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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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Breuker, Roeland De
Delft University of Technology
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (22/22 displayed)
- 2024Aeroelastic Tailoring of a Strut-Braced Wing for a Medium Range Aircraftcitations
- 2023Optimization Framework of a Ram Air Inlet Composite Morphing Flapcitations
- 2022Application of Aeroelastic Tailoring for Load Alleviation on a Flying Demonstrator Wing †citations
- 2022Assessment of an Increased-Fidelity Aeroelastic Experiment for Free Flying Wing Response to Gust Excitation
- 2022Aeroelastic Wing Demonstrator with a Distributed and Decentralized Control Architecturecitations
- 2022An aeroelastic optimisation framework for manufacturable variable stiffness composite wings including critical gust loadscitations
- 2021Development and testing of an active trailing edge morphing demonstrator for a rotary wingcitations
- 2021Skin Panel Optimization of the Common Research Model Wing using Sandwich Compositescitations
- 2021Aeroelastic optimisation of manufacturable tow-steered composite wings with cruise shape constraint and gust loadscitations
- 2021Developing the Model Reduction Framework in High Frame Rate Visual Tracking Environment
- 2020Static and dynamic aeroelastic tailoring with composite blending and manoeuvre load alleviationcitations
- 2020Ground Testing of the FLEXOP Demonstrator Aircraftcitations
- 2019Aeroelastic optimization of composite wings including fatigue loading requirementscitations
- 2018FLEXOP – Application of aeroelastic tailoring to a flying demonstrator wing
- 2018Aeroelastic optimization of composite wings subjected to fatigue loadscitations
- 2017Aeroelastic Design of Blended Composite Structures Using Lamination Parameterscitations
- 2017Aeroelastic tailoring for static and dynamic loads with blending constraints
- 2016Aeroelastic Optimization of Variable Stiffness Composite Wing with Blending Constraintscitations
- 2016A Conceptual Development of a Shape Memory Alloy Actuated Variable Camber Morphing Wing
- 2016Derivation and application of blending constraints in lamination parameter space for composite optimisationcitations
- 2015Special Issue
- 2015Development and Testing of an Unconventional Morphing Wing Concept with Variable Chord and Camber
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article
Derivation and application of blending constraints in lamination parameter space for composite optimisation
Abstract
The present paper proposes a set of blending constraints expressed in lamination parameter space, applicable during the continuous optimisation of composite structures. Thicknesses and ply orientations of large composite structures are often locally optimised in response to unequal spatial load distribution. During this process, ensuring structural continuity is essential in order to achieve designs ready to be manufactured. Single step stacking sequence optimisations relying on evolutionary algorithms to enforce continuity, through the application of blending rules, are prone to the curse of dimensionality. By contrast, multi-step optimisation strategies including a continuous sub-step can optimise composite structures with reasonable computational effort. However, the discrepancies between continuous and discrete optimisation step result in performance loss during stacking sequence retrieval. By deriving and applying blending constraints during the continuous optimisation, this paper aim is to reduce the performance loss observed between optimisation levels. The first part of this paper is dedicated to the derivation of blending constraints. The proposed constraints are then successfully applied to a benchmark blending problem in the second part of this paper. Numerical results demonstrate the achievement of near-optimal easy-to-blend continuous designs in a matter of seconds. Keywords: Composite materials, Blending, Lamination parameters, Optimisation, Variable