Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Александр Евгеньевич Демин"'
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 1, Pp 18-28 (2019)
Gas Turbine Engine (GTE) operating characteristics such as thrust (or power), specific fuel consumption and other cycle parameters on different regimes, can be determined by engine modeling and applying correspondent calculation method. Its accuracy
Externí odkaz:
https://doaj.org/article/6e3bed4ee361430ca3cc1e60e54d51b0
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 6, Pp 34-44 (2020)
The implementation of the high requirements for modern gas turbine engines depends on the perfection of their components. The reliability of the engine operation is largely determined by the compressor gas-dynamic stability margin. In this paper, a r
Externí odkaz:
https://doaj.org/article/4fe60fbaaca441c6bf84c7fbff1f8d30
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 6, Pp 58-64 (2017)
In developing of methods for diagnostic based on the parameters of the working process of the flow-through part of aviation gas turbine engines, the development of the working process thermogasdynamic model for the engine is the main task. Math model
Externí odkaz:
https://doaj.org/article/ff76a7dba11846f9a358b48833bd4999