Advance Nacelle Aerodynamic Optimisation

Informazioni relative al progetto

ANACO

ID dell’accordo di sovvenzione: 820997

DOI 10.3030/820997

Progetto chiuso

Data della firma CE 10 Ottobre 2018

Data di avvio 1 Novembre 2018

Data di completamento 30 Novembre 2022

Finanziato da

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Costo totale € 2 257 998,75

Contributo UE € 2 257 998,75

Coordinato da

AIRCRAFT RESEARCH ASSOCIATION LIMITED
United Kingdom

Pubblicazioni

Conference proceedings (5)

Robust Aerodynamic Design of Nacelles for Future Civil Aero-Engines

Autori: B. Deneys J. Schreiner, Fernando Tejero, David G. MacManus, Christopher Sheaf
Pubblicato in: ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition; Volume 1: Aircraft Engine; Fans and Blowers, Numero September 21–25, 2020 Virtual, Online; published 11 January 2021, 2021, ISBN 978-0-7918-8405-8
Editore: The American Society of Mechanical Engineers
DOI: 10.1115/gt2020-14470

Optimization of installed compact and robust nacelles using surrogate models

Autori: Sanchez-Moreno F, MacManus D, Hueso-Rebassa J, Tejero F & Sheaf C
Pubblicato in: ICAS 2022: 33rd Congress of the International Council of the Aeronautical Sciences, Numero 4-9 September 2022, 2022, Pagina/e Paper ICAS2022_0167
Editore: ICAS

Robustness of optimisation algorithms for transonic aerodynamic design

Autori: Sanchez-Moreno F, MacManus D, Tejero F, Matesanz-Garcia J & Sheaf C
Pubblicato in: 9th European Conference for Aeronautics and Space Sciences (EUCASS-3AF 2022), Numero 27 June - 1 July 2022, 2022
Editore: EUCASS-3AF

Transonic nacelle design for future medium range aero-engines

Autori: Schreiner BDJ, MacManus DG, Tejero F, Sanchez-Moreno F & Sheaf C
Pubblicato in: ICAS 2022: 33rd Congress of the International Council of the Aeronautical Sciences, Numero 4-9 September 2022, 2022, Pagina/e Paper ICAS2022_0380
Editore: ICAS

Aerodynamic optimisation of civil aero-engine nacelles by dimensionality reduction and multi-fidelity techniques

Autori: Tejero F, MacManus D, Hueso-Rebassa J, Sanchez-Moreno F, Goulos I & Sheaf C
Pubblicato in: AERO2022: 56th 3AF International Conference on Applied Aerodynamics, Numero 28-30 March 2022, 2023
Editore: 3AF

Peer reviewed articles (2)

Aerodynamic optimisation of civil aero-engine nacelles by dimensionality reduction and multi-fidelity techniques

Autori: Tejero F, MacManus DG, Hueso-Rebassa J, Sanchez-Moreno F, Goulos I & Sheaf C
Pubblicato in: International Journal of Numerical Methods for Heat and Fluid Flow, Numero 30 Sept 2022, 2022, ISSN 0961-5539
Editore: Emerald Group Publishing Ltd.
DOI: 10.1108/hff-06-2022-0368

Neural network-based multi-point, multi-objective optimisation for transonic applications

Autori: Tejero F, MacManus DG, Sanchez-Moreno F, Sheaf C
Pubblicato in: Aerospace Science and Technology, Numero Vol 136, 2023, Pagina/e Article 108208, ISSN 1626-3219
Editore: Elsevier Masson SAS
DOI: 10.1016/j.ast.2023.108208