Ultra Performance Wing

Información del proyecto

UP Wing

Identificador del acuerdo de subvención: 101101974

DOI

10.3030/101101974

Fecha de la firma de la CE 8 Diciembre 2022

Fecha de inicio 1 Enero 2023

Fecha de finalización 31 Diciembre 2026

Financiado con arreglo a

• Climate, Energy and Mobility

Coste total

€ 43 814 468,34

Aportación de la UE

€ 38 005 938,75

Coordinado por

AIRBUS OPERATIONS GMBH
Germany

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

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

Publicaciones

Conference proceedings (28)

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

Autores: Wolf R. Krüger, Sunpeth Cumnuantip, Matthias Schulze
Publicado en: 2024
Editor: 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)

Autores: V.J.E. Aalbers, H.S. Timmermans, P. Blom
Publicado en: International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2024, 2024
Editor: TUD / NLR

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

Autores: Boulant, Thibault; Valla, Matthieu; Mariscal, Jean-François; Rouanet, Nicolas; Michel, David Tomline
Publicado en: SPIE Remote Sensing, 2023, 2023, ISSN 0277-786X
Editor: SPIE
DOI: 10.1117/12.2680187

Development of a vibration-based deicing system for aircraft wings

Autores: Michael Matthias, Denis Becker, Thorsten Koch, Chris Davies, Salvatore Ameduri
Publicado en: Active and Passive Smart Structures and Integrated Systems XIX, 2025
Editor: SPIE
DOI: 10.1117/12.3050817.SHORT

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

Autores: S. De Boer/R. De Breuker/J. Sodja
Publicado en: 2024
Editor: IFASD (TUD/NLR)

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

Autores: L. Martins-Pacheco, Ö. Petersson, A. C. Marta, F. Volle
Publicado en: Proceedings of the DLRK 2024 - Deutschen Luft- und Raumfahrtkongress, 2024
Editor: DLR

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

Autores: Keerthana Chandrasekar Jeyanthi (DLR), Johannes Löwe(DLR), Matthias Lühmann(Airbus), Tobias Knopp(DLR), Andreas Krumbein(DLR)
Publicado en: DGLR STAB-Symposium 2024, 2024
Editor: DLR

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

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

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

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

0137P - Entwicklung eines schwingungsbasierten Enteisungsverfahren für Flugzeugflügel

Autores: Denis Becker, Thorsten Koch, Michael Matthias, Chris Davies, Salvatore Ameduri
Publicado en: 2024
Editor: 4SMARTS Symposium 2024/Fraunhofer LBF

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

Autores: Luca Marino, Xuerui Wang, Jurij Sodja
Publicado en: 2024
Editor: TUD / NLR

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

Autores: 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
Publicado en: 2024
Editor: ICLAS

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

Autores: M. Méheut, D. Losada Costoso, E. Nguyen Van, O. Atinault
Publicado en: ECCOMAS 2024 - STS271 - Ultra-Performing Wing And Virtual Product Integration, 2024
Editor: ECCOMAS
DOI: 10.23967/ECCOMAS.2024.145

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

Autores: C. Julien, L. Coelho, L. Vertonghen, N. Fabbiane
Publicado en: Special Technology Sessions (STS) on Greening of Aviation, Transport and Renewable Energy, 2024
Editor: ONERA
DOI: 10.5281/zenodo.12568044

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

Autores: David Michel, Béatrice Augere, Thibault Bouland, Nicolas Cézard, Agnès Dolfi-Bouteyre, Anne Durecu, Didier Goular, François Gustave, Anasthase Liméry, Laurent Lombard, et al.
Publicado en: 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
Editor: 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

Autores: 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
Publicado en: 2023
Editor: DLR

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

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

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

Autores: 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
Publicado en: ICAS 2024 - 34th Congress of the International Council of the Aeronautical Sciences, 2024
Editor: ICAS

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

Autores: Luis M. M. Pacheco, Fabian Volle, Ogmundur Petersson and Andre C. Marta
Publicado en: 2025
Editor: AeroBest

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

Autores: Kilian M. Streitenberger, Johan M. Feldwisch
Publicado en: AIAA SCITECH 2025 Forum, 2025
Editor: 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

Autores: Fabian Volle
Publicado en: AIAA SCITECH 2025 Forum, 2025
Editor: 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

