Integration and Digital Demonstration of Low-emission Aircraft Technologies and Airport Operations

Información del proyecto

INDIGO

Identificador del acuerdo de subvención: 101096055

DOI

10.3030/101096055

Proyecto cerrado

Fecha de la firma de la CE 5 Diciembre 2022

Fecha de inicio 1 Febrero 2023

Fecha de finalización 30 Septiembre 2026

Financiado con arreglo a

• Climate, Energy and Mobility

Coste total

€ 3 111 446,25

Aportación de la UE

€ 3 111 446,25

Coordinado por

BARCELONA SUPERCOMPUTING CENTER CENTRO NACIONAL DE SUPERCOMPUTACION
Spain

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

Documents, reports (4)

Reference and Baseline aircraft concepts in CPACS format

The reference and baseline aircraft configurations will be defined and the data required to generate the geometry of the aircraft will be provided in CPACS format. This deliverable refers to Task 1.5

Extended Airport Operations and Performance Model

A report summarizing the adopted model for efficient evaluation of aircraft trajectories over airport area. This deliverable refers to Task 4.2.

Dissemination and communication action plan (DCAP)

Report detailing the DCA plan and responsibilities among the partners. This deliverable refers to Task 7.3.

Digital model definition in CPACS format of the selected aircraft configurations

Creation of the CPACS structure for the aircraft with minimal requirements for components. This deliverable refers to Task 3.1.

Websites, patent fillings, videos etc. (1)

Project website and social media presence

Project website, Linkedin, twitter and youtube channel. This deliverable refers to Task 7.3.

Data Management Plan (1)

Data management plan

Data management plan. This deliverable refers to Task 7.1.

Publicaciones

Conference proceedings (22)

Aerodynamic Performance of Distributed Electric Propulsion Wing Under Different Design and Operating Parameters

Autores: Fang Han, Luis Fernando Lopes de Moraes Filho, Djamel Rezgui, Burak Buda Turhan, Mahdi Azarpeyvand, Abhishek Gautam, Bin Zang, Beckett Zhou
Publicado en: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-3096

Data-Driven Multi-Fidelity Modelling of Large Aspect Ratio Wings with Distributed Propellers

Autores: Ciera, Zachary; Jones, Bryn; Fossati, Marco
Publicado en: AIAA AVIATION FORUM AND ASCEND 2025, 2025
DOI: 10.5281/ZENODO.14640284

Aeroacoustic Characteristics of a Twin-Propeller Distributed Electric Propulsion System with Phase Synchronisation at Various Wing Angles of Attack

Autores: Forrest Han; Christopher Yi; Luis Fernando F. Lopes De Moraes Filho; Burak Turhan; Djamel Rezgui; Mahdi Azarpeyvand
Publicado en: 32nd AIAA/CEAS Aeroacoustics Conference (2026), Edición AIAA 2026-3229, 2026
Editor: American Institute of Aeronautics and Astronautics Inc. (AIAA)
DOI: 10.2514/6.2026-3229

Aerodynamic Performance of Various Strut-Braced Wing Designs for Distributed Electric Propulsion Configurations in Forward Flights

Autores: Fang Han, Zachary K. Ciera, Burak Buda Turhan, Marco Fossati, Djamel Rezgui, Mahdi Azarpeyvand
Publicado en: AIAA AVIATION 2026 Forum, 2026
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2026-4600

Investigation of Aerodynamic and Aeroacoustic Performance of Various Distributed Electric Propulsion Configurations

Autores: Fang Han, Luis Fernando Lopes de Moraes Filho, Djamel Rezgui, Burak Buda Turhan, Mahdi Azarpeyvand, Abhishek Gautam, Bin Zang, Beckett Zhou
Publicado en: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-3644

Aeroacoustic Investigation of a High-Lift Propeller-Wing Configuration

Autores: Andrea Franco, Karl-Stéphane Rossignol, Roland Ewert, Jan Delfs
Publicado en: 32nd AIAA/CEAS Aeroacoustics Conference (2026), 2026
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2026-3393

LOCAL AIR QUALITY AND NOISE OPTIMIZATION OF A LARGE ASPECT RATIO WINGS WITH DISTRIBUTED HYBRID ELECTRIC PROPULSION

Autores: Cavallaro, Rauno; Norczyk Simon, Pablo; Cini, Andrea
Publicado en: 2025
Editor: ICAS
DOI: 10.5281/zenodo.13902089

Assessment of Aeroacoustic Simulations for the Installation Noise of a Propeller-Wing Configuration in Forward Flight Using Multi-Fidelity Solvers

Autores: Luis Fernando Lopes de Moraes Filho, Burak Buda Turhan, Andrea Franco, Leone Trascinelli, Djamel Rezgui, Mahdi Azarpeyvand, Roland Ewert, Beckett Zhou, Bin Zang
Publicado en: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-3642

Structural Optimisation for Mass Estimation of Large-Aspect-Ratio Wings with Distributed Hybrid Propulsion

Autores: Carvalho, João; Cavallaro, Rauno; Cini, Andrea
DOI: 10.3390/ENGPROC2025090085

Multidisciplinary Optimization of Strut-BracedWings with Distributed Electric Propulsion for Local Air Quality and Noise Improvements

