Periodic Reporting for period 1 - FALCON (Foreseeing the next generation of Aircraft: hybrid approach using Lattice-boltzmann, experiments and modelling to optimize fluid/struCture interactiONs)
Período documentado: 2024-01-01 hasta 2025-06-30
One of the main levers to decrease CO2 emissions is to reduce the airframe structural weight. This implies to provide even more flexible wings with large aspect ratio, slender fuselage and more flexible junctions between the main aircraft parts with higher relative displacements between them for which current prediction methods are insufficient.
As an answer, FALCON’s ambition is to enhance the design capabilities of the European industrial aircraft sector, focusing on fluid-structure interaction (FSI) phenomena to improve the aeroelastic performances of aircraft (unsteady loads), thus decreasing CO2 emissions. The enhanced FSI design capabilities will also benefit to specific noise emissions generated by flexible and mobile airframe structures when exposed to both low and high-speed fluid flows.
The website of the FALCON project can be seen at https://falconproject.eu/(se abrirá en una nueva ventana)
As several partners develop together the methods and setup of structure solvers, a coupling has been developed between MSC Nastran and ProLB (LaBS) and between ESPRESO and OpenLB. Specific methods and structure solvers are also being developed to tackle the complex conditions involving flexible structure in turbulence and compressible flows and high frequency vibrations. A monolithic approach for FSI has started based on full LBM approach for both fluid and structure and it is going well.
The flap-cove seal experiment has been designed and is ready to perform at DLR. Methodology, numerical simulations using LBM and a lot of different scenarios have been used to plan the best possible experiment.
A hybrid database is ready to be populated by numerical and experimental data. Sensitivity solvers for high-fidelity models have just started to be developed using automatic differenciation. The development of surrogate models are emergent and very encouraging to be used for FSI.
HPC platforms are now secured for each partner in the project. KAROLINA is one example. Work has been done on algorithm design, code porting and optimization in order to optimize the performance of the codes. Visualization of CFD results has been started and the first tests are very encouraging for the future of FALCON.
As a potential scientific impact, FALCON will produce a reference FSI benchmark database, open to the scientific community and covering the whole range of typical fluid/structure interaction phenomena in aeronautics. The project will also develop cost-efficient two-way fluid-structure interaction computations including acoustics and structural dynamics, expected to generate only a limited percentage of overhead compared to fixed geometry calculations, which will be highly beneficial for the aeronautics industry.
From an environmental point of view, the project will improve the durability of airframe structures (seals and flexible wings) and lead to an increase of the replacement cycle of seals by 20%. This will constitute valuable outcomes for industrials towards an industrialization by 2040-2050.
On a long-term perspective, FALCON will contribute to several Key Strategic Orientation (KSO) set by Horizon Europe. It will contribute to a more sustainable air transport by targeting a reduction of aircraft structural weight (greener transport), a reduction of the aerodynamical noise (quieter transport) and the replacement cycle of airframe structures experiencing vibrations and deformations (more sustainable transport). Additionally, the project will provide an efficient and state-of-the-art digital technology to reinforce the leadership of European aircraft industry.