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
Fedorchenko, D. G.
Issue
Section
Title
File
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Results of primary operation of NK-37 engine low emission combustion system
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
The task of creating the bypass engines of various thrust levels using the given gas generator
(Rus)
Vol 13, No 4 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Heat-shielding zirconium dioxide coating on an intermetallic substrate obtained by the method of high-energy plasma spraying for gas-turbine engine turbine blades
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Analysis of the thermal state of aircraft engine supports
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Influence of vibration conectedness on eigenmode shapes of bladed disks with non-identical blades
(Rus)
Vol 13, No 5-4 (2014): Special Issue
ISSUE WITHOUT SECTION
Formation of spread in resonance stresses in bladed disks with non-identical blades and loose vibration conectedness
(Rus)
Vol 13, No 5-4 (2014): Special Issue
ISSUE WITHOUT SECTION
Calculation of exciting aerodynamic load on a gas turbine engine compressor blade induced by the effect of a non-uniform gas flow
(Rus)
Vol 18, No 1 (2019)
MECHANICAL ENGINEERING
Application of additive technology of selective laser melting (SLM) in designing a low emission combustion chamber of a gas turbine plant
(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)
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