Hybrid Electric Regional Wing Integration Novel Green Technologies - HERWINGT

Informazioni relative al progetto

HERWINGT

ID dell’accordo di sovvenzione: 101102010

DOI

10.3030/101102010

Data della firma CE 9 Dicembre 2022

Data di avvio 1 Gennaio 2023

Data di completamento 31 Ottobre 2026

Finanziato da

• Climate, Energy and Mobility

Costo totale

€ 28 278 745,23

Contributo UE

€ 21 791 729,98

Coordinato da

AIRBUS DEFENCE AND SPACE SA
Spain

CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.

I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .

Risultati finali

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 (3)

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

Pubblicazioni

Conference proceedings (7)

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

Autori: Vittorio Cavalieri, Alessandro De Gaspari, Sergio Ricci
Pubblicato in: AIAA SCITECH 2024 Forum, 2024
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-2113

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

Autori: Xavier Carrillo, Roeland De Breuker, Jurij Sodja
Pubblicato in: AIAA SCITECH 2024 Forum, 2024
Editore: 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

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

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

Autori: Maria Chiara Noviello, Ignazio Dimino, Salvatore Ameduri, Antonio Concilio
Pubblicato in: 2024
Editore: ICAS
DOI: 10.5281/zenodo.14930442

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

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

Aero-Structural Design of a High-Aspect Ratio Wing

Autori: Pietro Catalano, Gianluca Diodati, Davide Lucariello, Pier Luigi Vitagliano
Pubblicato in: AIAA AVIATION FORUM AND ASCEND 2024, 2024
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-3502

Aerodynamic Noise Prediction of Strut-Braced Wing Aircraft

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