Hybrid Electric Regional Wing Integration Novel Green Technologies - HERWINGT

Project Information

HERWINGT

Grant agreement ID: 101102010

DOI

10.3030/101102010

EC signature date 9 December 2022

Start date 1 January 2023

End date 31 October 2026

Funded under

• Climate, Energy and Mobility

Total cost

€ 28 278 745,23

EU contribution

€ 21 791 729,98

Coordinated by

AIRBUS DEFENCE AND SPACE SA
Spain

CORDIS provides links to public deliverables and publications of HORIZON projects.

Links to deliverables and publications from FP7 projects, as well as links to some specific result types such as dataset and software, are dynamically retrieved from OpenAIRE .

Deliverables

Data Management Plan (1)

Data Management Plan

Data management methodology for all data sets that will be handled throughout the project. First version of the document (M3)

Documents, reports (4)

Enablers for Multi-Functional LE design
Project Management and Quality Assurance Plan

Project Plan document describing the proper procedures towards the quality assurance of the project

Final Assessment Report of SAFs Compatibility and further activities required

Summary of compatibility studies between SAF pathways

Plan for Dissemination & Exploitation including communication activities

The concrete strategy that will be followed regarding the Dissemination Communication and Exploitation Activities will be elaborated at the beginning of the project and will be monitored and updated throughout the entire project life cycle

Publications

Conference proceedings (9)

Aero-Structural Design Optimization of a Morphing Aileron Considering Actuation Aspects

Author(s): Vittorio Cavalieri, Alessandro De Gaspari, Sergio Ricci
Published in: AIAA SCITECH 2024 Forum, 2024
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-2113

The Aerodynamic Design of a Compliant Morphing Flap for Next-Generation Hybrid Electric Regional Aircraft

Author(s): Francesco Antonio D’Aniello, Pietro Catalano, Domenico Quagliarella, Mauro Minervino
Published in: EASN 2024, 2025, ISSN 2673-4591
Publisher: MDPI
DOI: 10.3390/ENGPROC2025090013

Aeroelastic Tailoring of a Strut-Braced Wing for a Medium Range Aircraft

Author(s): Xavier Carrillo, Roeland De Breuker, Jurij Sodja
Published in: AIAA SCITECH 2024 Forum, 2024
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-2590

Aerodynamic design of a compliant morphing flap for the next generation hybrid-electric regional aircrafts

Author(s): Francesco Antonio D'Aniello, Pietro Catalano, D. Quagliarella, and Mauro Minervino
Published in: 14th European Aeronautics Science Network (EASN) International Conference, 2025
Publisher: EASN
DOI: 10.5281/zenodo.14717267

Conceptual Design and Topology Optimization of a Compliant Morphing Flap for Next Generation Hybrid-Electric Regional Aircraft

Author(s): Maria Chiara Noviello, Ignazio Dimino, Salvatore Ameduri, Antonio Concilio
Published in: 2024
Publisher: ICAS
DOI: 10.5281/zenodo.14930442

Multi–objective design optimization of a morphing aileron for a hybrid electric regional aircraft

Author(s): Alessandro De Gaspari, Vittorio Cavalieri, Matteo Corti, and Sergio Ricci (POLIMI)
Published in: 34th Congress of the International Council of the Aeronautical Sciences (ICAS) Congress,, 2024
Publisher: ICAS
DOI: 10.5281/zenodo.14930343

Aero-Structural Design of a High-Aspect Ratio Wing

Author(s): Pietro Catalano, Gianluca Diodati, Davide Lucariello, Pier Luigi Vitagliano
Published in: AIAA AVIATION FORUM AND ASCEND 2024, 2024
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-3502

AI-Based Generative Algorithms Applied to the Design of Blended Wing Body Aircraft

Author(s): Marta A. Martín, Andrés Mateo, Thomas Wagenaar, Gonzalo Rubio, Sven A. Lanzan Ferran
Published in: AIAA AVIATION FORUM AND ASCEND 2025, 2025, ISSN 0001-1452
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-3292

Aerodynamic Noise Prediction of Strut-Braced Wing Aircraft

Author(s): Emanuele Sticchi, Daniele Ragni, Damiano Casalino, Francesco Avallone
Published in: 30th AIAA/CEAS Aeroacoustics Conference (2024), 2024
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-3012

Peer reviewed articles (2)

Design and Optimization of a Compliant Morphing Trailing Edge for High-Lift Generation

Author(s): Salvatore Ameduri, Bernardino Galasso, Maria Chiara Noviello, Ignazio Dimino, Antonio Concilio, Pietro Catalano, Francesco Antonio D’Aniello, Giovanni Marco Carossa, Laurent Pinazo, John Derry, Britney Biju, Shruthi Shreedharan
Published in: Applied Sciences, Issue 15, 2025, ISSN 2076-3417
Publisher: MDPI AG
DOI: 10.3390/APP15052529

Design optimization and virtual testing of a morphing aileron with high actuation bandwidth

Author(s): Vittorio Cavalieri, Alessandro De Gaspari
Published in: Aerospace Science and Technology, Issue 168, 2025, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/J.AST.2025.111110