Zobrazeno 1 - 10
of 50
pro vyhledávání: '"Roberto Marsilio"'
Publikováno v:
Fluids, Vol 9, Iss 8, p 179 (2024)
The work focuses on the characterization of the flowfield over a truncated linear aerospike by combining theoretical grounds, numerical simulations and experimental tests. The experimental investigations are carried out on a test rig designed at Poli
Externí odkaz:
https://doaj.org/article/a075e1170c1141cfabbb4465304d190b
Publikováno v:
Fluids, Vol 9, Iss 6, p 131 (2024)
Vortices belong to the most important phenomena in fluid dynamics and play an essential role in many engineering applications. They can act detrimentally by harnessing the flow energy and reducing the efficiency of an aerodynamic device, whereas in o
Externí odkaz:
https://doaj.org/article/480798d68879446d8ecd3efe20d38d8a
Publikováno v:
Fluids, Vol 6, Iss 12, p 441 (2021)
The application of the Shock Vector Control (SVC) approach to an axysimmetric supersonic nozzle is studied numerically. SVC is a Fluidic Thrust Vectoring (FTV) strategy that is applied to fixed nozzles in order to realize jet-vectoring effects normal
Externí odkaz:
https://doaj.org/article/f4717813692844f69133b1e635d1df90
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power, Vol 6, Iss 2, p 8 (2021)
Aerospike nozzles represent an interesting solution for Single-Stage-To-Orbit or clustered launchers owing to their self-adapting capability, which can lead to better performance compared to classical nozzles. Furthermore, they can provide thrust vec
Externí odkaz:
https://doaj.org/article/2eccae37946f4c5a9fda4864b560f3b3
Autor:
Valentin Bonnet, Francesca Ortone, Gaetano Maria Di Cicca, Roberto Marsilio, Michele Ferlauto
Publikováno v:
2022 IEEE 9th International Workshop on Metrology for AeroSpace (MetroAeroSpace).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1652a9c986e7a47f21d85708d9782cef
https://doi.org/10.1109/metroaerospace54187.2022.9855979
https://doi.org/10.1109/metroaerospace54187.2022.9855979
Publikováno v:
AIAA AVIATION 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::60a0bfbe652e153bdb0a4b0738e9ae08
https://doi.org/10.2514/6.2022-3262
https://doi.org/10.2514/6.2022-3262
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power
Volume 6
Issue 2
International Journal of Turbomachinery, Propulsion and Power, Vol 6, Iss 8, p 8 (2021)
Volume 6
Issue 2
International Journal of Turbomachinery, Propulsion and Power, Vol 6, Iss 8, p 8 (2021)
Aerospike nozzles represent an interesting solution for Single-Stage-To-Orbit or clustered launchers owing to their self-adapting capability, which can lead to better performance compared to classical nozzles. Furthermore, they can provide thrust vec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e5615dfbf3976b3efe8493051193d9fc
The aerospike nozzle represents an interesting technology for Single-Stage-To-Orbit vehicles because of its self-adapting capability. It is possible to get thrust vectoring capabilities in different ways. A straightforward solution consists in applyi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4e919d1cb51e10546cf435ff01e9ddf2
https://www.scipedia.com/public/Ferlauto_et_al_2021a
https://www.scipedia.com/public/Ferlauto_et_al_2021a
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f19e8e2344e0284e03dac4d4293ca499
https://doi.org/10.2514/6.2020-3777
https://doi.org/10.2514/6.2020-3777
A CFD based approach to the fully three-dimensional simulation of vectored nozzle is presented. The underlying tech- nology used is based on an active flow control technique known as Fluidic Thrust-Vectoring. The flow governing equations are solved b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::de1017ffbc4ed815ad3cee3fb78b71a5
http://hdl.handle.net/11583/2853848
http://hdl.handle.net/11583/2853848