Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Boscagli, Luca"'
Publikováno v:
In Aerospace Science and Technology December 2024 155 Part 2
Autor:
Boscagli, Luca, Sabnis, Kshitij, MacManus, David G., Babinsky, Holger, Tejero, Fernando, Sheaf, Christopher
Publikováno v:
In International Journal of Heat and Fluid Flow October 2024 109
Publikováno v:
In Aerospace Science and Technology October 2022 129
Akademický článek
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Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Autor:
Swarthout, Avery E., MacManus, David G., Tejero, Fernando, Matesanz García, Jesús, Goulos, Ioannis, Boscagli, Luca, Sheaf, Christopher T.
Next generation ultra-high bypass ratio turbofans may have larger fan diameters than the previous generation of aircraft engines. This will potentially increase the nacelle diameter and may incur penalties to the weight and drag of the powerplant. To
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od________70::a11df0264d6aa25e7291c838d1182225
https://dspace.lib.cranfield.ac.uk/handle/1826/19927
https://dspace.lib.cranfield.ac.uk/handle/1826/19927
Autor:
Boscagli, Luca, Tejero, Fernando, Swarthout, Avery, MacManus, David G., Sabnis, Kshitij, Babinsky, Holger, Sheaf, Christopher T.
Aero-engine nacelles are typically designed to fulfil both design and off-design aircraft manoeuvres. Under-off design conditions one of the objective is to avoid large flow separation either on the external cowl or within the intake that can influen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od________70::4ff7ef639b8616c87abcd074f4758965
https://dspace.lib.cranfield.ac.uk/handle/1826/19825
https://dspace.lib.cranfield.ac.uk/handle/1826/19825
Autor:
Tejero, Fernando, MacManus, David, Matesanz García, Jesús, Boscagli, Luca, Hueso Rebassa, Josep, Sheaf, Christopher T.
Computational fluid dynamics (CFD) methods have been widely used for the design and optimisation of complex non-linear systems. Within this context, the overall process can typically have a large computational overhead. For preliminary design studies
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od________70::22be363bf13667e9f5f12afc85e24a2f
https://dspace.lib.cranfield.ac.uk/handle/1826/19822
https://dspace.lib.cranfield.ac.uk/handle/1826/19822
When a civil aircraft engine is shut down during the cruise phase of flight and thus begins to windmill, a supersonic region forms on the external surface of the fan cowl. The terminating normal shock can separate the turbulent boundary layer develop
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b83a5d090f27695167251a7181d73ce1
Autor:
Sabnis, Kshitij, Boscagli, Luca, Swarthout, Avery, Tejero Embuena, Fernando, Babinsky, Holger, David, MacManus, Sheaf, Christopher
Ultra high-bypass ratio aircraft engines adopt slim fan cowl profiles which are sensitive to separation on their external surfaces under diversion windmilling conditions, when engine shutdown occurs during cruise. A two-dimensional wind tunnel rig is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::edb106198d3bceec55bf72168986f702
https://dspace.lib.cranfield.ac.uk/handle/1826/19260
https://dspace.lib.cranfield.ac.uk/handle/1826/19260