Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Ionut BRINZA"'
Autor:
Andreea BOBONEA, Florin MUNTEANU, Jean-Pierre ROSENBLUM, Catalin NAE, Corneliu STOICA, Mihai Victor PRICOP, Ionut BRINZA
Publikováno v:
INCAS Bulletin, Vol 4, Iss 1, Pp 67-75 (2012)
This paper presents experimental results obtained with passive high lift systems using a combination of smart flap kinematics and vortex generators. A mid-scale 2.5D wind tunnel model based on DLR-F15 is tested in INCAS Subsonic Wind Tunnel, swept at
Externí odkaz:
https://doaj.org/article/c14e13e8a6fb47f995f084903d9c9c13
Autor:
Mihai-Victor PRICOP, Ionut BRINZA
Publikováno v:
INCAS Bulletin, Vol 1, Iss 1, Pp 96-97 (2009)
Flow visualization is an important topic in scientific visualization and has been the subject of active research for many years. Typically, data originates from numerical simulations, such as those of computational fluid dynamics, and needs to be ana
Externí odkaz:
https://doaj.org/article/6190a7ca28624e7e99b096d9bde14f63
Autor:
Costin Ioan Cosoiu, Matei-Razvan Georgescu, Catalin Nae, George-Madalin Chitaru, Ionut Brinza
Publikováno v:
2017 International Conference on Energy and Environment (CIEM)
2017 International Conference on Energy and Environment (CIEM), Oct 2017, Bucharest, France. pp.394-398, ⟨10.1109/CIEM.2017.8120851⟩
2017 International Conference on Energy and Environment (CIEM), Oct 2017, Bucharest, France. pp.394-398, ⟨10.1109/CIEM.2017.8120851⟩
Dust or sand heavy environments cause many problems for the aircraft industry due to the impact of fine particles upon equipment lifespan. We created a CFD model and conducted the numerical simulations needed to determine the distribution of a granul
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8522faa1a8ecb54cbd2113b7e12baf54
https://hal.archives-ouvertes.fr/hal-02351576
https://hal.archives-ouvertes.fr/hal-02351576
Autor:
Elie Carafoli, Ionut Brinza, Catalin Nae, Jean-Pierre Rosenblum, Florin Munteanu, Corneliu Stoica, Mihai Victor Pricop, Quai Marcel Dassault, Andreea Bobonea, B-dul Iuliu Maniu
Publikováno v:
INCAS Bulletin, Vol 4, Iss 1, Pp 67-75 (2012)
This paper presents experimental results obtained with passive high lift systems using a combination of smart flap kinematics and vortex generators. A mid-scale 2.5D wind tunnel model based on DLR-F15 is tested in INCAS Subsonic Wind Tunnel, swept at