Ultra Performance Wing

Informations projet

UP Wing

N° de convention de subvention: 101101974

DOI

10.3030/101101974

Date de signature de la CE 8 Decembre 2022

Date de début 1 Janvier 2023

Date de fin 31 Decembre 2026

Financé au titre de

• Climate, Energy and Mobility

Coût total

€ 43 814 468,34

Contribution de l’UE

€ 38 005 938,75

Coordonné par

AIRBUS OPERATIONS GMBH
Germany

CORDIS fournit des liens vers les livrables publics et les publications des projets HORIZON.

Les liens vers les livrables et les publications des projets du 7e PC, ainsi que les liens vers certains types de résultats spécifiques tels que les jeux de données et les logiciels, sont récupérés dynamiquement sur OpenAIRE .

Livrables

Documents, reports (4)

D5.1-5: Plan for Communication & Dissemination of Results v3

Third version of the document that defines the methods and targets of dissemination and communication activities; management and tracking of these activities will be done in the DiPP tool; the outcomes will form part of periodic reporting

D5.4-1: Data Management Plan v1

First version of the document that defines the standards and guide the consortium with regard to data storage access and management including Open Access principles

D5.1-3: Plan for Communication & Dissemination of Results v1

Document that defines the methods and targets of dissemination and communication activities management and tracking of these activities will be done in the DiPP tool the outcomes will form part of periodic reporting

D5.4-3: Data Management Plan v3

Prepare and release the updated version of the data management plan

Publications

Conference proceedings (28)

0111P - Assessment of the aeroelastic stability of high aspect ratio wing aircraft during the preliminary design

Auteurs: Wolf R. Krüger, Sunpeth Cumnuantip, Matthias Schulze
Publié dans: 2024
Éditeur: TUD / NLR

0068P - FLIGHT SHAPE DETERMINATION OF THE HIGHLY FLEXIBLE UP WING WIND TUNNEL MODEL USING HIGH AND LOW FIDELITY AERODYNAMIC METHODS IN CONJUNCTION WITH NONLINEAR STRUCTURAL METHODS (Paper)

Auteurs: V.J.E. Aalbers, H.S. Timmermans, P. Blom
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2024, 2024
Éditeur: TUD / NLR

0005p-Robust molecular wind lidar with Quadri Mach-Zehnder interferometer and UV fiber laser for calibration/validation and future generation of Aeolus

Auteurs: Boulant, Thibault; Valla, Matthieu; Mariscal, Jean-François; Rouanet, Nicolas; Michel, David Tomline
Publié dans: SPIE Remote Sensing, 2023, 2023, ISSN 0277-786X
Éditeur: SPIE
DOI: 10.1117/12.2680187

Development of a vibration-based deicing system for aircraft wings

Auteurs: Michael Matthias, Denis Becker, Thorsten Koch, Chris Davies, Salvatore Ameduri
Publié dans: Active and Passive Smart Structures and Integrated Systems XIX, 2025
Éditeur: SPIE
DOI: 10.1117/12.3050817.SHORT

0020P - Continuous Parametrisation of Wing Movable Layout for Design Optimisation

Auteurs: S. De Boer/R. De Breuker/J. Sodja
Publié dans: 2024
Éditeur: IFASD (TUD/NLR)

0133P - A high-fidelity MDO framework applied to the design of a high aspect-ratio transport wing (Paper)

Auteurs: L. Martins-Pacheco, Ö. Petersson, A. C. Marta, F. Volle
Publié dans: Proceedings of the DLRK 2024 - Deutschen Luft- und Raumfahrtkongress, 2024
Éditeur: DLR

0127P - Preliminary verification, validation and stabilization of Reynolds stress models using the CFD Software by ONERA, DLR, Airbus (CODA)

Auteurs: Keerthana Chandrasekar Jeyanthi (DLR), Johannes Löwe(DLR), Matthias Lühmann(Airbus), Tobias Knopp(DLR), Andreas Krumbein(DLR)
Publié dans: DGLR STAB-Symposium 2024, 2024
Éditeur: DLR

0065p - Modelling of an ice protection system based on icephobic and piezoelectric technologies, for WT demonstration

