Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Ilia N. Krupenich"'
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 235:2014-2021
Development of a gas turbine engine starts with optimization of the working process parameters. Turbine inlet temperature is among the most influential parameters that largely determine performance of an engine. As typical turbine inlet temperatures
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d088ad12d745f63f8e16d8d3aa067fc8
https://doi.org/10.1177/09576509211014981
https://doi.org/10.1177/09576509211014981
Publikováno v:
2020 International Multi-Conference on Industrial Engineering and Modern Technologies (FarEastCon).
Finding the right engine for a given aircraft is a complicated task itself. Small-scale engines feature extra complexity as the Reynolds number is an additional factor that impacts their efficiency and is to be taken into the account during the optim
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29631328b6d72af4f6482df47027f365
https://doi.org/10.1109/fareastcon50210.2020.9271150
https://doi.org/10.1109/fareastcon50210.2020.9271150
Publikováno v:
2020 International Multi-Conference on Industrial Engineering and Modern Technologies (FarEastCon).
Further improvement of engines' efficiency is becoming increasingly challenging, especially for small-scale gas turbines. A promising approach to achieve this goal is to combine engine's structural optimization with a parametric optimization of its w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a20b063ad8f37ec413504a4385f5f243
https://doi.org/10.1109/fareastcon50210.2020.9271481
https://doi.org/10.1109/fareastcon50210.2020.9271481
Publikováno v:
Russian Aeronautics. 61:78-83
This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::17d6f871a14cf0c8254db6f9171f0f6c
https://doi.org/10.3103/s1068799818010129
https://doi.org/10.3103/s1068799818010129
Autor:
Ilia N. Krupenich, V. S. Kuz'michev, H H Omar, Yu A Tkachenko, Evgeniy P. Filinov, Ya A Ostapyuk
Publikováno v:
Journal of Physics: Conference Series. 1891:012011
Development of a gas turbine engine starts with optimization of the working process parameters. Turbine inlet temperature is among the most influential parameters that largely determine performance of an engine. As typical turbine inlet temperatures
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::140ce45e3fe7fc516c1364337a202700
https://doi.org/10.1088/1742-6596/1891/1/012011
https://doi.org/10.1088/1742-6596/1891/1/012011
Publikováno v:
International Journal of Mechanical Engineering and Robotics Research. :36-41
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6798d145f68cad69d8aab7ef2c20e938
https://doi.org/10.18178/ijmerr.6.1.36-41
https://doi.org/10.18178/ijmerr.6.1.36-41
Publikováno v:
International Journal of Mechanical Engineering and Robotics Research. :28-35
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c0253fe3fdf5761bf556a11b47401153
https://doi.org/10.18178/ijmerr.6.1.28-35
https://doi.org/10.18178/ijmerr.6.1.28-35
Publikováno v:
SIMULTECH
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2837231e27cd2891e9836fb55865773e
https://doi.org/10.5220/0007948003320337
https://doi.org/10.5220/0007948003320337
Publikováno v:
MATEC Web of Conferences, Vol 220, p 03002 (2018)
The aim of engine control optimization is to derive the optimal control law for engine operation managing during the aircraft flight. For numerical modeling a continuous flight process defined by a system of differential equations is replaced by a di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::57d2fd8ecefd1439968fdc813aa14ab3
https://doaj.org/article/e4200c0dc22c487092da839111f4222c
https://doaj.org/article/e4200c0dc22c487092da839111f4222c
Autor:
Evgeny Filinov, Viktor Rybakov, Ilia N. Krupenich, A Y Tkachenko, Yulia Novikova, V. S. Kuz'michev
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8f6a713652b5000bbe426f08e04c55a3
https://doi.org/10.2514/6.2017-4898
https://doi.org/10.2514/6.2017-4898