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
Шулепов, А. П.
Issue
Section
Title
File
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Milling and microballs strengthening conditions influence on high-temperature alloies and steels part’s coating surface quality experimental investigation
(Rus)
Vol 13, No 5-4 (2014): Special Issue
ISSUE WITHOUT SECTION
Creation of a data retrieval system for choosing the optimal cutting tool in manufacturing aircraft engine parts
(Rus)
Vol 15, No 4 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Mathematical model of surface layer formation during hydroabrasive jet machining
(Rus)
Vol 22, No 1 (2023)
MECHANICAL ENGINEERING
Prospects of improving control over the process of electrochemical machining of the blade airfoil profile using the duplex mode method
(Rus)
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