Auteurs: Salvatore Ameduri; Rehfeld, Nadine; Luigi Mangiacrapa; Antonio Concilio; Giuseppe Mingione; Filomena Piscitelli
Publié dans: GMM-Fachbericht 110 ACTUATOR 2024 International Conference and Exhibition on New Actuator Systems and Applications, 2024, ISSN 978-3-8007-6391
Éditeur: VDE/VDI

Realization of Icing Wind Tunnel Demonstrators for the Characterization of a Hybrid Ice Protection System

Auteurs: Luigi Mangiacrapa, Filomena Piscitelli, Nadine Rehfeld, Francesco Amoroso, Giuseppe Mingione, Salvatore Ameduri
Publié dans: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-3525

0137P - Entwicklung eines schwingungsbasierten Enteisungsverfahren für Flugzeugflügel

Auteurs: Denis Becker, Thorsten Koch, Michael Matthias, Chris Davies, Salvatore Ameduri
Publié dans: 2024
Éditeur: 4SMARTS Symposium 2024/Fraunhofer LBF

0109P - Nonlinear analysis of combined rate and acceleration limits effect on actuator response

Auteurs: Luca Marino, Xuerui Wang, Jurij Sodja
Publié dans: 2024
Éditeur: TUD / NLR

0096P - Aeronautics lidar revisited – Towards lidar-based gust and turbulence measurement for aircraft load alleviation control

Auteurs: P. Vrancken; L. Bizet; Th. Boulant; P. Cutipa; N. Fezans; M. Faccioni; H. de Haan; H. Jentink; D. Kiehn; O. Kliebisch; Ph. Linsmayer; L. Lombard; R. Lorbeer; T. Michel; P. Pichon; J. Pouillaude; A. S. Pankan; J. Thurn; R. Tump; M. Valla
Publié dans: 2024
Éditeur: ICLAS

0098P - Aerodynamic design of a high aspect ratio strut-braced wing

Auteurs: M. Méheut, D. Losada Costoso, E. Nguyen Van, O. Atinault
Publié dans: ECCOMAS 2024 - STS271 - Ultra-Performing Wing And Virtual Product Integration, 2024
Éditeur: ECCOMAS
DOI: 10.23967/ECCOMAS.2024.145

0099d - Aeroelastic design of a Strut-braced Wing for LH2 powered Aircrafts

Auteurs: C. Julien, L. Coelho, L. Vertonghen, N. Fabbiane
Publié dans: Special Technology Sessions (STS) on Greening of Aviation, Transport and Renewable Energy, 2024
Éditeur: ONERA
DOI: 10.5281/zenodo.12568044

0006p - Heterodyne and direct detection wind lidar developed at ONERA

Auteurs: David Michel, Béatrice Augere, Thibault Bouland, Nicolas Cézard, Agnès Dolfi-Bouteyre, Anne Durecu, Didier Goular, François Gustave, Anasthase Liméry, Laurent Lombard, et al.
Publié dans: LIDAR 2023: 3rd international workshop on space-based lidar remote sensing techniques and emerging technologies, Jun 2023, Milos Island, Greece, Greece. pp.227-238, 2024
Éditeur: Springer Nature Switzerland AG
DOI: 10.1007/978-3-031-53618-2_20

0038 - How Future Aircraft Shall Lose Weight Thanks to Doppler Wind Lidar Technology - the UP Wing Project of the EC Clean Aviation Joint Undertaking

Auteurs: Vrancken, Patrick; Linsmayer, Philippe; Cutipa, Paula; Fezans, Nicolas; Kiehn, Daniel; Kliebisch, Oliver; Thurn, Johann; Lorbeer, Raoul-Amadeus; Damm, Matthias; de Haan, Harald; Tump, Robert; Jentink, H.W.; Lombard, Laurent; Michel, David To
Publié dans: 2023
Éditeur: DLR

0069 - Materials for erosion protection – Self-healing properties for leading edge coatings

Auteurs: """Nadine Rehfeld, Claus Schreiner, Björn Speckmann, Volkmar Stenzel (Fraunhofer IFAM) Jesper Dal Hasager (R&D Test Systems) Silke Gruenke (Airbus Operations GmbH)"""
Publié dans: 2024
Éditeur: Fraunhofer IFAM
DOI: 10.5281/zenodo.10679707

