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
Бадыков, Р. Р.
Issue
Section
Title
File
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Research of radial face contact seal tightness in the support of the aircraft engine compressor at various operational modes
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Analysis of the thermal state of aircraft engine supports
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Improving the reliability of radial face seals of aircraft engine rotor supports
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Research of serviceability of pulsed face seals with pumpback structures
(Rus)
Vol 22, No 1 (2023)
MECHANICAL ENGINEERING
Development of an experimental plant and a numerical model of an axial magnetic rotor suspension
(Rus)
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