NEXTAIR - multi-disciplinary digital - enablers for NEXT-generation AIRcraft design and operations

Projektinformationen

NEXTAIR

ID Finanzhilfevereinbarung: 101056732

DOI 10.3030/101056732

EK-Unterschriftsdatum 11 Mai 2022

Startdatum 1 September 2022

Enddatum 31 August 2025

Finanziert unter

• Climate, Energy and Mobility

Gesamtkosten € 4 720 526,75

EU-Beitrag € 4 720 525,00

Koordiniert durch

OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Frankreich

CORDIS bietet Links zu öffentlichen Ergebnissen und Veröffentlichungen von HORIZONT-Projekten.

Links zu Ergebnissen und Veröffentlichungen von RP7-Projekten sowie Links zu einigen Typen spezifischer Ergebnisse wie Datensätzen und Software werden dynamisch von OpenAIRE abgerufen.

Leistungen

Dokumente, Berichte (2)

Assessment of transition models & their adjoints

Development of the Adjoints to the Transition Models used in NEXTAIR. Presentation of results on the NLF wing, comparisons, assessement of the use of the adjoint to the transition model in terms of the accuracy of objective function gradients. Linked to task 1.2.

DENs to Speed-up MDOs

Report on the benefits from (b) linking the NEXTAIR s/w with EuroHPC programs, (b) using multi-level approaches in MDO, (c) mesh adaptation in laminar wing cases, (d) computing Pareto fronts by adjoint. Report on techniques to reduce the cost of unsteady adjoint. All with demonstration in NEXTAIR cases. Linked to task 1.3.

Demonstrationssysteme, Piloten, Prototypen (1)

Instant CFD demonstrator on NACA0012 design and ONERA M6 wing cases (publicly available)

Demonstrators of (i) a hybrid deep learning and multi-ridge framework that can predict entire RANS flow-field instanteously (ii) dimension reduction methods for flow-fields rooted in computational optimal transport and manifold optimisation; and (iii) lambda-DNN based approach for fluid flow-field and interactions. The outputs will directly feed into the robust design of a high bypass-ratio fan in WP4/WP5, along with the Digital Twin of the heat exchanger in task 6.3. The lambda-DNN approach will be deployed in WP3/4. Linked to methodologies devloped in task 2.1.

Websites, Patentanmeldungen, Videos etc. (1)

Communication kit (social media, website, flyer, video)

Creation and delivery of the complete visual identity materials to partners in order to ensure the transfer of a recognisable and coherent image of the project in all communication and dissemination activities. Linked to task 7.2.

Veröffentlichungen

Konferenzprotokolle (4)

AN ADJOINT BODY-FORCE APPROACH FOR FULLY-COUPLED AERO-PROPULSIVE OPTIMIZATIONS

Autoren: Cyril Dosne; Raphaël Barrier, Sébastien Bourasseau, Marco Carini, Rocco Moretti and Jacques Peter.
Veröffentlicht in: Eccomas Proceedia EUROGEN (2023), 2023
Herausgeber: ECCOMAS
DOI: 10.7712/140123.10197.18932

COMPARISON OF EFFICIENT UNCERTAINTY QUANTIFICATION TECHNIQUES ON A TRANSONIC AIRFOIL, USING RANS COMPUTATIONS AND ADJOINT METHOD

Autoren: Quentin Bennehard, Jacques Peter, and Marco Carini
Veröffentlicht in: Eccomas Proceedia EUROGEN (2023), Ausgabe 15, 2023
Herausgeber: ECCOMAS
DOI: 10.7712/140123.10196.18920

Enhancing Decision Making in MDO through Interactive Visual Analytics on the Web

Autoren: Henriques-Gil, Javier and Mejia Parra, Daniel and Simoes, Bruno
Veröffentlicht in: Proceedings of the 28th International ACM Conference on 3D Web Technology, Ausgabe Web3D '23, 2023, ISBN 9798400703249
Herausgeber: Association for Computing Machinery
DOI: 10.1145/3611314.3615906

A First Assessment of Adjoint Body-Force Modeling Capabilities for Fan Design

Autoren: Cyril Dosne, Raphaël Barrier, Sébastien Bourasseau, Marco Carini, Rocco Moretti and Jacques Peter
Veröffentlicht in: AIAA, Ausgabe AIAA 2024-2640, 2024
Herausgeber: AIAA 2024-2640
DOI: 10.2514/6.2024-2640

Fachlich begutachtete Artikel (2)

Radial Basis Function Surrogates for Uncertainty Quantification and Aerodynamic Shape Optimization under Uncertainties

Autoren: Marina G. Kontoua, Varvara G. Asoutia, Kyriakos C. Giannakogloua
Veröffentlicht in: Fluids, Ausgabe 8(11), 292, 2023, ISSN 2311-5521
Herausgeber: MDPI
DOI: 10.3390/fluids8110292

Heat Transfer Analysis of Damaged Shrouded High-Pressure Turbine Rotor Blades

Autoren: Carta, M., Ghisu, T., Shahpar, S.
Veröffentlicht in: Int. J. Turbomach. Propuls. Power, Ausgabe 8 (3), 2023, ISSN 2504-186X
Herausgeber: MDPI
DOI: 10.3390/ijtpp8030024