Advance Nacelle Aerodynamic Optimisation

Información del proyecto

ANACO

Identificador del acuerdo de subvención: 820997

DOI 10.3030/820997

Proyecto cerrado

Fecha de la firma de la CE 10 Octubre 2018

Fecha de inicio 1 Noviembre 2018

Fecha de finalización 30 Noviembre 2022

Financiado con arreglo a

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Coste total € 2 257 998,75

Aportación de la UE € 2 257 998,75

Coordinado por

AIRCRAFT RESEARCH ASSOCIATION LIMITED
United Kingdom

Publicaciones

Conference proceedings (5)

Robust Aerodynamic Design of Nacelles for Future Civil Aero-Engines

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

Optimization of installed compact and robust nacelles using surrogate models

Autores: Sanchez-Moreno F, MacManus D, Hueso-Rebassa J, Tejero F & Sheaf C
Publicado en: ICAS 2022: 33rd Congress of the International Council of the Aeronautical Sciences, Edición 4-9 September 2022, 2022, Página(s) Paper ICAS2022_0167
Editor: ICAS

Robustness of optimisation algorithms for transonic aerodynamic design

Autores: Sanchez-Moreno F, MacManus D, Tejero F, Matesanz-Garcia J & Sheaf C
Publicado en: 9th European Conference for Aeronautics and Space Sciences (EUCASS-3AF 2022), Edición 27 June - 1 July 2022, 2022
Editor: EUCASS-3AF

Transonic nacelle design for future medium range aero-engines

Autores: Schreiner BDJ, MacManus DG, Tejero F, Sanchez-Moreno F & Sheaf C
Publicado en: ICAS 2022: 33rd Congress of the International Council of the Aeronautical Sciences, Edición 4-9 September 2022, 2022, Página(s) Paper ICAS2022_0380
Editor: ICAS

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

Autores: Tejero F, MacManus D, Hueso-Rebassa J, Sanchez-Moreno F, Goulos I & Sheaf C
Publicado en: AERO2022: 56th 3AF International Conference on Applied Aerodynamics, Edición 28-30 March 2022, 2023
Editor: 3AF

Peer reviewed articles (2)

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

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

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

Autores: Tejero F, MacManus DG, Sanchez-Moreno F, Sheaf C
Publicado en: Aerospace Science and Technology, Edición Vol 136, 2023, Página(s) Article 108208, ISSN 1626-3219
Editor: Elsevier Masson SAS
DOI: 10.1016/j.ast.2023.108208