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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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Sodja, Jurij
Delft University of Technology
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (8/8 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
- 2021Development and testing of an active trailing edge morphing demonstrator for a rotary wingcitations
- 2020Ground Testing of the FLEXOP Demonstrator Aircraftcitations
- 2018FLEXOP – Application of aeroelastic tailoring to a flying demonstrator wing
- 2015Development and Testing of an Unconventional Morphing Wing Concept with Variable Chord and Camber
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document
Optimization Framework of a Ram Air Inlet Composite Morphing Flap
Abstract
The ram air inlets flaps are used in some aircraft to modulate the amount of ram<br/>air cooling the Environmental Control System. The current flap design features two metallic plates connected with a hinge. The present work studies an alternative design that replaces the metallic plates with a single composite laminate with morphing capabilities. An optimization framework is proposed to define the thickness distribution of the laminate taking into account the desired operational shapes, manufacturing guidelines and maximum allowable strains. This framework combines linear and nonlinear simulations to account for the large deflections while limiting the computational cost of the optimization. The results of the optimization framework are discussed at the end of the paper and next steps are formulated.