| People | Locations | Statistics |
|---|---|---|
| Naji, M. |
| |
| Motta, Antonella |
| |
| Aletan, Dirar |
| |
| Mohamed, Tarek |
| |
| Ertürk, Emre |
| |
| Taccardi, Nicola |
| |
| Kononenko, Denys |
| |
| Petrov, R. H. | Madrid |
|
| Alshaaer, Mazen | Brussels |
|
| Bih, L. |
| |
| Casati, R. |
| |
| Muller, Hermance |
| |
| Kočí, Jan | Prague |
|
| Šuljagić, Marija |
| |
| Kalteremidou, Kalliopi-Artemi | Brussels |
|
| Azam, Siraj |
| |
| Ospanova, Alyiya |
| |
| Blanpain, Bart |
| |
| Ali, M. A. |
| |
| Popa, V. |
| |
| Rančić, M. |
| |
| Ollier, Nadège |
| |
| Azevedo, Nuno Monteiro |
| |
| Landes, Michael |
| |
| Rignanese, Gian-Marco |
|
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
Places of action
| Organizations | Location | People |
|---|
document
FLEXOP – Application of aeroelastic tailoring to a flying demonstrator wing
Abstract
This paper presents the application of aeroelastic tailoring in the design of flying demonstrator wings. The work is part of the Flutter Free Flight Envelope eXpansion (FLEXOP) project, funded under the Horizon 2020 framework. The project involves the design, manufacturing and flight-testing of a UAV toward two principle goals: i) to demonstrate the passive load alleviation potential through composite tailoring, ii) to validate methods and tools for flutter modelling and flutter control. The work presented here addresses the first of the above mentioned goals.<br/>The design of the primary load-carrying wing-box in this task is performed using a joint DLR – TU Delft optimization strategy. In total, two sets of wings are designed in order to demonstrate the potential benefits of aeroelastic tailoring – i) a reference wing wherein the laminates of the wing-box entities are restricted to balanced and symmetric laminates; ii) a tailored wing wherein the laminates are allowed to be unbalanced, hence enhancing the bending-torsion coupling essential for aeroelastic tailoring.<br/>The optimized design is then manufactured and extensively tested to validate and improve the simulation models corresponding to the wing design. Flight tests are scheduled to be performed in late 2018 to demonstrate the load alleviation capabilities attained through the applied aeroelastic tailoring.