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
Tretyakov, V. V.
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Simulation of drop coagulations in swirled time dependent streams with reference to gas turbine engine combustion chambers
(Rus)
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Development of a generalized model of heat-mass transfer between fuel drops and gas stream with reference to gas turbine engine combustion chambers
(Rus)
Vol 14, No 2 (2015)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Fuel spraying and mixing in a simulated combustion chamber in the presence of air flow precession
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Experimental investigations of fluid atomization by model frontal devices of combustion chambers
(Rus)
Vol 15, No 4 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber
(Rus)
Vol 15, No 4 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder
(Rus)
Vol 17, No 4 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Comparative analysis of fuel distribution downstream of the gas-dynamic flame holder with various methods of injection
(Rus)
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