Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Yu. A. Ezrokhi"'
Publikováno v:
Russian Aeronautics. 65:361-367
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::478d305f044f67c09a36ca97b7f82c3e
https://doi.org/10.3103/s1068799822020143
https://doi.org/10.3103/s1068799822020143
Autor:
E. A. Khoreva, Yu. A. Ezrokhi
Publikováno v:
Mechanical Engineering and Computer Science. :19-30
The paper considers techniques to develop a mathematical model using a method of «parallel compressors». The model is intended to estimate the impact of the air inlet distortion on the primary parameters of the aero-engine. The paper presents rated
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::179147ea889a82cc54865e611544e290
https://doi.org/10.24108/0118.0001360
https://doi.org/10.24108/0118.0001360
Autor:
Yu. A. Ezrokhi, E. A. Khoreva
Publikováno v:
Aèrokosmičeskij Naučnyj Žurnal, Vol 3, Iss 3, Pp 1-19 (2017)
The paper considers methodological approaches to the mathematical models (MM) of various levels, dedicated to estimate an impact of the entrance flow heterogeneity on the main parameters and performances of the aviation GTE and it units. By an exampl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doajarticles::d46babb96eeb43e053097561f021a179
https://aerospace.elpub.ru/jour/article/view/64
https://aerospace.elpub.ru/jour/article/view/64
Autor:
Yu. A. Ezrokhi, E. A. Khoreva
Publikováno v:
Aèrokosmičeskij Naučnyj Žurnal, Vol 3, Iss 2, Pp 34-47 (2017)
The article describes high-level mathematical models developed to solve special problems arising at later stages of design with regard to calculation of the aircraft gas turbine engine (GTE) under real operating conditions. The use of blade row mathe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doajarticles::976b1310d457d5557cb833bc1e3a5cca
https://aerospace.elpub.ru/jour/article/view/61
https://aerospace.elpub.ru/jour/article/view/61
Publikováno v:
Nauka i Obrazovanie, Vol 0, Iss 3, Pp 116-136 (2017)
Based on the analysis results from the patent search and review of domestic and foreign publications in variable cycle engines (VCE) was created a classification of the possible schematic diagrams of VCE realizing three-stream engine technologies (th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8997f8bae6551c4dd839c9dcd9a63ef5
https://doi.org/10.7463/0317.0000964
https://doi.org/10.7463/0317.0000964
Autor:
E. A. Khoreva, Yu. A. Ezrokhi
Publikováno v:
Aèrokosmičeskij Naučnyj Žurnal, Vol 3, Iss 1, Pp 1-14 (2017)
The paper presents the analytical review results of the ordinary mathematical models of the operating process used to study aviation GTE parameters and characteristics at all stages of its creation and operation. Considers the mathematical models of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doajarticles::7497d57cc3257236afffef9e1d61ac3c
https://aerospace.elpub.ru/jour/article/view/59
https://aerospace.elpub.ru/jour/article/view/59