and Flow Analysis of Friction Surface Cladding with Varying Clad Layer Thickness
- 2015Single scan vector prediction in selective laser meltingcitations
- 2015Cyclic shear behavior of austenitic stainless steel sheet
- 2015Large strain cyclic behavior of metastable austenic stainless steelcitations
- 2015Friction surface claddingcitations
- 2015Influence of ring growth rate on damage development in hot ring rollingcitations
- 2014Influence of feed rate on damage development in hot ring rollingcitations
- 2013Modeling of the Austenite-Martensite Transformation in Stainless and TRIP Steelscitations
- 2013Strain direction dependency of martensitic transformation in austenitic stainless steels: The effect of gamma-texturecitations
- 2013Cladding of Advanced Al Alloys Employing Friction Stir Weldingcitations
- 2013Multi-Stage FE Simulation of Hot Ring Rollingcitations
- 2012Free Surface Modeling of Contacting Solid Metal Flows Employing the ALE formulationcitations
- 2011Comparison of ALE finite element method and adaptive smoothed finite element method for the numerical simulation of friction stir welding
- 2007Numerical forming simulations and optimisation in advanced materials
- 2000Improvements in FE-analysis of real-life sheet metal forming
Places of action
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article
A level-set-based strategy for thickness optimization of blended composite structures
Abstract
<p>An approach is presented for the thickness optimization of stiffened composite skins, which guarantees the continuity (blending) of plies over all individual panels. To fulfill design guidelines with respect to symmetry, covering ply, disorientation, percentage rule, balance, and contiguity of the layup, first a stacking sequence table is generated. Next, a level-set gradient-based method is introduced for the global optimization of the location of ply drops. The method aims at turning the discrete optimization associated with the integer number of plies into a continuous problem. It gives the optimum thickness distribution over the structure in relation to a specific stacking sequence table. The developed method is verified by application to the well-known 18-panel Horseshoe Problem. Subsequently, the proposed method is applied to the optimization of a composite stiffened skin of a wing torsion box. The problem objective is mass minimization and the constraint is local buckling.</p>