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Installed adVAnced Nacelle uHbr Optimisation and Evaluation

Rezultaty

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

Publikacje

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

Autorzy: Andrea Magrini; Denis Buosi; Ernesto Benini
Opublikowane w: Aerospace Science and Technology, Numer 12709638, 2021, ISSN 1270-9638
Wydawca: Elsevier BV
DOI: 10.1016/j.ast.2021.107169

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

Autorzy: Andrea Magrini, Ernesto Benini, Hua-Dong Yao, Jos Postma, Chris Sheaf
Opublikowane w: Progress in Aerospace Sciences, Numer 119, 2020, Strona(/y) 100680, ISSN 0376-0421
Wydawca: 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

Autorzy: Andrea Magrini; Denis Buosi; Ernesto Benini
Opublikowane w: Aerospace Science and Technology, Numer 12709638, 2022, ISSN 1270-9638
Wydawca: Elsevier BV
DOI: 10.1016/j.ast.2022.107756

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

Autorzy: Andrea Magrini
Opublikowane w: Aerospace; Volume 9; Numer 11; Pages: 725, 2022, ISSN 2226-4310
Wydawca: MDPI
DOI: 10.3390/aerospace9110725

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

Autorzy: Andrea Magrini; Ernesto Benini
Opublikowane w: Aerospace Science and Technology, Numer Volume 132, 108048, 2023, ISSN 1270-9638
Wydawca: 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

Autorzy: A. Magrini, D. Buosi, F. Poltronieri, E. De Leo, E. Benini
Opublikowane w: Energies, Numer 16(8), 2023, Strona(/y) 3323, ISSN 1996-1073
Wydawca: 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

Autorzy: Andrea Magrini; Ernesto Benini; Denis Buosi; Frenk Wubben; Sinus Hegen; Jos Postma
Opublikowane w: AIAA Propulsion and Energy 2021, 2021
Wydawca: AIAA Propulsion and Energy 2021
DOI: 10.2514/6.2021-3555

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

Autorzy: J. Andersson, T. Grönstedt, H.-D. Yao
Opublikowane w: 3rd ECATS Conference: Making Aviation Environmentally Sustainable, 2020, Strona(/y) 136-139, ISBN 978-1-910029-58-9
Wydawca: ECATS

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

Autorzy: W. Na, D. Yang, A. Surendran, S. Boij, A, Morgans, H.-D. Yao
Opublikowane w: Inter-Noise 2022, Numer 21-24 August, Scottish Event Campus, Glasgow, 2022, 2022, Strona(/y) 464, ISBN 978-1-906913-42-7
Wydawca: Inter-Noise

Ultra-high bypass nacelle geometry design space exploration

Autorzy: Andrea Magrini, Denis Buosi, Ernesto Benini, Christopher Sheaf
Opublikowane w: AIAA Scitech 2021 Forum, 2021
Wydawca: 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

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

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

Autorzy: A. Magrini, D. Buosi, E. Benini
Opublikowane w: AIAA SciTech Forum 2022, 2022
Wydawca: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0205

Comparison of engine models of UHBPR turbofan at high incidence

Autorzy: A. Magrini, G. Subbian, D. Buosi, S. Spinner, E. Benini, R. Radespiel
Opublikowane w: 2023
Wydawca: AIAA SciTech Forum
DOI: 10.2514/6.2023-1653

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

Autorzy: G. Subbian, A. Magrini, D. Buosi, R. Radespiel
Opublikowane w: AIAA Propulsion and Energy 2021, 2021
Wydawca: 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

Autorzy: D. Buosi, A. Magrini, E. Benini
Opublikowane w: AIAA SciTech Forum 2022, 2022
Wydawca: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0208

Installation effects on engine design

Autorzy: X. Li, H.-D. Yao
Opublikowane w: 3rd ECATS Conference: Making Aviation Environmentally Sustainable, 2020, Strona(/y) 151-157, ISBN 978-1-910029-58-9
Wydawca: 3rd ECATS Conference: Making Aviation Environmentally Sustainable

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

Autorzy: A. Magrini, D. Buosi, E. Benini
Opublikowane w: AIAA SciTech Forum 2022, 2022
Wydawca: 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

Autorzy: G. Subbian, A. Magrini, E. Benini, D. Buosi, R. Ponza, R. Radespiel
Opublikowane w: AIAA SciTech Forum 2022, 2022
Wydawca: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0048

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