Robust- and sustainable-by-design ultra-higH aspEct ratio wing and Airframe

Informations projet

RHEA

N° de convention de subvention: 883670

DOI

10.3030/883670

Projet clôturé

Date de signature de la CE 15 Avril 2020

Date de début 1 Juillet 2020

Date de fin 30 Novembre 2023

Financé au titre de

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Coût total

€ 1 323 981,27

Contribution de l’UE

€ 1 323 981,27

Coordonné par

TECHNISCHE UNIVERSITAET BRAUNSCHWEIG
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 (8)

Report on final assessment of SBW

Report on final assessment of SBW USTRATH SOTON ICL M41

Report on estimated environmental impact of SBW and associated implications with regulatory framework, technology road map

D61 Report on the environmental impact of SBW on CO2 emissions and noise and associated implications with regulatory framework assessment of the technological roadmap as needed to achieve higher TRL ICL USTRATH SOTON M41

Dissemination and Communication Plan

Dissemination action plan to describe dissemination and communication strategy towards the different audience in collaboration with the JU Project ManagerContributors TUBS USTRATH Imperial IRT DNW

Literature study report

Report summarizing the stateoftheart technologies and configurations and the numerical experimental strategies required to escalate the TRL of ultrahigh aspect ratio wing concept and airframe This will also include three stateoftheart reference aircraftContributorsUSTRATHICLIRTTUBS

Report on the preliminary design approach and the six initial architectures, MDO of the mid-range configuration

D31 Report on the preliminary design approach and the six initial architectures MDO of the midrange aircraft lessons learned during the exploration of MDO processIRT TUBS USTRATH SOTON M32

Project plan

A project plan will be developedContributors TUBS USTRATH ICL IRT DNW

Report on methods for uncertainty quantification

Report on methods characterisation of uncertainty for conceptual and preliminary design including design of experiments for sensitivity study and UMDOContributors USTRATH

Report on the aeroelastic coupled aerostructural modelling methodologies and associated open-source implementations

Report on the aeroelastic coupled aerostructural modelling methodologies and associated opensource implementationsContributors TUBS ICL IRT

Open Research Data Pilot (1)

Data Management Plan

A data management plan DMP will be developedContributors TUBS USTRATH ICL IRT DNW

Publications

Other (2)

Session 6: Enabling technologies

Auteurs: Marco Fossati; Christian Breitenstein; Silvestre Pinho; Joseph Morlier
Publié dans: Parametric study of the aerodynamic performance of high-aspect ratio strut-braced wings, Numéro AR20+: Workshop on High Aspect Ratio Wing Technologies, 2023
Éditeur: Brahmal Vasudevan Institute for Sustainable Aviation at Imperial College London
DOI: 10.52843/cassyni.0gzc6q

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Auteurs: Nagy P., Bennie S., Fossati M.
Publié dans: 2023
Éditeur: UK Fluids Machine Learning Special Interest Group Meeting

Peer reviewed articles (7)

Twin-fuselage configuration for improving fuel efficiency of passenger aircraft

Auteurs: Yiyuan Ma, Ali Elham
Publié dans: Aerospace Science and Technology, Numéro 118 (2021), 2021, ISSN 1270-9638
Éditeur: Elsevier BV
DOI: 10.1016/j.ast.2021.107000

Conceptual design and comparative study of strut-braced wing and twin-fuselage aircraft configurations with ultra-high aspect ratio wings

Auteurs: Yiyuan Ma, Stanislav Karpuk, Ali Elham
Publié dans: Aerospace Science and Technology, Numéro Volume 121, February 2022, 107395, 2022, ISSN 1270-9638
Éditeur: Elsevier BV
DOI: 10.1016/j.ast.2022.107395

Adaptive Data-Driven Model Order Reduction for Unsteady Aerodynamics

Auteurs: Peter Nagy; Marco Fossati
Publié dans: Fluids 2022, Numéro 7, 130, 2022, ISSN 2311-5521
Éditeur: MDPI
DOI: 10.3390/fluids7040130

Geometric sensitivity study on the aerodynamics of a strut-braced wing

Auteurs: Jones, B., Nagy, P., Minisci, E., Fossati, M.
Publié dans: Aerospace Science and Technology, 2023, ISSN 1270-9638
Éditeur: Elsevier BV

A numerical investigation on direct and data-driven flutter prediction methods

Auteurs: Simiriotis N., Palacios R.
Publié dans: Journal of Fluids and Structures, Numéro Vol. 117, No. 103835, 2023, ISSN 0889-9746
Éditeur: Academic Press
DOI: 10.1016/j.jfluidstructs.2023.103835

Geometrically Nonlinear Coupled Adjoint Aerostructural Optimization of Natural-Laminar-Flow Strut-Braced Wing

