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

Informacje na temat projektu

INDIGO

Identyfikator umowy o grant: 101096055

DOI

10.3030/101096055

Projekt został zamknięty

Data podpisania przez KE 5 Grudnia 2022

Data rozpoczęcia 1 Lutego 2023

Data zakończenia 30 Września 2026

Finansowanie w ramach

• Climate, Energy and Mobility

Koszt całkowity

€ 3 111 446,25

Wkład UE

€ 3 111 446,25

Koordynowany przez

BARCELONA SUPERCOMPUTING CENTER CENTRO NACIONAL DE SUPERCOMPUTACION
Spain

CORDIS oferuje możliwość skorzystania z odnośników do publicznie dostępnych publikacji i rezultatów projektów realizowanych w ramach programów ramowych HORYZONT.

Odnośniki do rezultatów i publikacji związanych z poszczególnymi projektami 7PR, a także odnośniki do niektórych konkretnych kategorii wyników, takich jak zbiory danych i oprogramowanie, są dynamicznie pobierane z systemu OpenAIRE .

Rezultaty

Documents, reports (10)

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

DHEP-LARW Aircraft performance model

The aircraft performance model will consist of data-driven models for aerodynamics, structures, aeroelasticiy, emissions and acoustics. This deliverable refers to Task 3.6.

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.

Models for combustion chamber, propeller noise and electrical power system

Extensive database capturing the flame behaviour and gas components distribution within the combustion chamber by changing load conditions as well as fuel composition. This deliverable refers to Task 2.3.

Pareto-front of optimal DHEP-LARW air-craft and margins incl. selected nominal aircraft

Report describing the set of optimal integration solutions for LARW and DHEP with respect to LAQN metrics. This deliverable refers to Task 5.5.

Uncertainty modelling of TRL for LARW, DHEP and integrated technologies

Report summarizing the models developed to address the uncertainty on performance resulting from the TRL of a given technology. This deliverable refers to Task 5.1.

Preliminary greener LTO cycles and future airport scenarios

Report summarizing the identification of landing and take-off cycles deemed to provide the lowest environmental impact. This deliverable refers to Task 4.4.

Integrated hybrid propulsion system model including noise source modelling

A model of the integrated hybrid propulsion system incorporating pollutants emissions and noise will be defined and validated. This deliverable refers to Task 2.4.

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.

Publikacje

Conference proceedings (22)

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

Autorzy: Fang Han, Luis Fernando Lopes de Moraes Filho, Djamel Rezgui, Burak Buda Turhan, Mahdi Azarpeyvand, Abhishek Gautam, Bin Zang, Beckett Zhou
Opublikowane w: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Wydawca: 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

Autorzy: Ciera, Zachary; Jones, Bryn; Fossati, Marco
Opublikowane w: 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

Autorzy: Forrest Han; Christopher Yi; Luis Fernando F. Lopes De Moraes Filho; Burak Turhan; Djamel Rezgui; Mahdi Azarpeyvand
Opublikowane w: 32nd AIAA/CEAS Aeroacoustics Conference (2026), Numer AIAA 2026-3229, 2026
Wydawca: 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

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

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

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

Aeroacoustic Investigation of a High-Lift Propeller-Wing Configuration

Autorzy: Andrea Franco, Karl-Stéphane Rossignol, Roland Ewert, Jan Delfs
Opublikowane w: 32nd AIAA/CEAS Aeroacoustics Conference (2026), 2026
Wydawca: 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

Autorzy: Cavallaro, Rauno; Norczyk Simon, Pablo; Cini, Andrea
Opublikowane w: 2025
Wydawca: 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

Autorzy: Luis Fernando Lopes de Moraes Filho, Burak Buda Turhan, Andrea Franco, Leone Trascinelli, Djamel Rezgui, Mahdi Azarpeyvand, Roland Ewert, Beckett Zhou, Bin Zang
Opublikowane w: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Wydawca: 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

Autorzy: 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

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

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

Autorzy: Gallego Pozo, Alberto; Cavallaro, Rauno
Opublikowane w: 2024
DOI: 10.82439/CEAS-IFASD-2024-182

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

Autorzy: Pablo, Norczyk Simon; Cavallaro, Rauno; Zheng Zhang, Danlin; Brižs, Jānis
Opublikowane w: 2025
DOI: 10.5281/ZENODO.15182834

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

Autorzy: Jones, Catherine E; Fong, Kenny; Norman, Patrick
Opublikowane w: 2024
DOI: 10.5281/ZENODO.14622365

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

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

Advanced CRN Emission Prediction Model for Aircraft Engine Design

Autorzy: Ziaja, Karl; Lieder, Daniel; Göing, Jan; Friedrichs, Jens; Francesca, di Mare
Opublikowane w: 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

Autorzy: 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

Autorzy: Ciera, Zachary; Jones, Bryn; Nagy, Peter; Fossati, Marco
Opublikowane w: 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

Autorzy: Barcelona Supercomputing Center; University of Strathclyde; Ruhr University Bochum
Opublikowane w: 2025
DOI: 10.5281/ZENODO.14833158

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

Autorzy: Fossati, Marco; Jones, Bryn; Nagy, Peter; Hepperle, Martin
Opublikowane w: AIAA SCITECH 2024 Forum, 2024
DOI: 10.2514/6.2024-2332

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

Autorzy: 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

Autorzy: 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

Autorzy: Leone Trascinelli; Gianluca Romani; Liam Hanson; Damiano Casalino; B. Zang; Beckett Y. Zhou; Mahdi Azarpeyvand
Opublikowane w: The Journal of the Acoustical Society of America, Numer 158, 2025, ISSN 1520-8524
Wydawca: 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

Autorzy: Leone Trascinelli, Gianluca Romani, Damiano Casalino, B. Zang, Beckett Zhou, Mahdi Azarpeyvand
Opublikowane w: Journal of Fluid Mechanics, Numer 1039, 2026, ISSN 0022-1120
Wydawca: 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

Autorzy: Nicolina Montella, Domenico Quagliarella
Opublikowane w: Computational Methods in Applied Sciences, Advances in Evolutionary and Deterministic Methods for Design, Optimization and Control, 2026, ISSN 1871-3033
Wydawca: 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

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