Zobrazeno 1 - 10
of 57
pro vyhledávání: '"Cîrciu, Ionică"'
Autor:
Cîrciu, Ionică, CÎRCIU, Evelina
Publikováno v:
Redefining Community in Intercultural Context. 8(1):177-180
Externí odkaz:
https://www.ceeol.com/search/article-detail?id=874313
Autor:
CÎRCIU, Ionică1 circiuionica@yahoo.co.uk
Publikováno v:
Proceedings of the Scientific Conference AFASES. 2018, Vol. 1, p139-142. 4p.
Publikováno v:
Journal of Defense Resources Management (JoDRM). 5(1):123-128
Externí odkaz:
https://www.ceeol.com/search/article-detail?id=13969
Autor:
CÎRCIU, Ionică1 circiuionica@yahoo.co.uk, PRISACARIU, Vasile1 aerosavelli73@yahoo.com
Publikováno v:
Proceedings of the Scientific Conference AFASES. 2019, p107-112. 6p.
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
Publikováno v:
Journal of Defense Resources Management (JoDRM). 4(1):203-210
Externí odkaz:
https://www.ceeol.com/search/article-detail?id=53935
Publikováno v:
Journal of Defense Resources Management (JoDRM). 1(1):93-100
Externí odkaz:
https://www.ceeol.com/search/article-detail?id=266794
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:
CÎRCIU, Ionică, MIHAI, Eduard
Publikováno v:
Scientific Research & Education in the Air Force - AFASES; 2023, Vol. 2023, p137-141, 5p
Publikováno v:
MATEC Web of Conferences, Vol 121, p 01012 (2017)
Using of the flying wing (the UAVs category) in various fields (civilian and military) determine interests sustained of the aerodynamic and trajectory optimizations. The article presents analysis of wing flying performance (in morphing concept) by st
Externí odkaz:
https://doaj.org/article/00164fef4f114b9fb91fec8f228c3593