Robust Aerodynamic Design of Nacelles for Future Civil Aero-Engines
(si apre in una nuova finestra)
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
