Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Leonid Shabliy"'
Publikováno v:
SIMULTECH
Publikováno v:
Procedia Engineering. 104:29-35
This paper describes the designing process of rocket engine with thrust 25N for system of orientation and starting of spacecraft instead the prototype with burnout chamber defect that was not fixed during the development to completely exclude the bur
Publikováno v:
The Open Mechanical Engineering Journal. 8:445-449
The aim of this article was the development of the gas-dynamic models allowing to calculate the working processes of the gas turbine engine (GTE) in the compressor, in the combustion chamber and in the turbine at the same time. The possibilities of s
Publikováno v:
Volume 2C: Turbomachinery.
This article describes the technique for CFD-modeling of a powerful two-stage pump with the following main parameters: main rotor speed is 13,300 rpm, inlet pressure is 0.2 MPa, pressure head is more than 3,000 meters with mass flow of 250 kg/s. The
Publikováno v:
Volume 2B: Turbomachinery.
This article reports CFD-modeling technique of flow through a kerosene pump and suggests appropriate CFD tools, model configuration, types of boundary conditions, turbulence models and meshing technique. The flow features were analyzed and error of t
Publikováno v:
ASME 2014 Gas Turbine India Conference.
In this paper, we present a methodology to integrated simulation of gas turbine engine (GTE). This method allow to predict performance of GTE components workflows with account the mutual influence. Steady state CFD modeling of compressor, combustion
Publikováno v:
ASME 2014 Gas Turbine India Conference.
This article presents the CFD-modeling of fuel pump with program ANSYS CFX. Paper gives detailed description of CFD model and techniques for improving its adequacy. Verification with experimental data allows recognize used CFD-model adequate within t
Autor:
Aleksandr Cherniaev, Leonid Shabliy
Publikováno v:
ASME 2014 Gas Turbine India Conference.
The article describes an example of design optimizing of gas turbine compressor blade row with coupled simulation (coupled gas dynamics and strength) using technology of fluid-structure-interaction simulation by ANSYS tools. Geometry model, gas-dynam
Publikováno v:
Scopus-Elsevier
ResearcherID
SIMULTECH
ResearcherID
SIMULTECH
The research goal was the methodology to calculate gas turbine engine (GTE) workflows and in the compressor, in the combustion chamber and the turbine at the same time. Our method allows predicting interactions between components of a GTE. Solution i
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https://explore.openaire.eu/search/publication?articleId=doi_dedup___::776f51381c72268c4d63add415f381d1
http://www.scopus.com/inward/record.url?eid=2-s2.0-85015831357&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-85015831357&partnerID=MN8TOARS
Publikováno v:
Scopus-Elsevier
ResearcherID
ResearcherID
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::6440623188931db30e6939a0970793cb
http://www.scopus.com/inward/record.url?eid=2-s2.0-84915732569&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84915732569&partnerID=MN8TOARS