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Ultra High Aspect Ratio Wing Advanced Research and Designs

Deliverables

Data Management Plan

This report addresses the relevant aspects of making data findable, accessible, interoperable and re-usable, including what data the project will generate, whether and how it will be made accessible for verification and re-use, and how it will be curated and preserved. This deliverable allows to participate in the Open Research Data Pilot

Dissemination, Communication and Exploitation Plan

Plan for dissemination and exploitation of project results (D). Contribution: (All the beneficiaries)

Literature review and aircraft user-case definition

Report describing the literature study and the identification and aerodynamic reverse design of the aircraft reference

Definition of test objectives and requirements

Selection of the Wind Tunnel and Definition of test objectives and requirements. The document includes the target of the test, the description of the test setup to be provided including number and type of measurements, a preliminary test matrix. (contr. ONERA, UNIVBRIS, IBK)

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Publications

A THT Project Aiming at Ultra High Aspect Ratio Wings Advanced Research and DesignsS

Author(s): Sergio Ricci
Published in: 2021
Publisher: n/a
DOI: 10.5281/zenodo.5145447

Multidisciplinary analysis and design of strut-braced wing concept for medium range aircraft

Author(s): Gerald G. Carrier, Guillaume Arnoult, Nicolo Fabbiane, Jean-Sebastien Schotte, Christophe David, Sébastien Defoort, Emmanuel Benard and Martin Delavenne
Published in: AIAA SCITECH 2022 Forum, 1, 2022
Publisher: AIAA
DOI: 10.2514/6.2022-0726

Sizing of High Aspect Ratio Wings with Folding Wing Tips

Author(s): Huaiyuan Gu, Fintan Healy, Djamel Rezgui and Jonathan E. Cooper
Published in: AIAA SCITECH 2022 Forum, 1, 2022
Publisher: AIAA
DOI: 10.2514/6.2022-0723

Aero-Servo-Elastic Optimization in Early Design Phases

Author(s): Toffol, F.; Ricci, S.
Published in: AIDAA - XXVI INTERNATIONAL CONGRESS 31ST AUGUST – 3 RD SEPTEMBER 2021, 1, 2021
Publisher: AIDAA

Recent Achievements in the Design of Ultra High Aspect Ratio Wings of Environmental Friendly Aircraft

Author(s): Ricci Sergio
Published in: 2021
Publisher: IOP Publishing Ltd
DOI: 10.5281/zenodo.5706398

Aeroelastic Optimization of High Aspect Ratio Wings for Environmentally Friendly Aircraft

Author(s): Ricci, S.; Marchetti, L.; Toffol, F.; Beretta, J.; Paletta, N.
Published in: AIAA SCITECH 2022 Forum, 1, 2022
Publisher: AIAA
DOI: 10.2514/6.2022-0166

SIZING OF HIGH ASPECT RATIO WINGS INCORPORATING FOLDING WINGTIP

Author(s): H. Gu, F. Healy, J.E.Cooper
Published in: 2021
Publisher: IDMEC Instituto Superior Técnico Universidade de Lisboa

Sizing of High Aspect Ratio Wing incorporating Folding Wingtips

Author(s): Huaiyuan Gu, Fintan Healy, Jonathan Cooper
Published in: 2021, ISBN 978-989-99424-8-6
Publisher: IDMEC Instituto Superior Técnico Universidade de Lisboa
DOI: 10.5281/zenodo.5708286

U-HARWARD: a CS2 EU Funded Project Aiming at the Design of Ultra High Aspect Ratio Wings Aircraft

Author(s): Ricci, S.; Paletta, N.; Defoort, S.; Benard, E.; Cooper, J. E.; Barabinot, P.
Published in: AIAA SCITECH 2022 Forum, 1, 2022
Publisher: AIAA
DOI: 10.2514/6.2022-0168

Wingbox Meta-Model and Aero-Servo-Elastic Optimization With NEOPT

Author(s): Toffol, F.; Ricci, S.
Published in: AeroBest 2021 Lisboa, 21-23 July 2021, 2, 2021, ISBN 978-989-99424-8-6
Publisher: IDMEC