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

Deliverables

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

Project plan

A project plan will be developedContributors TUBS USTRATH ICL IRT DNW

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

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Publications

Twin-fuselage configuration for improving fuel efficiency of passenger aircraft

Author(s): Yiyuan Ma, Ali Elham
Published in: Aerospace Science and Technology, 118 (2021), 2021, ISSN 1270-9638
Publisher: 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

Author(s): Yiyuan Ma, Stanislav Karpuk, Ali Elham
Published in: Aerospace Science and Technology, Volume 121, February 2022, 107395, 2022, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/j.ast.2022.107395

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

Author(s): Yiyuan Ma, Jin Yan, Ali Elham
Published in: SAWE 80th International Conference on Mass Properties Engineering, 2021
Publisher: 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

Author(s): Yiyuan Ma, Stanislav Karpuk, Ali Elham
Published in: AIAA AVIATION 2021 FORUM, 2021, ISBN 978-1-62410-610-1
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2021-2425

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

Author(s): Cea, A; Palacios, R
Published in: AIAA Scitech 2021 Forum, 2021
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2021-1154

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

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