Installed adVAnced Nacelle uHbr Optimisation and Evaluation

Informazioni relative al progetto

IVANHOE

ID dell’accordo di sovvenzione: 863415

DOI

10.3030/863415

Progetto chiuso

Data della firma CE 26 Settembre 2019

Data di avvio 1 Ottobre 2019

Data di completamento 31 Ottobre 2023

Finanziato da

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Costo totale

€ 2 801 779,95

Contributo UE

€ 2 801 779,95

Coordinato da

CHALMERS TEKNISKA HOGSKOLA AB
Sweden

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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

Websites, patent fillings, videos etc. (1)

Dissemination and Exploitation Plan

Describe dissemination and communication strategy towards the different audience in collaboration with the JU and Topic Manager Include corporate identity and website 5 years hosting and maintenance if not provided by the JU common website The plan is due at M6 followed by an update as part of the contractual M18 report

Pubblicazioni

Peer reviewed articles (6)

Maximisation of installed net resulting force through multi-level optimisation of an ultra-high bypass ratio engine nacelle

Autori: Andrea Magrini; Denis Buosi; Ernesto Benini
Pubblicato in: Aerospace Science and Technology, Numero 12709638, 2021, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2021.107169

A review of installation effects of ultra-high bypass ratio engines

Autori: Andrea Magrini, Ernesto Benini, Hua-Dong Yao, Jos Postma, Chris Sheaf
Pubblicato in: Progress in Aerospace Sciences, Numero 119, 2020, Pagina/e 100680, ISSN 0376-0421
Editore: Pergamon Press Ltd.
DOI: 10.1016/j.paerosci.2020.100680

Analysis of installation aerodynamics and comparison of optimised configuration of an ultra-high bypass ratio turbofan nacelle

Autori: Andrea Magrini; Denis Buosi; Ernesto Benini
Pubblicato in: Aerospace Science and Technology, Numero 12709638, 2022, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2022.107756

Body Force Model Implementation of Transonic Rotor for Fan/Airframe Simulations

Autori: Andrea Magrini
Pubblicato in: Aerospace; Volume 9; Numero 11; Pages: 725, 2022, ISSN 2226-4310
Editore: MDPI
DOI: 10.3390/aerospace9110725

Aeropropulsive assessment of engine installation at cruise for UHBPR turbofan with body force fan modelling

Autori: Andrea Magrini; Ernesto Benini
Pubblicato in: Aerospace Science and Technology, Numero Volume 132, 108048, 2023, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2022.108048

CFD-Based Analysis of Installed Fuel Consumption and Aerodynamics of Transonic Transport Aircraft during Cruise Flight

Autori: A. Magrini, D. Buosi, F. Poltronieri, E. De Leo, E. Benini
Pubblicato in: Energies, Numero 16(8), 2023, Pagina/e 3323, ISSN 1996-1073
Editore: Multidisciplinary Digital Publishing Institute (MDPI)
DOI: 10.3390/en16083323

Conference proceedings (12)

Computational Evaluation of Turbo and Electric Powered Simulators for Wind Tunnel Tests of Ultra-High Bypass Engines

Autori: Andrea Magrini; Ernesto Benini; Denis Buosi; Frenk Wubben; Sinus Hegen; Jos Postma
Pubblicato in: AIAA Propulsion and Energy 2021, 2021
Editore: AIAA Propulsion and Energy 2021
DOI: 10.2514/6.2021-3555

Propulsion Installation Modelling for geared Ultra-high bypass ratio engine cycle design

Autori: J. Andersson, T. Grönstedt, H.-D. Yao
Pubblicato in: 3rd ECATS Conference: Making Aviation Environmentally Sustainable, 2020, Pagina/e 136-139, ISBN 978-1-910029-58-9
Editore: ECATS

A slug length calculation for a contraction with mean flow between two half cylinders

Autori: W. Na, D. Yang, A. Surendran, S. Boij, A, Morgans, H.-D. Yao
Pubblicato in: Inter-Noise 2022, Numero 21-24 August, Scottish Event Campus, Glasgow, 2022, 2022, Pagina/e 464, ISBN 978-1-906913-42-7
Editore: Inter-Noise

Ultra-high bypass nacelle geometry design space exploration

Autori: Andrea Magrini, Denis Buosi, Ernesto Benini, Christopher Sheaf
Pubblicato in: AIAA Scitech 2021 Forum, 2021
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2021-0990

Analysis of Ultra-High Bypass Ratio Turbofan Nacelle Geometries With Conventional and Short Intakes at Take-Off and Cruise

Autori: Andrea Magrini; Denis Bousi; Ernesto Benini
Pubblicato in: Proceedings of the ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition, Numero Volume 10C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions. Rotterdam, Netherlands. June 13–17, 2022, 2022
Editore: ASME
DOI: 10.1115/gt2022-81912

Comparison of nacelle models for the evaluation of an ultra-high bypass engine aerodynamics

Autori: A. Magrini, D. Buosi, E. Benini
Pubblicato in: AIAA SciTech Forum 2022, 2022
Editore: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0205

Comparison of engine models of UHBPR turbofan at high incidence

Autori: A. Magrini, G. Subbian, D. Buosi, S. Spinner, E. Benini, R. Radespiel
Pubblicato in: 2023
Editore: AIAA SciTech Forum
DOI: 10.2514/6.2023-1653

Investigation of HL-CRM aerodynamics with a UHBPR nacelle in powered-on condition

Autori: G. Subbian, A. Magrini, D. Buosi, R. Radespiel
Pubblicato in: AIAA Propulsion and Energy 2021, 2021
Editore: AIAA Propulsion and Energy 2021
DOI: 10.2514/6.2021-3547

Installed performance of ultra-high bypass turbofans: estimation of power saving in optimised configurations

Autori: D. Buosi, A. Magrini, E. Benini
Pubblicato in: AIAA SciTech Forum 2022, 2022
Editore: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0208

Installation effects on engine design

Autori: X. Li, H.-D. Yao
Pubblicato in: 3rd ECATS Conference: Making Aviation Environmentally Sustainable, 2020, Pagina/e 151-157, ISBN 978-1-910029-58-9
Editore: 3rd ECATS Conference: Making Aviation Environmentally Sustainable

Assessment of engine modelling on the installed aerodynamics of an ultra-high bypass turbofan

Autori: A. Magrini, D. Buosi, E. Benini
Pubblicato in: AIAA SciTech Forum 2022, 2022
Editore: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0206

RANS Analysis of HL-CRM at Landing Configuration with different Flap Deflections and Engine Representations

Autori: G. Subbian, A. Magrini, E. Benini, D. Buosi, R. Ponza, R. Radespiel
Pubblicato in: AIAA SciTech Forum 2022, 2022
Editore: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0048