VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine
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Author Details
Author Details
Zubanov, V. M.
Issue
Section
Title
File
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
The parameters of turbulence models and grids investigation on CFD results of plane turbine cascade
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Methods of modeling the work process of hydrogen screw-centrifugal pumps using ANSYS CFD
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Procedure of validated CFD-modeling of a two-stage screw-centrifugal pump
(Rus)
Vol 15, No 4 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen
(Rus)
Vol 15, No 4 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Simulation of the work process of a two-stage pump with a first-stage hydraulic drive
(Rus)
Vol 19, No 3 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time
(Rus)
Vol 22, No 1 (2023)
MECHANICAL ENGINEERING
Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade
(Rus)
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