Auteurs: Ma, Y., Abouhamzeh, M. & Elham, A.
Publié dans: Journal of Aircraft, 2022, ISSN 1533-3868
Éditeur: Aerospace Research Central
DOI: 10.2514/1.c036988

Geometrically Nonlinear Effects on the Aeroelastic Response of a Transport Aircraft Configuration

Auteurs: Cea A., Palacios R.
Publié dans: Journal of Aircraft, Numéro Vol. 60, No. 1,, 2023, Page(s) 205-2020, ISSN 1533-3868
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.c036740

Conference proceedings (12)

Initial Weight Estimation of Twin-Fuselage Configuration in Aircraft Conceptual Design

Auteurs: Yiyuan Ma, Jin Yan, Ali Elham
Publié dans: SAWE 80th International Conference on Mass Properties Engineering, 2021
Éditeur: SAWE International Conference on Mass Properties Engineering - Conference Proceedings

Conceptual Design and Comparative Study of Strut-Braced Wing and Twin-Fuselage Aircraft Configurations with Ultra-High Aspect Ratio Wings

Auteurs: Yiyuan Ma, Stanislav Karpuk, Ali Elham
Publié dans: AIAA Aviation 2021 Forum, Numéro 2021, 2021
Éditeur: AIAA
DOI: 10.2514/6.2021-2425

Next steps in aerostructural design of ultra-high aspect ratio wings

Auteurs: Ma, Y., Elham
Publié dans: Aerospace Europe Conference 2023, Numéro 10th EUCASS - 9th CEAS, 9-13 July 2023, 2023
Éditeur: Aerospace Europe Conference
DOI: 10.13009/eucass2023-478

A non-intrusive nonlinear aeroelastic extension of loads packages with application to long range transport aircraft configuration

Auteurs: Cea, A; Palacios, R
Publié dans: AIAA Scitech 2021 Forum, 2021
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2021-1154

A Geometrically Nonlinear Structural Model for Aerostructural Optimization of Ultra-High Aspect Ratio Composite Wings

Auteurs: Abouhamzeh, M., Ma., Y., Elham, A.
Publié dans: AIAA SciTech, Numéro January 3-7, 2022, 2022
Éditeur: AIAA

Initial Weight Estimation of Twin-Fuselage Configuration in Aircraft Conceptual Design

Auteurs: Ma, Y., Yan, J., Elham, A.
Publié dans: Proceedings of the Institution of Mechanical Engineers, Numéro Part G: Journal of Aerospace Engineering, 2022
Éditeur: EUCASS

Polynomial preconditioning in unsteady aerodynamic models for aeroelasticity

Auteurs: Palacios R., Cea A.
Publié dans: RAeS 8th Aircraft Structural Design Conference, Numéro 3-4 October 2023, 2023
Éditeur: Royal Aeronautical Society

Adaptive reduced order modelling for steady aerodynamics flow

Auteurs: Fortunato, G., Pascarella, G., Barrenechea, G., Fossati M
Publié dans: AIAA Scitech Forum 2021, 2021
Éditeur: American Institute of Aeronautics and Astronautics

Investigating the Influence of Uncertainty in Novel Airframe Technologies on Realizing Ultra-high Aspect Ratio Wings

Auteurs: Yiyuan Ma, Edmondo Minisci, Ali Elham
Publié dans: AeroBest 2021 - International Conference on Multidisciplinary Design Optimization of Aerospace Systems, 2021, Page(s) 575-596, ISBN 978-989-99424-8-6
Éditeur: IDMEC Instituto Superior Técnico, Universidade de Lisboa

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Auteurs: Nagy P., Bennie S., Fossati M.
Publié dans: UK Fluids Machine Learning Special Interest Group Meeting, 2023
Éditeur: Leeds Institute for Fluid Dynamics

Comprehensive approach for aerostructural optimisation of ultra-high aspect ratio wings

Auteurs: Ma, Y., Elham, A.
Publié dans: RAeS 8th Aircraft Structural Design Conference, Numéro 3-4 October 2023, 2023
Éditeur: Royal Aeronautical Society

Computational Challenges in the Modular Design of Future Aircraft Concepts with Flutter Constraints

Auteurs: Cea A., Nagy P., Roussouly N., Fossati M., Palacios R.
Publié dans: AeroBest, Numéro 19-21 July 2023, 2023
Éditeur: AeroBest

Book chapters (1)

Multi-fidelity Nonlinear Aeroelastic Analysis of a Strut-braced Ultra-high Aspect Ratio Wing Configuration

Auteurs: Peter Nagy; Bryn Jones; Edmondo Minisci; Marco Fossati; Alvaro Cea; Rafael Palacios; Nicolas Roussouly; Anne Gazaix
Publié dans: AIAA Aviation Forum 2022, Numéro 2022, 2022
Éditeur: American Institute of Aeronautics and Astronautics Inc.
DOI: 10.2514/6.2022-3668