Installed adVAnced Nacelle uHbr Optimisation and Evaluation

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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

Publications

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

Auteurs: Andrea Magrini; Denis Buosi; Ernesto Benini
Publié dans: Aerospace Science and Technology, Numéro 12709638, 2021, ISSN 1270-9638
Éditeur: Elsevier BV
DOI: 10.1016/j.ast.2021.107169

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

Auteurs: Andrea Magrini, Ernesto Benini, Hua-Dong Yao, Jos Postma, Chris Sheaf
Publié dans: Progress in Aerospace Sciences, Numéro 119, 2020, Page(s) 100680, ISSN 0376-0421
Éditeur: 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

Auteurs: Andrea Magrini; Denis Buosi; Ernesto Benini
Publié dans: Aerospace Science and Technology, Numéro 12709638, 2022, ISSN 1270-9638
Éditeur: Elsevier BV
DOI: 10.1016/j.ast.2022.107756

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

Auteurs: Andrea Magrini
Publié dans: Aerospace; Volume 9; Numéro 11; Pages: 725, 2022, ISSN 2226-4310
Éditeur: MDPI
DOI: 10.3390/aerospace9110725

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

Auteurs: Andrea Magrini; Ernesto Benini
Publié dans: Aerospace Science and Technology, Numéro Volume 132, 108048, 2023, ISSN 1270-9638
Éditeur: 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

Auteurs: A. Magrini, D. Buosi, F. Poltronieri, E. De Leo, E. Benini
Publié dans: Energies, Numéro 16(8), 2023, Page(s) 3323, ISSN 1996-1073
Éditeur: Multidisciplinary Digital Publishing Institute (MDPI)
DOI: 10.3390/en16083323

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

Auteurs: Andrea Magrini; Ernesto Benini; Denis Buosi; Frenk Wubben; Sinus Hegen; Jos Postma
Publié dans: AIAA Propulsion and Energy 2021, 2021
Éditeur: AIAA Propulsion and Energy 2021
DOI: 10.2514/6.2021-3555

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

Auteurs: J. Andersson, T. Grönstedt, H.-D. Yao
Publié dans: 3rd ECATS Conference: Making Aviation Environmentally Sustainable, 2020, Page(s) 136-139, ISBN 978-1-910029-58-9
Éditeur: ECATS

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

Auteurs: W. Na, D. Yang, A. Surendran, S. Boij, A, Morgans, H.-D. Yao
Publié dans: Inter-Noise 2022, Numéro 21-24 August, Scottish Event Campus, Glasgow, 2022, 2022, Page(s) 464, ISBN 978-1-906913-42-7
Éditeur: Inter-Noise

Ultra-high bypass nacelle geometry design space exploration

Auteurs: Andrea Magrini, Denis Buosi, Ernesto Benini, Christopher Sheaf
Publié dans: AIAA Scitech 2021 Forum, 2021
Éditeur: 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

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

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

Auteurs: A. Magrini, D. Buosi, E. Benini
Publié dans: AIAA SciTech Forum 2022, 2022
Éditeur: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0205

Comparison of engine models of UHBPR turbofan at high incidence

Auteurs: A. Magrini, G. Subbian, D. Buosi, S. Spinner, E. Benini, R. Radespiel
Publié dans: 2023
Éditeur: AIAA SciTech Forum
DOI: 10.2514/6.2023-1653

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

Auteurs: G. Subbian, A. Magrini, D. Buosi, R. Radespiel
Publié dans: AIAA Propulsion and Energy 2021, 2021
Éditeur: 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

Auteurs: D. Buosi, A. Magrini, E. Benini
Publié dans: AIAA SciTech Forum 2022, 2022
Éditeur: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0208

Installation effects on engine design

Auteurs: X. Li, H.-D. Yao
Publié dans: 3rd ECATS Conference: Making Aviation Environmentally Sustainable, 2020, Page(s) 151-157, ISBN 978-1-910029-58-9
Éditeur: 3rd ECATS Conference: Making Aviation Environmentally Sustainable

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

Auteurs: A. Magrini, D. Buosi, E. Benini
Publié dans: AIAA SciTech Forum 2022, 2022
Éditeur: 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

Auteurs: G. Subbian, A. Magrini, E. Benini, D. Buosi, R. Ponza, R. Radespiel
Publié dans: AIAA SciTech Forum 2022, 2022
Éditeur: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0048

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