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
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Agapovichev, A. V.
Issue
Section
Title
File
Vol 13, No 5-2 (2014): Special Issue
ISSUE WITHOUT SECTION
Development techniques of casting complex parts of aerospace profiles using additive technologies
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Development of a technique of molding small complex parts of gas turbine engines from high-temperature alloys using additive technologies
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Application of numerical simulation systems for the research of the blade casting process in blank production
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Application of the technology of pulsed laser surface coating in correcting casting defects of parts made of «ЖС-32» alloy
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Technology of pulsed laser surface coating in pressing tool repair
(Rus)
Vol 19, No 1 (2020)
MECHANICAL ENGINEERING
New technologies implemented in the design of a low-emission combustion chamber of a gas-turbine unit
(Rus)
Vol 19, No 2 (2020)
MECHANICAL ENGINEERING
Mathematical modeling of the process of selective laser melting of Ti-6Al-4V titanium alloy powder
(Rus)
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