Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Razvan NICOARA"'
Publikováno v:
Aerospace, Vol 10, Iss 11, p 928 (2023)
As a main component of most gas-turbine engines, the axial flow turbines have been in a process of continuous improvement, reaching high efficiencies and reliability. A well-known drawback of these systems is the rapid decrease in performance when op
Externí odkaz:
https://doaj.org/article/3f3cd8e2e8ea47da9083ee593695b38b
Autor:
Emilia PRISACARIU, Tudor PRISECARU, Valeriu VILAG, Cosmin SUCIU, Cristian DOBROMIRESCU, Marius ENACHE, Razvan NICOARA
Publikováno v:
INCAS Bulletin, Vol 13, Iss 3, Pp 113-122 (2021)
In general, the Schlieren visualization method is used to qualitatively describe phenomena. However, recent studies have attempted to convert the classical Schlieren system into a quantitative method to describe certain flow parameters. This paper ai
Externí odkaz:
https://doaj.org/article/fbd77946606f45d9b68ca2151cc1990b
Autor:
Valeriu Vilag, Emilia Prisacariu, Marius Enache, Cristian Dobromirescu, Cosmin Suciu, Razvan Nicoara, Tudor Prisecaru
Publikováno v:
INCAS Bulletin, Vol 13, Iss 3, Pp 113-122 (2021)
In general, the Schlieren visualization method is used to qualitatively describe phenomena. However, recent studies have attempted to convert the classical Schlieren system into a quantitative method to describe certain flow parameters. This paper ai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ee45abb53682f759f6b194d12466ed4f
https://doi.org/10.13111/2066-8201.2021.13.3.10
https://doi.org/10.13111/2066-8201.2021.13.3.10
Publikováno v:
International Journal of Aeronautical and Space Sciences. 22:359-365
During service, a turbine engine undergoes frequently dynamic operations. Because of the changes in mass flow, temperature, pressure, as well as the different reaction of the components of turbine to these changes, the turbine performances may vary s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ffd89f3a82e2072bc5bc1b6564774559
https://doi.org/10.1007/s42405-020-00312-4
https://doi.org/10.1007/s42405-020-00312-4
Publikováno v:
Lecture Notes in Electrical Engineering ISBN: 9783030215064
In the context of developing a propulsion system for small-scale space platforms, particularly CubeSats, currently treated as secondary payload, several challenges are raised by designing an experimental installation dedicated to testing a H2/O2 thru
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c647e191f6f2632669917d93a8ee0324
https://doi.org/10.1007/978-3-030-21507-1_2
https://doi.org/10.1007/978-3-030-21507-1_2
Publikováno v:
Aerospace (MDPI Publishing); Nov2023, Vol. 10 Issue 11, p928, 16p
Publikováno v:
International Journal of Aeronautical & Space Sciences; Apr2021, Vol. 22 Issue 2, p359-365, 7p
Publikováno v:
AIP Conference Proceedings; 2019, Vol. 2164 Issue 1, p070003-1-070003-10, 10p, 4 Diagrams, 4 Charts, 1 Graph