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

Resultado final

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

Data Management Plan

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

Publicaciones

Session 6: Enabling technologies

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

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Autores: Nagy P., Bennie S., Fossati M.
Publicado en: 2023
Editor: UK Fluids Machine Learning Special Interest Group Meeting

Twin-fuselage configuration for improving fuel efficiency of passenger aircraft

Autores: Yiyuan Ma, Ali Elham
Publicado en: Aerospace Science and Technology, Edición 118 (2021), 2021, ISSN 1270-9638
Editor: 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

Autores: Yiyuan Ma, Stanislav Karpuk, Ali Elham
Publicado en: Aerospace Science and Technology, Edición Volume 121, February 2022, 107395, 2022, ISSN 1270-9638
Editor: Elsevier BV
DOI: 10.1016/j.ast.2022.107395

Adaptive Data-Driven Model Order Reduction for Unsteady Aerodynamics

Autores: Peter Nagy; Marco Fossati
Publicado en: Fluids 2022, Edición 7, 130, 2022, ISSN 2311-5521
Editor: MDPI
DOI: 10.3390/fluids7040130

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

Autores: Jones, B., Nagy, P., Minisci, E., Fossati, M.
Publicado en: Aerospace Science and Technology, 2023, ISSN 1270-9638
Editor: Elsevier BV

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

Autores: Simiriotis N., Palacios R.
Publicado en: Journal of Fluids and Structures, Edición Vol. 117, No. 103835, 2023, ISSN 0889-9746
Editor: Academic Press
DOI: 10.1016/j.jfluidstructs.2023.103835

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

Autores: Cea A., Palacios R.
Publicado en: Journal of Aircraft, Edición Vol. 60, No. 1,, 2023, Página(s) 205-2020, ISSN 1533-3868
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.c036740

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

Autores: Yiyuan Ma, Jin Yan, Ali Elham
Publicado en: SAWE 80th International Conference on Mass Properties Engineering, 2021
Editor: 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

Autores: Yiyuan Ma, Stanislav Karpuk, Ali Elham
Publicado en: AIAA Aviation 2021 Forum, Edición 2021, 2021
Editor: AIAA
DOI: 10.2514/6.2021-2425

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

Autores: Ma, Y., Elham
Publicado en: Aerospace Europe Conference 2023, Edición 10th EUCASS - 9th CEAS, 9-13 July 2023, 2023
Editor: 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

Autores: Cea, A; Palacios, R
Publicado en: AIAA Scitech 2021 Forum, 2021
Editor: 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

Autores: Abouhamzeh, M., Ma., Y., Elham, A.
Publicado en: AIAA SciTech, Edición January 3-7, 2022, 2022
Editor: AIAA

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

Autores: Ma, Y., Yan, J., Elham, A.
Publicado en: Proceedings of the Institution of Mechanical Engineers, Edición Part G: Journal of Aerospace Engineering, 2022
Editor: EUCASS

Polynomial preconditioning in unsteady aerodynamic models for aeroelasticity

Autores: Palacios R., Cea A.
Publicado en: RAeS 8th Aircraft Structural Design Conference, Edición 3-4 October 2023, 2023
Editor: Royal Aeronautical Society

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

Autores: Yiyuan Ma, Edmondo Minisci, Ali Elham
Publicado en: AeroBest 2021 - International Conference on Multidisciplinary Design Optimization of Aerospace Systems, 2021, Página(s) 575-596, ISBN 978-989-99424-8-6
Editor: IDMEC Instituto Superior Técnico, Universidade de Lisboa

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Autores: Nagy P., Bennie S., Fossati M.
Publicado en: UK Fluids Machine Learning Special Interest Group Meeting, 2023
Editor: Leeds Institute for Fluid Dynamics

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

Autores: Ma, Y., Elham, A.
Publicado en: RAeS 8th Aircraft Structural Design Conference, Edición 3-4 October 2023, 2023
Editor: Royal Aeronautical Society

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

Autores: Cea A., Nagy P., Roussouly N., Fossati M., Palacios R.
Publicado en: AeroBest, Edición 19-21 July 2023, 2023
Editor: AeroBest

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

Autores: Peter Nagy; Bryn Jones; Edmondo Minisci; Marco Fossati; Alvaro Cea; Rafael Palacios; Nicolas Roussouly; Anne Gazaix
Publicado en: AIAA Aviation Forum 2022, Edición 2022, 2022
Editor: American Institute of Aeronautics and Astronautics Inc.
DOI: 10.2514/6.2022-3668

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