Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Parviz Abdullayev"'
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 17, Iss 2, Pp 89-106 (2024)
The priority technological direction of thermal protection of hot section components, basically turbine parts is the development of thermal barrier coatings (TBCs) in order to improve the operational performance of aero gas turbine engines (GTEs). Th
Externí odkaz:
https://doaj.org/article/8b2b4fa75d1540cd833c9560a95ecb97
Autor:
Nijat Abdulla, Parviz Abdullayev
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 16, Iss 1, Pp 15-40 (2023)
Combustion and flow thermogasdynamics is one of the most sophisticated computational stages in liquid rocket engine (LRE) design. A considerable amount of different methodologies used to conduct the thermogasdynamic analysis of the combustion and flo
Externí odkaz:
https://doaj.org/article/b4baee2be8a14e3ab35ab9c21b8645d3
Publikováno v:
Aviation, Vol 12, Iss 4 (2008)
In this paper, it is shown that the use of probability‐statistic methods, especially at the early stage of diagnosing the technical condition of aviation gas turbine engines (GTE) when the flight information has fuzzy and limitation and uncertainty
Externí odkaz:
https://doaj.org/article/633b3f1d23974c8eae481ac6744e9c00
Autor:
Parviz Abdullayev
Publikováno v:
Scopus-Elsevier
* Head of "Design and Maintenance of Aircrafts and Aviation Engines" department, D.Ph. (Eng), Ass. Prof. In this paper is shown the efficiency of the new So ft Computing technology application at different diagnosing stages of aviation Gas Turbine En
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::83522d1e3afa35c19c3a8d59a1d39492
http://www.scopus.com/inward/record.url?eid=2-s2.0-77957852342&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-77957852342&partnerID=MN8TOARS
