Installed adVAnced Nacelle uHbr Optimisation and Evaluation

Project Information

IVANHOE

Grant agreement ID: 863415

DOI

10.3030/863415

Project closed

EC signature date 26 September 2019

Start date 1 October 2019

End date 31 October 2023

Funded under

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Total cost

€ 2 801 779,95

EU contribution

€ 2 801 779,95

Coordinated by

CHALMERS TEKNISKA HOGSKOLA AB
Sweden

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Links to deliverables and publications from FP7 projects, as well as links to some specific result types such as dataset and software, are dynamically retrieved from OpenAIRE .

Deliverables

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

Publications

Peer reviewed articles (6)

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

Author(s): Andrea Magrini; Denis Buosi; Ernesto Benini
Published in: Aerospace Science and Technology, Issue 12709638, 2021, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/j.ast.2021.107169

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

Author(s): Andrea Magrini, Ernesto Benini, Hua-Dong Yao, Jos Postma, Chris Sheaf
Published in: Progress in Aerospace Sciences, Issue 119, 2020, Page(s) 100680, ISSN 0376-0421
Publisher: 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

Author(s): Andrea Magrini; Denis Buosi; Ernesto Benini
Published in: Aerospace Science and Technology, Issue 12709638, 2022, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/j.ast.2022.107756

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

Author(s): Andrea Magrini
Published in: Aerospace; Volume 9; Issue 11; Pages: 725, 2022, ISSN 2226-4310
Publisher: MDPI
DOI: 10.3390/aerospace9110725

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

Author(s): Andrea Magrini; Ernesto Benini
Published in: Aerospace Science and Technology, Issue Volume 132, 108048, 2023, ISSN 1270-9638
Publisher: 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

Author(s): A. Magrini, D. Buosi, F. Poltronieri, E. De Leo, E. Benini
Published in: Energies, Issue 16(8), 2023, Page(s) 3323, ISSN 1996-1073
Publisher: 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

Author(s): Andrea Magrini; Ernesto Benini; Denis Buosi; Frenk Wubben; Sinus Hegen; Jos Postma
Published in: AIAA Propulsion and Energy 2021, 2021
Publisher: AIAA Propulsion and Energy 2021
DOI: 10.2514/6.2021-3555

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

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

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

Author(s): W. Na, D. Yang, A. Surendran, S. Boij, A, Morgans, H.-D. Yao
Published in: Inter-Noise 2022, Issue 21-24 August, Scottish Event Campus, Glasgow, 2022, 2022, Page(s) 464, ISBN 978-1-906913-42-7
Publisher: Inter-Noise

Ultra-high bypass nacelle geometry design space exploration

Author(s): Andrea Magrini, Denis Buosi, Ernesto Benini, Christopher Sheaf
Published in: AIAA Scitech 2021 Forum, 2021
Publisher: 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

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

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

Author(s): A. Magrini, D. Buosi, E. Benini
Published in: AIAA SciTech Forum 2022, 2022
Publisher: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0205

Comparison of engine models of UHBPR turbofan at high incidence

Author(s): A. Magrini, G. Subbian, D. Buosi, S. Spinner, E. Benini, R. Radespiel
Published in: 2023
Publisher: AIAA SciTech Forum
DOI: 10.2514/6.2023-1653

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

Author(s): G. Subbian, A. Magrini, D. Buosi, R. Radespiel
Published in: AIAA Propulsion and Energy 2021, 2021
Publisher: 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

Author(s): D. Buosi, A. Magrini, E. Benini
Published in: AIAA SciTech Forum 2022, 2022
Publisher: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0208

Installation effects on engine design

Author(s): X. Li, H.-D. Yao
Published in: 3rd ECATS Conference: Making Aviation Environmentally Sustainable, 2020, Page(s) 151-157, ISBN 978-1-910029-58-9
Publisher: 3rd ECATS Conference: Making Aviation Environmentally Sustainable

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

Author(s): A. Magrini, D. Buosi, E. Benini
Published in: AIAA SciTech Forum 2022, 2022
Publisher: 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

Author(s): G. Subbian, A. Magrini, E. Benini, D. Buosi, R. Ponza, R. Radespiel
Published in: AIAA SciTech Forum 2022, 2022
Publisher: AIAA SciTech Forum 2022
DOI: 10.2514/6.2022-0048