Zobrazeno 1 - 10
of 102
pro vyhledávání: '"Rotaru, Constantin"'
Autor:
ROTARU, Constantin1 rotaru.constantin@afahc.ro
Publikováno v:
Proceedings of the Scientific Conference AFASES. 2019, p184-193. 10p.
Publikováno v:
MATEC Web of Conferences, Vol 290, p 04009 (2019)
PDE propulsion can work from a subsonic regime to hypersonic regimes; this type of engine can have higher thermodynamic efficiency compared to other turbojet or turbofan engines due to the removal of rotating construction elements (compressors and tu
Externí odkaz:
https://doaj.org/article/2211ca6433b24375a04f4bae70ec9bb6
Autor:
Cîrciu Ionică, Rotaru Constantin
Publikováno v:
MATEC Web of Conferences, Vol 290, p 06003 (2019)
The Coandă Effect, or better said, the deviation of fluid jets to stay attached to a convex surface is a complex gas-dynamic effect, named after the Romanian aviation engineer Henri Coandă and it was for the first time highlighted by him in 1910 du
Externí odkaz:
https://doaj.org/article/1a831825628d411cbae56c3e8bc08c32
Autor:
Rotaru, Constantin
Publikováno v:
Studii de securitate publică / Public Security Studies. (1):13-21
Externí odkaz:
https://www.ceeol.com/search/article-detail?id=36679
Autor:
Rotaru, Constantin
Publikováno v:
Studii de securitate publică / Public Security Studies. (1):209-215
Externí odkaz:
https://www.ceeol.com/search/article-detail?id=36663
Autor:
ROTARU, Constantin1 rotaru.constantin@afahc.ro, TANASE, Janel1, CIUIC, Oliver1, MIHAI, Eduard1
Publikováno v:
Proceedings of the Scientific Conference AFASES. 2018, Vol. 1, p233-238. 6p.
Publikováno v:
MATEC Web of Conferences, Vol 234, p 01001 (2018)
A pulse detonation engine (PDE) is a type of propulsion system that uses detonation waves to combust the fuel and oxidizer mixture. The engine is pulsed because the mixture must be renewed in the combustor between each detonation wave. Theoretically,
Externí odkaz:
https://doaj.org/article/0a5143150cc44c2e97101600fbca53bc
Autor:
ANDREI, Irina-Carmen1 andrei.irina@incas.ro, ROTARU, Constantin2 rotaru.constantin@yahoo.com, FADGYAS, Maria-Cristina1, STROE, Gabriela3 ing.Stroe@yaoo.com, NICULESCU, Mihai Leonida1 niculescu.mihai@incas.ro
Publikováno v:
Proceedings of the Scientific Conference AFASES. 2017, Vol. 1, p35-48. 14p.
Autor:
ANDREI, Irina-Carmen1 andrei.irina@incas.ro, ROTARU, Constantin2 rotaru.constantin@yahoo.com, FADGYAS, Maria-Cristina1, STROE, Gabriela3 ing.Stroe@yaoo.com, NICULESCU, Mihai Leonida1 niculescu.mihai@incas.ro
Publikováno v:
Proceedings of the Scientific Conference AFASES. 2017, Vol. 1, p23-34. 12p.
Autor:
Rotaru Constantin
Publikováno v:
MATEC Web of Conferences, Vol 133, p 01008 (2017)
The paper presents some results regarding the identification of a turbojet engine’s optimal combustion chamber geometry, characterized by small dimensions, with enhanced possibilities for air and fuel mixture circulation in the primary combustion z
Externí odkaz:
https://doaj.org/article/f8de1dc99dbf45c2b395a3cf55e6f719