0070P - Strut-Braced Dry Wing Concept for Hydrogen-Powered Aircraft

Auteurs: M. Meheut, D. Losada Costoso, F. Moens, O. Atinault, C. Julien, L. Vertonghen, L. Coelho, V. Priasso, A. Lannoo, S. Defoort, E. NGuyen Van, C. David, D. Glenis, J. Sodja, S. de Boer, J. Schwingel & D. Eisenhut
Publié dans: ICAS 2024 - 34th Congress of the International Council of the Aeronautical Sciences, 2024
Éditeur: ICAS

0175P - HIGH ASPECT-RATIO COMPOSITE WING AEROSTRUCTURAL OPTIMISATION OF A SHORT-MEDIUM RANGE AIRCRAFT

Auteurs: Luis M. M. Pacheco, Fabian Volle, Ogmundur Petersson and Andre C. Marta
Publié dans: 2025
Éditeur: AeroBest

CFD-Based Aeroelastic Maneuver and Gust Loads Analysis for a High Aspect Ratio Wing Configuration

Auteurs: Kilian M. Streitenberger, Johan M. Feldwisch
Publié dans: AIAA SCITECH 2025 Forum, 2025
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-1663

Aero-Structural Optimization of the AIAA MDO Benchmark Model With TAU and Lagrange

Auteurs: Fabian Volle
Publié dans: AIAA SCITECH 2025 Forum, 2025
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-2815

0067P - DESIGN OF A HIGH ASPECT RATIO WINDTUNNEL MODEL FOR TRANSONIC GUST LOAD ALLEVIATION

Auteurs: H.S. Timmermans, A. Jurisson, W.R. Krüger, F. Stalla, C. Kapteijn
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2024, 2024
Éditeur: TUD / NLR

0010p - Parametric study of a switchable vortex generator for load alleviation in transonic conditions

Auteurs: Jurij Soda, L. Marino, I. Kiat, A. Eberle
Publié dans: 2024
Éditeur: American Institute of Aeronautics and Astronautics Inc. (AIAA)
DOI: 10.2514/6.2024-2110

0162P - Stoßwellenbasierte Oberflächenreinigung von Insektenrückständen mittels CO2 Laser (Paper)

Auteurs: Anika Langebeck, Lewin Rathmann, Tim Radel
Publié dans: 2025
Éditeur: Hochschule Mittweidaer

0176P - A COMPARISON OF MDO BI-LEVEL FORMULATION VARIANTS WITH MDF ON A HIGH-FIDELITY AEROELASTIC WING TEST CASE

Auteurs: Gilberto Ruiz Jimenez, Nicolas Roussouly, Francois Gallard, Anne Gazaix, Joel Brezillon, Kittinan Thanissaranon, Vida Bruck and Joaquim R.R.A. Martins
Publié dans: AeroBest 2025, 2025
Éditeur: AeroBest

0092P - Direct-detection airborne UV wind lidar including Quadri Mach-Zehnder interferometer for 3D wind reconstruction

Auteurs: David-Tomline Michel, Thibault Boulant, Laurent Bizet, Matthieu Valla, Olivier Gazzano, Yann Ferrec
Publié dans: CLRC 2024 - Coherent Laser Radar Conference, 2024
Éditeur: ILRC (DLR)

0029PClean Aviation Ultra-Performance Wing (UP-Wing)

Auteurs: Eberle, Adrian; Stefes, Bruno; Reckzeh, Daniel
Publié dans: AIAA SCITECH 2024 Forum, 2024
Éditeur: American Institute of Aeronautics and Astronautics Inc. (AIAA)
DOI: 10.2514/6.2024-2109

C1.1 - Comparison of Polyimide to Silicon Nitride Membranes for Robust Thermal Flow Sensors

Auteurs: T. Trautmann, A. Schander, M. Vellekoop
Publié dans: Lectures, 2025
Éditeur: AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany
DOI: 10.5162/SMSI2025/C1.1

Thesis and dissertations (2)

0024 - Parametric investigation of mini-tab for load alleviation

Auteurs: I. Kiat
Publié dans: 2024
Éditeur: TU Delft

0117 - Modelling and implementation of a real-time flexible aircraft simulation environment with animation of flight path, attitude and airframe deformation (Thesis)

Auteurs: Zeinab Aboelmagd Ahmed Eltaher Ahmed
Publié dans: 2025
Éditeur: TU Berlin
DOI: 10.5281/zenodo.15012245

