Robust Aerodynamic Design of Nacelles for Future Civil Aero-Engines
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Auteurs:
B. Deneys J. Schreiner, Fernando Tejero, David G. MacManus, Christopher Sheaf
Publié dans:
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition; Volume 1: Aircraft Engine; Fans and Blowers, Numéro September 21–25, 2020 Virtual, Online; published 11 January 2021, 2021, ISBN 978-0-7918-8405-8
Éditeur:
The American Society of Mechanical Engineers
DOI:
10.1115/gt2020-14470
Optimization of installed compact and robust nacelles using surrogate models
Auteurs:
Sanchez-Moreno F, MacManus D, Hueso-Rebassa J, Tejero F & Sheaf C
Publié dans:
ICAS 2022: 33rd Congress of the International Council of the Aeronautical Sciences, Numéro 4-9 September 2022, 2022, Page(s) Paper ICAS2022_0167
Éditeur:
ICAS
Robustness of optimisation algorithms for transonic aerodynamic design
Auteurs:
Sanchez-Moreno F, MacManus D, Tejero F, Matesanz-Garcia J & Sheaf C
Publié dans:
9th European Conference for Aeronautics and Space Sciences (EUCASS-3AF 2022), Numéro 27 June - 1 July 2022, 2022
Éditeur:
EUCASS-3AF
Transonic nacelle design for future medium range aero-engines
Auteurs:
Schreiner BDJ, MacManus DG, Tejero F, Sanchez-Moreno F & Sheaf C
Publié dans:
ICAS 2022: 33rd Congress of the International Council of the Aeronautical Sciences, Numéro 4-9 September 2022, 2022, Page(s) Paper ICAS2022_0380
Éditeur:
ICAS
Aerodynamic optimisation of civil aero-engine nacelles by dimensionality reduction and multi-fidelity techniques
Auteurs:
Tejero F, MacManus D, Hueso-Rebassa J, Sanchez-Moreno F, Goulos I & Sheaf C
Publié dans:
AERO2022: 56th 3AF International Conference on Applied Aerodynamics, Numéro 28-30 March 2022, 2023
Éditeur:
3AF
