Ultra Performance Wing

Informazioni relative al progetto

UP Wing

ID dell’accordo di sovvenzione: 101101974

DOI

10.3030/101101974

Data della firma CE 8 Dicembre 2022

Data di avvio 1 Gennaio 2023

Data di completamento 31 Dicembre 2026

Finanziato da

• Climate, Energy and Mobility

Costo totale

€ 43 814 468,34

Contributo UE

€ 38 005 938,75

Coordinato da

AIRBUS OPERATIONS GMBH
Germany

CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.

I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .

Risultati finali

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

Pubblicazioni

Conference proceedings (28)

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

Autori: Wolf R. Krüger, Sunpeth Cumnuantip, Matthias Schulze
Pubblicato in: 2024
Editore: 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)

Autori: V.J.E. Aalbers, H.S. Timmermans, P. Blom
Pubblicato in: International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2024, 2024
Editore: TUD / NLR

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

Autori: Boulant, Thibault; Valla, Matthieu; Mariscal, Jean-François; Rouanet, Nicolas; Michel, David Tomline
Pubblicato in: SPIE Remote Sensing, 2023, 2023, ISSN 0277-786X
Editore: SPIE
DOI: 10.1117/12.2680187

Development of a vibration-based deicing system for aircraft wings

Autori: Michael Matthias, Denis Becker, Thorsten Koch, Chris Davies, Salvatore Ameduri
Pubblicato in: Active and Passive Smart Structures and Integrated Systems XIX, 2025
Editore: SPIE
DOI: 10.1117/12.3050817.SHORT

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

Autori: S. De Boer/R. De Breuker/J. Sodja
Pubblicato in: 2024
Editore: IFASD (TUD/NLR)

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

Autori: L. Martins-Pacheco, Ö. Petersson, A. C. Marta, F. Volle
Pubblicato in: Proceedings of the DLRK 2024 - Deutschen Luft- und Raumfahrtkongress, 2024
Editore: DLR

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

Autori: Keerthana Chandrasekar Jeyanthi (DLR), Johannes Löwe(DLR), Matthias Lühmann(Airbus), Tobias Knopp(DLR), Andreas Krumbein(DLR)
Pubblicato in: DGLR STAB-Symposium 2024, 2024
Editore: DLR

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

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

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

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

0137P - Entwicklung eines schwingungsbasierten Enteisungsverfahren für Flugzeugflügel

Autori: Denis Becker, Thorsten Koch, Michael Matthias, Chris Davies, Salvatore Ameduri
Pubblicato in: 2024
Editore: 4SMARTS Symposium 2024/Fraunhofer LBF

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

Autori: Luca Marino, Xuerui Wang, Jurij Sodja
Pubblicato in: 2024
Editore: TUD / NLR

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

Autori: 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
Pubblicato in: 2024
Editore: ICLAS

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

Autori: M. Méheut, D. Losada Costoso, E. Nguyen Van, O. Atinault
Pubblicato in: ECCOMAS 2024 - STS271 - Ultra-Performing Wing And Virtual Product Integration, 2024
Editore: ECCOMAS
DOI: 10.23967/ECCOMAS.2024.145

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

Autori: C. Julien, L. Coelho, L. Vertonghen, N. Fabbiane
Pubblicato in: Special Technology Sessions (STS) on Greening of Aviation, Transport and Renewable Energy, 2024
Editore: ONERA
DOI: 10.5281/zenodo.12568044

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

Autori: David Michel, Béatrice Augere, Thibault Bouland, Nicolas Cézard, Agnès Dolfi-Bouteyre, Anne Durecu, Didier Goular, François Gustave, Anasthase Liméry, Laurent Lombard, et al.
Pubblicato in: 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
Editore: 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

Autori: 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
Pubblicato in: 2023
Editore: DLR

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

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

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

Autori: 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
Pubblicato in: ICAS 2024 - 34th Congress of the International Council of the Aeronautical Sciences, 2024
Editore: ICAS

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

Autori: Luis M. M. Pacheco, Fabian Volle, Ogmundur Petersson and Andre C. Marta
Pubblicato in: 2025
Editore: AeroBest

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

Autori: Kilian M. Streitenberger, Johan M. Feldwisch
Pubblicato in: AIAA SCITECH 2025 Forum, 2025
Editore: 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

Autori: Fabian Volle
Pubblicato in: AIAA SCITECH 2025 Forum, 2025
Editore: 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