Peer reviewed articles (9)

Parametric Study of a Switchable Vortex Generator for Load Alleviation in Transonic Conditions

Auteurs: Luca Marino, Ilias Kiat, Adrian Eberle, Jurij Sodja
Publié dans: Journal of Aircraft, 2025, ISSN 0021-8669
Éditeur: American Institute of Aeronautics and Astronautics (AIAA)
DOI: 10.2514/1.C037939

Estimation of the Parameters of a Three-Dimensional Gust Model with a Wind Lidar

Auteurs: Christian Musso, Thibault Boulant, Matthieu Valla, Sidonie Lefebvre, David T. Michel
Publié dans: AIAA Journal, 2025, ISSN 0001-1452
Éditeur: American Institute of Aeronautics and Astronautics (AIAA)
DOI: 10.2514/1.J064209

0072 - Omni first-ply-failure envelopes - A conservative approach to assess laminate failure

Auteurs: E. Kappel
Publié dans: Composites Part C: Open Access, Numéro Volume 14, July 2024, 100460, 2024, ISSN 2666-6820
Éditeur: Elsevier B.V.
DOI: 10.1016/j.jcomc.2024.100460

0078 - Laser cleaning of insect residue without surface alteration

Auteurs: Tim Radel, Lewin Rathmann
Publié dans: PhotonicsViews: Volume 21, Numéro 5, Numéro Volume 21, Numéro 5, 2024, ISSN 2626-1308
Éditeur: Wiley-VCH GmbH (Weinheim, Germany)
DOI: 10.1002/phvs.202400025

0042 - On stacking-sequence independent bending properties of Double-Double laminates – A short communication

Auteurs: Erik Kappel
Publié dans: Composites and Advanced Materials (SAGE Journals), Numéro Volume 33, January-December 2024, 2024, ISSN 2634-9833
Éditeur: SAGE Publications Ltd
DOI: 10.1177/26349833241237244

Unified Aeroelastic Flutter and Loads Control via Data-Enabled Policy Optimization

Auteurs: Xuerui Wang, Feiran Zhao, Andres Jurisson, Florian D¨orfler, Roy S. Smith
Publié dans: IEEE Transactions on Aerospace and Electronic Systems, 2025, ISSN 0018-9251
Éditeur: Institute of Electrical and Electronics Engineers (IEEE)
DOI: 10.1109/TAES.2025.3566351

Laser Cleaning of Insect Residue with a TEA-CO2 -Laser in Shockwave Regime

Auteurs: L. Rathmann, T. Radel
Publié dans: Lasers in Manufacturing and Materials Processing, 2025, ISSN 2196-7229
Éditeur: Springer Science and Business Media LLC
DOI: 10.1007/s40516-025-00278-9

0049 - On the Double-Double laminate buckling optimum for the 18-panel ’horse-shoe’ reference case

Auteurs: Kappel, Erik
Publié dans: Journal of Composites Science, Vol 8, Iss 2, p 77 (2024), 2024, ISSN 2504-477X
Éditeur: Elsevier
DOI: 10.3390/jcs8020077

Development of an all-fiber spliced laser system using stimulated Brillouin scattering mitigation techniques and achieving 50 ns, 10 kW peak power for lidar applications

Auteurs: Jonathan Pouillaude, Pierre Pichon, Xavier Delen, Philippe Roy, Baptiste Leconte, Patrick Georges, Laurent Lombard
Publié dans: Optics Letters, Numéro 50, 2025, ISSN 0146-9592
Éditeur: Optica Publishing Group
DOI: 10.1364/OL.553536

Monographic books (1)

0059 - On measuring laminate strains of a bent tapered Double-Double panel – Comparing strain data from an FE calculation, a high-resolution 3D camera system (ARAMIS) and a fiber-optical sensor system (FOSS)

Auteurs: Erik Kappel, Yannick Boose, Robert Prussak, Jens Kosmann
Publié dans: 2023
Éditeur: DLR
DOI: 10.57965/rgsk-sa64

Other (1)

0112 - Double-Double laminates - A review on the status quo in spring 2024

Auteurs: Erik Kappel, Stephen W. Tsai
Publié dans: 2024
Éditeur: DLR
DOI: 10.57965/g2cb-8t21