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

Risultati finali

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.

Pubblicazioni

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

Autori: Fang Han, Luis Fernando Lopes de Moraes Filho, Djamel Rezgui, Burak Buda Turhan, Mahdi Azarpeyvand, Abhishek Gautam, Bin Zang, Beckett Zhou
Pubblicato in: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editore: 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

Autori: Ciera, Zachary; Jones, Bryn; Fossati, Marco
Pubblicato in: 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

Autori: Forrest Han; Christopher Yi; Luis Fernando F. Lopes De Moraes Filho; Burak Turhan; Djamel Rezgui; Mahdi Azarpeyvand
Pubblicato in: 32nd AIAA/CEAS Aeroacoustics Conference (2026), Numero AIAA 2026-3229, 2026
Editore: 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

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

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

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

Aeroacoustic Investigation of a High-Lift Propeller-Wing Configuration

Autori: Andrea Franco, Karl-Stéphane Rossignol, Roland Ewert, Jan Delfs
Pubblicato in: 32nd AIAA/CEAS Aeroacoustics Conference (2026), 2026
Editore: 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

Autori: Cavallaro, Rauno; Norczyk Simon, Pablo; Cini, Andrea
Pubblicato in: 2025
Editore: 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

Autori: Luis Fernando Lopes de Moraes Filho, Burak Buda Turhan, Andrea Franco, Leone Trascinelli, Djamel Rezgui, Mahdi Azarpeyvand, Roland Ewert, Beckett Zhou, Bin Zang
Pubblicato in: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editore: 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

Autori: 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

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

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

Autori: Gallego Pozo, Alberto; Cavallaro, Rauno
Pubblicato in: 2024
DOI: 10.82439/CEAS-IFASD-2024-182

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

Autori: Pablo, Norczyk Simon; Cavallaro, Rauno; Zheng Zhang, Danlin; Brižs, Jānis
Pubblicato in: 2025
DOI: 10.5281/ZENODO.15182834

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

Autori: Jones, Catherine E; Fong, Kenny; Norman, Patrick
Pubblicato in: 2024
DOI: 10.5281/ZENODO.14622365

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

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

Advanced CRN Emission Prediction Model for Aircraft Engine Design

Autori: Ziaja, Karl; Lieder, Daniel; Göing, Jan; Friedrichs, Jens; Francesca, di Mare
Pubblicato in: 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

Autori: 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

Autori: Ciera, Zachary; Jones, Bryn; Nagy, Peter; Fossati, Marco
Pubblicato in: 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

Autori: Barcelona Supercomputing Center; University of Strathclyde; Ruhr University Bochum
Pubblicato in: 2025
DOI: 10.5281/ZENODO.14833158

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

Autori: Fossati, Marco; Jones, Bryn; Nagy, Peter; Hepperle, Martin
Pubblicato in: AIAA SCITECH 2024 Forum, 2024
DOI: 10.2514/6.2024-2332

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

Autori: 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

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

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

Autori: Leone Trascinelli; Gianluca Romani; Liam Hanson; Damiano Casalino; B. Zang; Beckett Y. Zhou; Mahdi Azarpeyvand
Pubblicato in: The Journal of the Acoustical Society of America, Numero 158, 2025, ISSN 1520-8524
Editore: 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

Autori: Leone Trascinelli, Gianluca Romani, Damiano Casalino, B. Zang, Beckett Zhou, Mahdi Azarpeyvand
Pubblicato in: Journal of Fluid Mechanics, Numero 1039, 2026, ISSN 0022-1120
Editore: Cambridge University Press (CUP)
DOI: 10.1017/JFM.2026.11801

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

Autori: Nicolina Montella, Domenico Quagliarella
Pubblicato in: Computational Methods in Applied Sciences, Advances in Evolutionary and Deterministic Methods for Design, Optimization and Control, 2026, ISSN 1871-3033
Editore: 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

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

Risultati dei progetti

Risultati finali

Pubblicazioni

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