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of 3
pro vyhledávání: '"Вадим Анатольевич Даценко"'
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 7, Pp 21-30 (2019)
The results of mathematical modeling processes in the turboshaft gas turbine engine (GTE) are presented. The using calculation method based on a high-level GTE mathematical model, which is founded on a multi-stage axial compressor blade-to-blade desc
Externí odkaz:
https://doaj.org/article/f70d7d43c002474c983877e8991baa6e
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 4, Pp 70-75 (2017)
The mathematical model of a turbo-shaft engine with a two-stage gas generator was obtained. This model is based on the multi-stage compressor blade – to - blade description, which makes it possible to evaluate the effect of air humidity on its perf
Externí odkaz:
https://doaj.org/article/f62445377d1541d1bcffb278a7ddf3ac