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

Informacje na temat projektu

RHEA

Identyfikator umowy o grant: 883670

DOI

10.3030/883670

Projekt został zamknięty

Data podpisania przez KE 15 Kwietnia 2020

Data rozpoczęcia 1 Lipca 2020

Data zakończenia 30 Listopada 2023

Finansowanie w ramach

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Koszt całkowity

€ 1 323 981,27

Wkład UE

€ 1 323 981,27

Koordynowany przez

TECHNISCHE UNIVERSITAET BRAUNSCHWEIG
Germany

CORDIS oferuje możliwość skorzystania z odnośników do publicznie dostępnych publikacji i rezultatów projektów realizowanych w ramach programów ramowych HORYZONT.

Odnośniki do rezultatów i publikacji związanych z poszczególnymi projektami 7PR, a także odnośniki do niektórych konkretnych kategorii wyników, takich jak zbiory danych i oprogramowanie, są dynamicznie pobierane z systemu OpenAIRE .

Rezultaty

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

Publikacje

Other (2)

Session 6: Enabling technologies

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

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Autorzy: Nagy P., Bennie S., Fossati M.
Opublikowane w: 2023
Wydawca: UK Fluids Machine Learning Special Interest Group Meeting

Peer reviewed articles (7)

Twin-fuselage configuration for improving fuel efficiency of passenger aircraft

Autorzy: Yiyuan Ma, Ali Elham
Opublikowane w: Aerospace Science and Technology, Numer 118 (2021), 2021, ISSN 1270-9638
Wydawca: 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

Autorzy: Yiyuan Ma, Stanislav Karpuk, Ali Elham
Opublikowane w: Aerospace Science and Technology, Numer Volume 121, February 2022, 107395, 2022, ISSN 1270-9638
Wydawca: Elsevier BV
DOI: 10.1016/j.ast.2022.107395

Adaptive Data-Driven Model Order Reduction for Unsteady Aerodynamics

Autorzy: Peter Nagy; Marco Fossati
Opublikowane w: Fluids 2022, Numer 7, 130, 2022, ISSN 2311-5521
Wydawca: MDPI
DOI: 10.3390/fluids7040130

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

Autorzy: Jones, B., Nagy, P., Minisci, E., Fossati, M.
Opublikowane w: Aerospace Science and Technology, 2023, ISSN 1270-9638
Wydawca: Elsevier BV

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

Autorzy: Simiriotis N., Palacios R.
Opublikowane w: Journal of Fluids and Structures, Numer Vol. 117, No. 103835, 2023, ISSN 0889-9746
Wydawca: Academic Press
DOI: 10.1016/j.jfluidstructs.2023.103835

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

Autorzy: Ma, Y., Abouhamzeh, M. & Elham, A.
Opublikowane w: Journal of Aircraft, 2022, ISSN 1533-3868
Wydawca: Aerospace Research Central
DOI: 10.2514/1.c036988

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

Autorzy: Cea A., Palacios R.
Opublikowane w: Journal of Aircraft, Numer Vol. 60, No. 1,, 2023, Strona(/y) 205-2020, ISSN 1533-3868
Wydawca: 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

Autorzy: Yiyuan Ma, Jin Yan, Ali Elham
Opublikowane w: SAWE 80th International Conference on Mass Properties Engineering, 2021
Wydawca: 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

Autorzy: Yiyuan Ma, Stanislav Karpuk, Ali Elham
Opublikowane w: AIAA Aviation 2021 Forum, Numer 2021, 2021
Wydawca: AIAA
DOI: 10.2514/6.2021-2425

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

Autorzy: Ma, Y., Elham
Opublikowane w: Aerospace Europe Conference 2023, Numer 10th EUCASS - 9th CEAS, 9-13 July 2023, 2023
Wydawca: 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

Autorzy: Cea, A; Palacios, R
Opublikowane w: AIAA Scitech 2021 Forum, 2021
Wydawca: 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

Autorzy: Abouhamzeh, M., Ma., Y., Elham, A.
Opublikowane w: AIAA SciTech, Numer January 3-7, 2022, 2022
Wydawca: AIAA

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

Autorzy: Ma, Y., Yan, J., Elham, A.
Opublikowane w: Proceedings of the Institution of Mechanical Engineers, Numer Part G: Journal of Aerospace Engineering, 2022
Wydawca: EUCASS

Polynomial preconditioning in unsteady aerodynamic models for aeroelasticity

Autorzy: Palacios R., Cea A.
Opublikowane w: RAeS 8th Aircraft Structural Design Conference, Numer 3-4 October 2023, 2023
Wydawca: Royal Aeronautical Society

Adaptive reduced order modelling for steady aerodynamics flow

Autorzy: Fortunato, G., Pascarella, G., Barrenechea, G., Fossati M
Opublikowane w: AIAA Scitech Forum 2021, 2021
Wydawca: American Institute of Aeronautics and Astronautics

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

Autorzy: Yiyuan Ma, Edmondo Minisci, Ali Elham
Opublikowane w: AeroBest 2021 - International Conference on Multidisciplinary Design Optimization of Aerospace Systems, 2021, Strona(/y) 575-596, ISBN 978-989-99424-8-6
Wydawca: IDMEC Instituto Superior Técnico, Universidade de Lisboa

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Autorzy: Nagy P., Bennie S., Fossati M.
Opublikowane w: UK Fluids Machine Learning Special Interest Group Meeting, 2023
Wydawca: Leeds Institute for Fluid Dynamics

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

Autorzy: Ma, Y., Elham, A.
Opublikowane w: RAeS 8th Aircraft Structural Design Conference, Numer 3-4 October 2023, 2023
Wydawca: Royal Aeronautical Society

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

Autorzy: Cea A., Nagy P., Roussouly N., Fossati M., Palacios R.
Opublikowane w: AeroBest, Numer 19-21 July 2023, 2023
Wydawca: AeroBest

Book chapters (1)

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

Autorzy: Peter Nagy; Bryn Jones; Edmondo Minisci; Marco Fossati; Alvaro Cea; Rafael Palacios; Nicolas Roussouly; Anne Gazaix
Opublikowane w: AIAA Aviation Forum 2022, Numer 2022, 2022
Wydawca: American Institute of Aeronautics and Astronautics Inc.
DOI: 10.2514/6.2022-3668