NEXTAIR - multi-disciplinary digital - enablers for NEXT-generation AIRcraft design and operations | NEXTAIR | Project | Results | HORIZON | CORDIS

Resultado final

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.

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.

Publicaciones

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

Autores: Cyril Dosne; Raphaël Barrier, Sébastien Bourasseau, Marco Carini, Rocco Moretti and Jacques Peter.
Publicado en: Eccomas Proceedia EUROGEN (2023), Edición 15, 2023
Editor: ECCOMAS
DOI: 10.7712/140123.10197.18932

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

Autores: Quentin Bennehard, Jacques Peter, and Marco Carini
Publicado en: Eccomas Proceedia EUROGEN (2023), Edición 15, 2023
Editor: ECCOMAS
DOI: 10.7712/140123.10196.18920

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

Autores: Henriques-Gil, Javier and Mejia Parra, Daniel and Simoes, Bruno
Publicado en: Proceedings of the 28th International ACM Conference on 3D Web Technology, Edición Web3D '23, 2023, ISBN 9798400703249
Editor: Association for Computing Machinery
DOI: 10.1145/3611314.3615906

"""High-Fidelity Aerodynamic Shape and Multi-Disciplinary Optimisation in Early Aircraft Design Phase: a Capability Perspective with Applications"""

Autores: Joël Brezillon
Publicado en: Eurogen 2023, Edición """15th International Conference on Evolutionary and Deterministic Methods for Design, Optimization and Control""", 2023

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

Autores: Cyril Dosne, Raphaël Barrier, Sébastien Bourasseau, Marco Carini, Rocco Moretti and Jacques Peter
Publicado en: AIAA, Edición AIAA 2024-2640, 2024
DOI: 10.2514/6.2024-2640

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

Autores: Carta, M., Ghisu, T., Shahpar, S.
Publicado en: Int. J. Turbomach. Propuls. Power, Edición 8 (3), 2023, ISSN 2504-186X
Editor: MDPI
DOI: 10.3390/ijtpp8030024

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

Resultado final

Publicaciones

Compartir esta página

Descargar