Zobrazeno 1 - 10
of 42
pro vyhledávání: '"Mario Tindaro Migliorino"'
Autor:
Manuel Stella, Lucia Zeni, Luca Nichelini, Nicolas Bellomo, Daniele Pavarin, Mario Tindaro Migliorino, Marco Fabiani, Daniele Bianchi, Francesco Nasuti, Christian Paravan, Luciano Galfetti, Attilio Cretella, Rocco Carmine Pellegrini, Enrico Cavallini, Francesco Barato
Publikováno v:
Applied Sciences, Vol 14, Iss 13, p 5625 (2024)
Hybrid rockets have very interesting characteristics like simplicity, reliability, safety, thrust modulation, environmental friendliness and lower costs, which make them very attractive for several applications like sounding rockets, small launch veh
Externí odkaz:
https://doaj.org/article/3ab67113fdcc4dce81982b3c33ed6c87
Publikováno v:
Aerospace, Vol 8, Iss 8, p 213 (2021)
Hybrid rockets are considered a promising future propulsion alternative for specific applications to solid or liquid rockets. In order to raise their technology readiness level, it is important to perform predictive numerical simulations of their int
Externí odkaz:
https://doaj.org/article/6a59657ecb604ba8af2b324bcf9222d1
Autor:
Mario Tindaro Migliorino, Giorgio Gubernari, Daniele Bianchi, Francesco Nasuti, Daniele Cardillo, Francesco Battista
Publikováno v:
Journal of Propulsion and Power. :1-15
Reynolds-averaged Navier–Stokes simulations with submodels of turbulence, chemistry, fluid–surface interaction, and radiation are performed in this work to rebuild the internal ballistics of an experimentally tested hybrid rocket engine with para
Publikováno v:
Journal of Spacecraft and Rockets. 59:1574-1591
Autor:
Mario Tindaro Migliorino, Giorgio Gubernari, Daniele Bianchi, Francesco Nasuti, Daniele Cardillo, Francesco Battista, Simone Pizzurro, Marco Pizzarelli, Rocco Carmine Pellegrini, Enrico Cavallini
Publikováno v:
AIAA SCITECH 2023 Forum.
Autor:
Mario Tindaro Migliorino, Marco Fabiani, Daniele Bianchi, Francesco Nasuti, Francesco Barato, Nicolas Bellomo, Daniele Pavarin, Simone Pizzurro, Marco Pizzarelli, Rocco Carmine Pellegrini, Enrico Cavallini
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
The prediction of wall heat flux at the nozzle throat is of paramount importance in liquid rocket engine (LRE) design for both sizing and safety purposes. Computational fluid dynamics (CFD) simulations can aid in the prediction, provided that they ca
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::213fa9d09185c01bc636f51123b5d402
https://hdl.handle.net/11573/1651305
https://hdl.handle.net/11573/1651305