Autores: H.S. Timmermans, A. Jurisson, W.R. Krüger, F. Stalla, C. Kapteijn
Publicado en: International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2024, 2024
Editor: TUD / NLR

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

Autores: Jurij Soda, L. Marino, I. Kiat, A. Eberle
Publicado en: 2024
Editor: American Institute of Aeronautics and Astronautics Inc. (AIAA)
DOI: 10.2514/6.2024-2110

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

Autores: Anika Langebeck, Lewin Rathmann, Tim Radel
Publicado en: 2025
Editor: Hochschule Mittweidaer

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

Autores: Gilberto Ruiz Jimenez, Nicolas Roussouly, Francois Gallard, Anne Gazaix, Joel Brezillon, Kittinan Thanissaranon, Vida Bruck and Joaquim R.R.A. Martins
Publicado en: AeroBest 2025, 2025
Editor: AeroBest

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

Autores: David-Tomline Michel, Thibault Boulant, Laurent Bizet, Matthieu Valla, Olivier Gazzano, Yann Ferrec
Publicado en: CLRC 2024 - Coherent Laser Radar Conference, 2024
Editor: ILRC (DLR)

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

Autores: Eberle, Adrian; Stefes, Bruno; Reckzeh, Daniel
Publicado en: AIAA SCITECH 2024 Forum, 2024
Editor: 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

Autores: T. Trautmann, A. Schander, M. Vellekoop
Publicado en: Lectures, 2025
Editor: 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

Autores: I. Kiat
Publicado en: 2024
Editor: TU Delft

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

Autores: Zeinab Aboelmagd Ahmed Eltaher Ahmed
Publicado en: 2025
Editor: TU Berlin
DOI: 10.5281/zenodo.15012245

Peer reviewed articles (9)

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

Autores: Luca Marino, Ilias Kiat, Adrian Eberle, Jurij Sodja
Publicado en: Journal of Aircraft, 2025, ISSN 0021-8669
Editor: 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

Autores: Christian Musso, Thibault Boulant, Matthieu Valla, Sidonie Lefebvre, David T. Michel
Publicado en: AIAA Journal, 2025, ISSN 0001-1452
Editor: 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

Autores: E. Kappel
Publicado en: Composites Part C: Open Access, Edición Volume 14, July 2024, 100460, 2024, ISSN 2666-6820
Editor: Elsevier B.V.
DOI: 10.1016/j.jcomc.2024.100460

0078 - Laser cleaning of insect residue without surface alteration

Autores: Tim Radel, Lewin Rathmann
Publicado en: PhotonicsViews: Volume 21, Edición 5, Edición Volume 21, Edición 5, 2024, ISSN 2626-1308
Editor: Wiley-VCH GmbH (Weinheim, Germany)
DOI: 10.1002/phvs.202400025

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

Autores: Erik Kappel
Publicado en: Composites and Advanced Materials (SAGE Journals), Edición Volume 33, January-December 2024, 2024, ISSN 2634-9833
Editor: SAGE Publications Ltd
DOI: 10.1177/26349833241237244

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

Autores: Xuerui Wang, Feiran Zhao, Andres Jurisson, Florian D¨orfler, Roy S. Smith
Publicado en: IEEE Transactions on Aerospace and Electronic Systems, 2025, ISSN 0018-9251
Editor: 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

Autores: L. Rathmann, T. Radel
Publicado en: Lasers in Manufacturing and Materials Processing, 2025, ISSN 2196-7229
Editor: 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

Autores: Kappel, Erik
Publicado en: Journal of Composites Science, Vol 8, Iss 2, p 77 (2024), 2024, ISSN 2504-477X
Editor: 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

Autores: Jonathan Pouillaude, Pierre Pichon, Xavier Delen, Philippe Roy, Baptiste Leconte, Patrick Georges, Laurent Lombard
Publicado en: Optics Letters, Edición 50, 2025, ISSN 0146-9592
Editor: 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)

Autores: Erik Kappel, Yannick Boose, Robert Prussak, Jens Kosmann
Publicado en: 2023
Editor: DLR
DOI: 10.57965/rgsk-sa64

Other (1)

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

Autores: Erik Kappel, Stephen W. Tsai
Publicado en: 2024
Editor: DLR
DOI: 10.57965/g2cb-8t21