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
Shakhmatov, E. V.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Excitation of pressure pulsations in the working fluid by vibration of the pipeline
(Rus)
Vol 6, No 1 (2007)
TECHNICAL SCIENCES
Modelling characteristics of pressure oscillation dampers with regard for distribution of their parameters
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Pressure pulsation dampener for air controller
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Analysis estimation of pulse jet engine operation in detonation mode
(Rus)
Vol 1, No 1 (2002)
ISSUE WITHOUT SECTION
Main research areas of Samara State Aerospace University
(Rus)
Vol 1, No 1 (2002)
TECHNICAL SCIENCES
Research of influencing of air delivery in a suction pipe line of the centrifugal pump on its vibroacoustical response
(Rus)
Vol 1, No 1 (2002)
TECHNICAL SCIENCES
Research of influencing of air delivery in a suction pipe line of the centrifugal pump on its vibroacoustical response
(Rus)
Vol 22, No 4 (2023)
MECHANICAL ENGINEERING
Model of the turboprop engine reduction gear tooth harmonic spectral component
(Rus)
Vol 23, No 2 (2024)
MECHANICAL ENGINEERING
Modelling width of the spectral component of a gas-turbine engine gearbox output shaft speed
(Rus)
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