Autores: Norczyk-Simon, Pablo; Cavallaro, Rauno
DOI: 10.5281/ZENODO.14809011

FLIGHT DYNAMIC-AEROELASTIC RESPONSE OF A HIGHLY FLEXIBLE AIRCRAFT WITH DISTRIBUTED PROPELLERS

Autores: Gallego Pozo, Alberto; Cavallaro, Rauno
Publicado en: 2024
DOI: 10.82439/CEAS-IFASD-2024-182

MULTIDISCIPLINARY DESIGN AND OPTIMIZATION OF STRUT-BRACED HYBRID-ELECTRIC AIRCRAFT UNDER MULTI-TRAJECTORY SCENARIOS

Autores: Pablo, Norczyk Simon; Cavallaro, Rauno; Zheng Zhang, Danlin; Brižs, Jānis
Publicado en: 2025
DOI: 10.5281/ZENODO.15182834

SAFETY-DRIVEN BASELINING OF HYBRID ELECTRIC AIRCRAFT ELECTRICAL POWER SYSTEM ARCHITECTURES

Autores: Jones, Catherine E; Fong, Kenny; Norman, Patrick
Publicado en: 2024
DOI: 10.5281/ZENODO.14622365

INtegration and Digital demonstration of low-emission aIrcraft technoloGies and airport Operations

Autores: Cavallaro, Rauno
DOI: 10.5281/ZENODO.14809164

Advanced CRN Emission Prediction Model for Aircraft Engine Design

Autores: Ziaja, Karl; Lieder, Daniel; Göing, Jan; Friedrichs, Jens; Francesca, di Mare
Publicado en: AIAA SCITECH 2026 Forum, 2026
DOI: 10.2514/6.2026-1181

DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS

Autores: Ziaja, Karl; Lieder, Daniel; Göing, Jan; Friedrichs, Jens; di Mare, Francesca
DOI: 10.5281/ZENODO.14246221

Aerodynamics of Large Aspect Ratio Wings With Distributed Propellers via the Vortex-Lattice Method and High-Fidelity Simulations

Autores: Ciera, Zachary; Jones, Bryn; Nagy, Peter; Fossati, Marco
Publicado en: AIAA AVIATION FORUM AND ASCEND 2024, 2024
DOI: 10.2514/6.2024-4015

Local Air Quality and Noise Assessment for Landing and Take-Off Operations in Future Airport Environment

DOI: 10.3390/ENGPROC2025090074

Analysis of pollutant dispersion of a DHEP and LARW aircraft design using high-fidelity simulations

Autores: Barcelona Supercomputing Center; University of Strathclyde; Ruhr University Bochum
Publicado en: 2025
DOI: 10.5281/ZENODO.14833158

An aerodynamic parametric study of large aspect-ratio wings with distributed propulsion for conceptual airframe definition

Autores: Fossati, Marco; Jones, Bryn; Nagy, Peter; Hepperle, Martin
Publicado en: AIAA SCITECH 2024 Forum, 2024
DOI: 10.2514/6.2024-2332

FLIGHT DYNAMIC-AEROELASTIC RESPONSE OF A HIGHLY FLEXIBLE AIRCRAFT WITH DISTRIBUTED PROPELLERS

Autores: Gallego Pozo, Alberto; Cavallaro, Rauno
DOI: 10.5281/ZENODO.14223847

Local Air Quality and Noise Improvements via Optimization of Strut-Braced Wings with Distributed Electric Propulsion

Autores: Cavallaro, Rauno; Norczyk, Pablo
DOI: 10.2514/6.2025-0456

Peer reviewed articles (2)

Numerical simulations of large-scale turbulence ingestion by a forward flight propeller

Autores: Leone Trascinelli; Gianluca Romani; Liam Hanson; Damiano Casalino; B. Zang; Beckett Y. Zhou; Mahdi Azarpeyvand
Publicado en: The Journal of the Acoustical Society of America, Edición 158, 2025, ISSN 1520-8524
Editor: June 2026 View This Issue Focus and Coverage The Journal of the Acoustical Society of America
DOI: 10.1121/10.0037219

Aeroacoustics of a forward-flight propeller ingesting small- and large-scale turbulent wakes

Autores: Leone Trascinelli, Gianluca Romani, Damiano Casalino, B. Zang, Beckett Zhou, Mahdi Azarpeyvand
Publicado en: Journal of Fluid Mechanics, Edición 1039, 2026, ISSN 0022-1120
Editor: Cambridge University Press (CUP)
DOI: 10.1017/JFM.2026.11801

Book chapters (2)

A Multiobjective Approach To Evaluate Suitable Battery Technologies To Power Hybrid Medium-Range Aircraft

Autores: Nicolina Montella, Domenico Quagliarella
Publicado en: Computational Methods in Applied Sciences, Advances in Evolutionary and Deterministic Methods for Design, Optimization and Control, 2026, ISSN 1871-3033
Editor: Springer Nature Switzerland
DOI: 10.1007/978-3-032-21893-3_12

Multidisciplinary Optimization of Large Aspect-Ratio Wings with Distributed Hybrid-Electric Propulsion for Enhanced Local Air Quality and Noise Reduction

Autores: João Carvalho, Pablo Norczyk, Rauno Cavallaro
Publicado en: Lecture Notes in Mechanical Engineering, Future Aviation Propulsion Systems: From Tank to Thrust, from Research to Qualification, 2026, ISSN 2195-4356
Editor: Springer Nature Switzerland
DOI: 10.1007/978-3-032-30740-8_6