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
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residual stresses
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structure
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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
Balyakin, V. B.
Issue
Section
Title
File
Vol 12, No 2 (2013)
MECHANICAL ENGINEERING AND POWER ENGINEERING
The influence of design and performance parameters of an angular ball bearing on the stiffness of gas turbine engine rotor supports
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Parametric instability of the dynamics of gear wheels
(Rus)
Vol 13, No 5-2 (2014): Special Issue
ISSUE WITHOUT SECTION
Modification of the surface of silicon carbide parts by laser treatment for improving their tribological properties
(Rus)
Vol 10, No 3-2 (2011): Special Issue
HUMANITIES
Training for innovative engineering through through parametrization
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Dynamik experimental researches of the face gas dynamic seal
(Rus)
Vol 2, No 1 (2003)
TECHNICAL SCIENCES
REDUCTION OF TURBO-PUMP UNIT VIBRATION BY REGULATING BEARING RIGIDITY
(Rus)
Vol 22, No 2 (2023)
MECHANICAL ENGINEERING
Influence of complex loading of radial bearings of the oscillation groups of liquid propellant engine steering gear on the frictional moment
(Rus)
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