Autori: H.S. Timmermans, A. Jurisson, W.R. Krüger, F. Stalla, C. Kapteijn
Pubblicato in: International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2024, 2024
Editore: TUD / NLR

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

Autori: Jurij Soda, L. Marino, I. Kiat, A. Eberle
Pubblicato in: 2024
Editore: American Institute of Aeronautics and Astronautics Inc. (AIAA)
DOI: 10.2514/6.2024-2110

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

Autori: Anika Langebeck, Lewin Rathmann, Tim Radel
Pubblicato in: 2025
Editore: Hochschule Mittweidaer

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

Autori: Gilberto Ruiz Jimenez, Nicolas Roussouly, Francois Gallard, Anne Gazaix, Joel Brezillon, Kittinan Thanissaranon, Vida Bruck and Joaquim R.R.A. Martins
Pubblicato in: AeroBest 2025, 2025
Editore: AeroBest

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

Autori: David-Tomline Michel, Thibault Boulant, Laurent Bizet, Matthieu Valla, Olivier Gazzano, Yann Ferrec
Pubblicato in: CLRC 2024 - Coherent Laser Radar Conference, 2024
Editore: ILRC (DLR)

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

Autori: Eberle, Adrian; Stefes, Bruno; Reckzeh, Daniel
Pubblicato in: AIAA SCITECH 2024 Forum, 2024
Editore: 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

Autori: T. Trautmann, A. Schander, M. Vellekoop
Pubblicato in: Lectures, 2025
Editore: 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

Autori: I. Kiat
Pubblicato in: 2024
Editore: TU Delft

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

Autori: Zeinab Aboelmagd Ahmed Eltaher Ahmed
Pubblicato in: 2025
Editore: TU Berlin
DOI: 10.5281/zenodo.15012245

Peer reviewed articles (9)

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

Autori: Luca Marino, Ilias Kiat, Adrian Eberle, Jurij Sodja
Pubblicato in: Journal of Aircraft, 2025, ISSN 0021-8669
Editore: 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

Autori: Christian Musso, Thibault Boulant, Matthieu Valla, Sidonie Lefebvre, David T. Michel
Pubblicato in: AIAA Journal, 2025, ISSN 0001-1452
Editore: 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

Autori: E. Kappel
Pubblicato in: Composites Part C: Open Access, Numero Volume 14, July 2024, 100460, 2024, ISSN 2666-6820
Editore: Elsevier B.V.
DOI: 10.1016/j.jcomc.2024.100460

0078 - Laser cleaning of insect residue without surface alteration

Autori: Tim Radel, Lewin Rathmann
Pubblicato in: PhotonicsViews: Volume 21, Numero 5, Numero Volume 21, Numero 5, 2024, ISSN 2626-1308
Editore: Wiley-VCH GmbH (Weinheim, Germany)
DOI: 10.1002/phvs.202400025

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

Autori: Erik Kappel
Pubblicato in: Composites and Advanced Materials (SAGE Journals), Numero Volume 33, January-December 2024, 2024, ISSN 2634-9833
Editore: SAGE Publications Ltd
DOI: 10.1177/26349833241237244

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

Autori: Xuerui Wang, Feiran Zhao, Andres Jurisson, Florian D¨orfler, Roy S. Smith
Pubblicato in: IEEE Transactions on Aerospace and Electronic Systems, 2025, ISSN 0018-9251
Editore: 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

Autori: L. Rathmann, T. Radel
Pubblicato in: Lasers in Manufacturing and Materials Processing, 2025, ISSN 2196-7229
Editore: 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

Autori: Kappel, Erik
Pubblicato in: Journal of Composites Science, Vol 8, Iss 2, p 77 (2024), 2024, ISSN 2504-477X
Editore: 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

Autori: Jonathan Pouillaude, Pierre Pichon, Xavier Delen, Philippe Roy, Baptiste Leconte, Patrick Georges, Laurent Lombard
Pubblicato in: Optics Letters, Numero 50, 2025, ISSN 0146-9592
Editore: 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)

Autori: Erik Kappel, Yannick Boose, Robert Prussak, Jens Kosmann
Pubblicato in: 2023
Editore: DLR
DOI: 10.57965/rgsk-sa64

Other (1)

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

Autori: Erik Kappel, Stephen W. Tsai
Pubblicato in: 2024
Editore: DLR
DOI: 10.57965/g2cb-8t21