VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
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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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Author Details
Author Details
Семёнычев, В. В.
Issue
Section
Title
File
Vol 8, No 3-2 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Properties and structure of "trivalent" chromium coatings, deposited with nanoparticles of metal oxides
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Effect of "trivalent" chrome plating structural steel on its performance
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Wear resistance of chromium coatings, formed in trivalent electrolytes at presence of nanosized particles of metal oxides
(Rus)
Vol 14, No 3 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Specific electrical conductivity of chromium plating and nickel plating electrolytes
(Rus)
Vol 14, No 3 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
The nature of «black spots» formation on the surface of large parts made of aluminum alloys in the process of anodic oxidising
(Rus)
Vol 21, No 3 (2022)
MECHANICAL ENGINEERING
Application of acoustic emission and scleroscopy for the analysis of carbon fiber-reinforced plastic samples with different degrees of matrix curing
(Rus)
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