Zobrazeno 1 - 10
of 46
pro vyhledávání: '"Fulvio Stella"'
Publikováno v:
AIAA Journal. 61:2314-2318
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::45b40ef081d072f70709fc1e81b8a5df
https://doi.org/10.2514/1.j062554
https://doi.org/10.2514/1.j062554
Autor:
Matteo Cimini, Fulvio Stella, Enrico Cavallini, Andrea di Mascio, Agostino Neri, Emanuele Martelli, Matteo Bernardini
This work aims at investigating the flow dynamics in solid rocket motors (SRMs), which are still of a great interest for space launchers. The internal ballistics of SRMs is generally characterized by the interaction of the hydrodynamic instabilities
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6ba0c87cb75440c9702ab48293b4228a
Autor:
Francesco Salvadore, Emanuele Martelli, Fulvio Stella, Agostino Neri, Andrea Di Mascio, Matteo Bernardini, Matteo Cimini, Enrico Cavallini
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
We explore the potential of the immersed boundary (IB) method to predict pressure oscillations in solid rocket motors (SRM) by performing three-dimensional, high-fidelity simulations of two different configurations, including a small, laboratory-scal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::35bc9d72d9c2aa259920f1bdf1be8e15
https://doi.org/10.2514/6.2021-3696
https://doi.org/10.2514/6.2021-3696
Autor:
Roberto Camussi, D. Barbagallo, C. Stoica, A. Di Marco, Matteo Bernardini, Fulvio Stella, L. Romano, F. De Gregorio, F. Paglia
An extensive wind tunnel test campaign devoted to the characterization of the aerodynamic and aeroacoustic behaviour of the new Space Launcher VEGA-C has been carried out in the trisonic wind tunnel available at the National Institute for Aerospace R
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dfdd83d4f3663ae4f70038d55850f084
https://hdl.handle.net/11590/363631
https://hdl.handle.net/11590/363631
Autor:
A. Di Mascio, Matteo Cimini, Fulvio Stella, Enrico Cavallini, Emanuele Martelli, Matteo Bernardini, Agostino Neri
A three-dimensional high-fidelity numerical simulation of a small-scale solid rocket motor is carried out adopting the implicit large-eddy simulation (ILES) approach to investigate the coupling bet...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a7dd2df429f5ce3257f395dd6d9ddb27
http://hdl.handle.net/11697/150371
http://hdl.handle.net/11697/150371
Autor:
B. Le Naour, Khaled Chetehouna, Nicolas Gascoin, Fulvio Stella, Marc Bouchez, Antonella Ingenito, L. Taddeo
Scramjets engines are suitable to propel high-speed hypersonic vehicles. As flight velocities increase, vehicle thermal protection becomes very critical. In this sense, regenerative cooling is a well-known cooling technique, particularly effective wh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::391690198ace3c511a882c8929f360c4
http://hdl.handle.net/11573/1317725
http://hdl.handle.net/11573/1317725
Autor:
Graham Morrison, Darrell W. Pepper, Patrick Bontoux, Fulvio Stella, Alexander I. Leontiev, Bernard Roux, Brian E. Milton, Tomek Kowalewski, Kemal Hanjalic, Leonid A. Dombrovsky, Guan Yeoh, Ivan Vladimirovich Egorov, Jacques Padet, Lawrence Doctors, Brian Launder, Faruk Arinç, Gordon D. Mallinson, Richard K.K. Yuen, Tianshou Zhao, Yildiz Bayazitoglu, Victoria Timchenko, Richard J Goldstein, John Reizes, Yogesh Jaluria, Terrence W. Simon, Robin Ford
Publikováno v:
International Journal of Heat and Mass Transfer. 152:119486
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d242513bbbb912d8b9b7fb1e5bb8f56c
https://doi.org/10.1016/j.ijheatmasstransfer.2020.119486
https://doi.org/10.1016/j.ijheatmasstransfer.2020.119486
Publikováno v:
Proceeding of THMT-18. Turbulence Heat and Mass Transfer 9 Proceedings of the Ninth International Symposium On Turbulence Heat and Mass Transfer.
An enhanced delayed detached eddy simulation of a shock wave/boundary layer interaction in an over-expanded planar transonic nozzle has been carried out to predict the fundamental features of shock low-frequency unsteadiness. The modification of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a82790fe07356260042c1e38201bde5d
https://doi.org/10.1615/thmt-18.740
https://doi.org/10.1615/thmt-18.740
Autor:
Antonella Ingenito, Bruno Le Naour, Khaled Chetehouna, L. Taddeo, Fulvio Stella, Nicolas Gascoin, Marc Bouchez
Publikováno v:
21st AIAA International Space Planes and Hypersonics Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8bafd0ff5dc82d10588e78671337d371
https://doi.org/10.2514/6.2017-2126
https://doi.org/10.2514/6.2017-2126